Loch Fyne Skiff – ‘Cumbrae Lass’

  

One of two replica Loch Fyne Skiffs, or ‘Slopemasts’ as they were known on the west coast; she was built by MacDuff Shipyards in the 1970’s she is a unique piece of Scottish Maritime history. Having spent the last 25+years in the same ownership based in Stornoway she has proved a very capable and sea worthy classic cruising boat. Delivered by the vendor to the main land for collection by the new owner we were please to assist with arranging to have the boat de-rigged and prepared for road transport to her new home in Brixham

 

Comments

This traditional skiff was designed by G L Watson and built by MacDuff Boatbuilding in 1979 as a cruising yacht along the lines of the iconic Loch Fyne herring skiff. Instantly recognisable with an almost plumb stem, the unmistakable stern and steeply raked sternpost. Ruggedly built in the fishing boat style she is a rare opportunity to acquire a relatively recent traditional boat with a recent modern Diesel. During recent years the current owner has upgraded the boat making her easier to handle with a smaller crew, with additions to the inventory and fit out on and below decks.

A deep cockpit aft is well sheltered by the doghouse with the long tiller extending far enough forward for the helmsman to enjoy the full benefits of the doghouse. Below decks comfortable accommodation for a full crew of 4 is provided with all bunks of a good size and the large saloon provides an excellent space for eating and entertaining.

With her interesting history and classic design she would be quiet at home attending classic boat festivals around Europe if desired. Currently lying afloat in Stornoway, Isle of Lewis. Contact office to arrange viewing or discuss transport arrangements.

 

Features of Loch Fyne Skiff:

Basic data

Type: Sailing cruiser

Year : 1979

Length: 9.9 m

Location: Aberdeenshire (United Kingdom)

Name: Cumbrae Lass

Flag: -

Shipyard: Loch Fyne

Material: Wood

Dimensions

Beam: 3.0 m

Draft: -

Ballast: -

Displacement: 18290 Kg

Capacity

Maximum number of passengers: -

Cabins: -

Berths: -

Heads: -

Water capacity: -

Motor

Number of engines: 1

Power: 62 HP

Fuel capacity: -

Motor type : Inboard

Fuel type : Diesel

Make of the motor: Beta (Kubota) BF2803

Engine usage (hours): -

This Sailing cruiser's equipment

Electronics

Gps, Depthsounder, Vhf, Compass, Plotter, Radar

 

Deck equipment

Liferaft, Tender, Tiller, Cockpit cover

 

Comfort / Interior

Manual bilge pump, Marine head, Oven, Heating

 

Additional Equipment

30kg CQR mainstay with 60 metres 10mm chain.CQR and fisherman kedges.

 

Construction

Designed around the lines of iconic Loch Fyne Skiff, a traditional working vessel; and manufactured by MacDuff Boatbuilding as you would expect the build is of a robust nature. Below decks the fit out is traditional in type and as such the massive structural frames and body planking are all readily visible. The body is of carvel type development with planking of 1.25" larch on substantial 3"x6" sawn oak frames. The deck is of 0.75" marina plywood on oak beams, sheathed in GRP. All interior fit out is of marina grade plywood with larch trims.

During the last lay-up the rudder was removed and overhauled including some subtle changes to its profile. These overhaul and modification has given the rudder improved qualities, reducing weather helm and making the vessel less tiring to helm with the rudder now being semi-balanced.

The vessel was last surveyed for insurance purposes in 2012 and a copy of this survey is available for any interested parties.

  

Accommodation

Below decks the fit out is of a traditional type with minimal linings to conceal the vessels structural timbers and planking giving the vessel a very traditional feel. Despite the classic design the seating space below decks is very roomy and well pre-owned with 5'10" of headroom and all bunks being 6'+.

The forepeak has two large single bunks in a V-berth formation with the stout square sectioned mast running through the room onto its solid oak keel step. Storage is provided with a selection of shelves and a small hanging safe

A small quantity room is located to starboard at the forward end of the bar with a sea toilet and pull out tank.

The bar area in the central part of the vessel is open plan in layout creating a great living space. The recently re-tailored galley is located at the forward end of the space to seaport with gasoline cooker, sink and stowage. A large bar desk is tailored centrally with stout bench seating running along its range outboard seaport and starboard. A diesel fired heater is located at the forward end of the bar with 2 hotplates on top to make use of excess heat, ideal for a kettle.

Two large quarter bunks are located seaport and starboard at the aft end of the space and run under the cockpit, both are of generous proseaportions.

 

Colosseum

Following, a text, in english, from the Wikipedia the Free Encyclopedia:

The Colosseum, or the Coliseum, originally the Flavian Amphitheatre (Latin: Amphitheatrum Flavium, Italian Anfiteatro Flavio or Colosseo), is an elliptical amphitheatre in the centre of the city of Rome, Italy, the largest ever built in the Roman Empire. It is considered one of the greatest works of Roman architecture and Roman engineering.

Occupying a site just east of the Roman Forum, its construction started between 70 and 72 AD[1] under the emperor Vespasian and was completed in 80 AD under Titus,[2] with further modifications being made during Domitian's reign (81–96).[3] The name "Amphitheatrum Flavium" derives from both Vespasian's and Titus's family name (Flavius, from the gens Flavia).

Capable of seating 50,000 spectators,[1][4][5] the Colosseum was used for gladiatorial contests and public spectacles such as mock sea battles, animal hunts, executions, re-enactments of famous battles, and dramas based on Classical mythology. The building ceased to be used for entertainment in the early medieval era. It was later reused for such purposes as housing, workshops, quarters for a religious order, a fortress, a quarry, and a Christian shrine.

Although in the 21st century it stays partially ruined because of damage caused by devastating earthquakes and stone-robbers, the Colosseum is an iconic symbol of Imperial Rome. It is one of Rome's most popular tourist attractions and still has close connections with the Roman Catholic Church, as each Good Friday the Pope leads a torchlit "Way of the Cross" procession that starts in the area around the Colosseum.[6]

The Colosseum is also depicted on the Italian version of the five-cent euro coin.

The Colosseum's original Latin name was Amphitheatrum Flavium, often anglicized as Flavian Amphitheater. The building was constructed by emperors of the Flavian dynasty, hence its original name, after the reign of Emperor Nero.[7] This name is still used in modern English, but generally the structure is better known as the Colosseum. In antiquity, Romans may have referred to the Colosseum by the unofficial name Amphitheatrum Caesareum; this name could have been strictly poetic.[8][9] This name was not exclusive to the Colosseum; Vespasian and Titus, builders of the Colosseum, also constructed an amphitheater of the same name in Puteoli (modern Pozzuoli).[10]

The name Colosseum has long been believed to be derived from a colossal statue of Nero nearby.[3] (the statue of Nero itself being named after one of the original ancient wonders, the Colossus of Rhodes[citation needed]. This statue was later remodeled by Nero's successors into the likeness of Helios (Sol) or Apollo, the sun god, by adding the appropriate solar crown. Nero's head was also replaced several times with the heads of succeeding emperors. Despite its pagan links, the statue remained standing well into the medieval era and was credited with magical powers. It came to be seen as an iconic symbol of the permanence of Rome.

In the 8th century, a famous epigram attributed to the Venerable Bede celebrated the symbolic significance of the statue in a prophecy that is variously quoted: Quamdiu stat Colisæus, stat et Roma; quando cadet colisæus, cadet et Roma; quando cadet Roma, cadet et mundus ("as long as the Colossus stands, so shall Rome; when the Colossus falls, Rome shall fall; when Rome falls, so falls the world").[11] This is often mistranslated to refer to the Colosseum rather than the Colossus (as in, for instance, Byron's poem Childe Harold's Pilgrimage). However, at the time that the Pseudo-Bede wrote, the masculine noun coliseus was applied to the statue rather than to what was still known as the Flavian amphitheatre.

The Colossus did eventually fall, possibly being pulled down to reuse its bronze. By the year 1000 the name "Colosseum" had been coined to refer to the amphitheatre. The statue itself was largely forgotten and only its base survives, situated between the Colosseum and the nearby Temple of Venus and Roma.[12]

The name further evolved to Coliseum during the Middle Ages. In Italy, the amphitheatre is still known as il Colosseo, and other Romance languages have come to use similar forms such as le Colisée (French), el Coliseo (Spanish) and o Coliseu (Portuguese).

Construction of the Colosseum began under the rule of the Emperor Vespasian[3] in around 70–72AD. The site chosen was a flat area on the floor of a low valley between the Caelian, Esquiline and Palatine Hills, through which a canalised stream ran. By the 2nd century BC the area was densely inhabited. It was devastated by the Great Fire of Rome in AD 64, following which Nero seized much of the area to add to his personal domain. He built the grandiose Domus Aurea on the site, in front of which he created an artificial lake surrounded by pavilions, gardens and porticoes. The existing Aqua Claudia aqueduct was extended to supply water to the area and the gigantic bronze Colossus of Nero was set up nearby at the entrance to the Domus Aurea.[12]

Although the Colossus was preserved, much of the Domus Aurea was torn down. The lake was filled in and the land reused as the location for the new Flavian Amphitheatre. Gladiatorial schools and other support buildings were constructed nearby within the former grounds of the Domus Aurea. According to a reconstructed inscription found on the site, "the emperor Vespasian ordered this new amphitheatre to be erected from his general's share of the booty." This is thought to refer to the vast quantity of treasure seized by the Romans following their victory in the Great Jewish Revolt in 70AD. The Colosseum can be thus interpreted as a great triumphal monument built in the Roman tradition of celebrating great victories[12], placating the Roman people instead of returning soldiers. Vespasian's decision to build the Colosseum on the site of Nero's lake can also be seen as a populist gesture of returning to the people an area of the city which Nero had appropriated for his own use. In contrast to many other amphitheatres, which were located on the outskirts of a city, the Colosseum was constructed in the city centre; in effect, placing it both literally and symbolically at the heart of Rome.

The Colosseum had been completed up to the third story by the time of Vespasian's death in 79. The top level was finished and the building inaugurated by his son, Titus, in 80.[3] Dio Cassius recounts that over 9,000 wild animals were killed during the inaugural games of the amphitheatre. The building was remodelled further under Vespasian's younger son, the newly designated Emperor Domitian, who constructed the hypogeum, a series of underground tunnels used to house animals and slaves. He also added a gallery to the top of the Colosseum to increase its seating capacity.

In 217, the Colosseum was badly damaged by a major fire (caused by lightning, according to Dio Cassius[13]) which destroyed the wooden upper levels of the amphitheatre's interior. It was not fully repaired until about 240 and underwent further repairs in 250 or 252 and again in 320. An inscription records the restoration of various parts of the Colosseum under Theodosius II and Valentinian III (reigned 425–455), possibly to repair damage caused by a major earthquake in 443; more work followed in 484[14] and 508. The arena continued to be used for contests well into the 6th century, with gladiatorial fights last mentioned around 435. Animal hunts continued until at least 523, when Anicius Maximus celebrated his consulship with some venationes, criticised by King Theodoric the Great for their high cost.

The Colosseum underwent several radical changes of use during the medieval period. By the late 6th century a small church had been built into the structure of the amphitheatre, though this apparently did not confer any particular religious significance on the building as a whole. The arena was converted into a cemetery. The numerous vaulted spaces in the arcades under the seating were converted into housing and workshops, and are recorded as still being rented out as late as the 12th century. Around 1200 the Frangipani family took over the Colosseum and fortified it, apparently using it as a castle.

Severe damage was inflicted on the Colosseum by the great earthquake in 1349, causing the outer south side, lying on a less stable alluvional terrain, to collapse. Much of the tumbled stone was reused to build palaces, churches, hospitals and other buildings elsewhere in Rome. A religious order moved into the northern third of the Colosseum in the mid-14th century and continued to inhabit it until as late as the early 19th century. The interior of the amphitheatre was extensively stripped of stone, which was reused elsewhere, or (in the case of the marble façade) was burned to make quicklime.[12] The bronze clamps which held the stonework together were pried or hacked out of the walls, leaving numerous pockmarks which still scar the building today.

During the 16th and 17th century, Church officials sought a productive role for the vast derelict hulk of the Colosseum. Pope Sixtus V (1585–1590) planned to turn the building into a wool factory to provide employment for Rome's prostitutes, though this proposal fell through with his premature death.[15] In 1671 Cardinal Altieri authorized its use for bullfights; a public outcry caused the idea to be hastily abandoned.

In 1749, Pope Benedict XIV endorsed as official Church policy the view that the Colosseum was a sacred site where early Christians had been martyred. He forbade the use of the Colosseum as a quarry and consecrated the building to the Passion of Christ and installed Stations of the Cross, declaring it sanctified by the blood of the Christian martyrs who perished there (see Christians and the Colosseum). However there is no historical evidence to support Benedict's claim, nor is there even any evidence that anyone prior to the 16th century suggested this might be the case; the Catholic Encyclopedia concludes that there are no historical grounds for the supposition. Later popes initiated various stabilization and restoration projects, removing the extensive vegetation which had overgrown the structure and threatened to damage it further. The façade was reinforced with triangular brick wedges in 1807 and 1827, and the interior was repaired in 1831, 1846 and in the 1930s. The arena substructure was partly excavated in 1810–1814 and 1874 and was fully exposed under Benito Mussolini in the 1930s.

The Colosseum is today one of Rome's most popular tourist attractions, receiving millions of visitors annually. The effects of pollution and general deterioration over time prompted a major restoration programme carried out between 1993 and 2000, at a cost of 40 billion Italian lire ($19.3m / €20.6m at 2000 prices). In recent years it has become a symbol of the international campaign against capital punishment, which was abolished in Italy in 1948. Several anti–death penalty demonstrations took place in front of the Colosseum in 2000. Since that time, as a gesture against the death penalty, the local authorities of Rome change the color of the Colosseum's night time illumination from white to gold whenever a person condemned to the death penalty anywhere in the world gets their sentence commuted or is released,[16] or if a jurisdiction abolishes the death penalty. Most recently, the Colosseum was illuminated in gold when capital punishment was abolished in the American state of New Mexico in April 2009.

Because of the ruined state of the interior, it is impractical to use the Colosseum to host large events; only a few hundred spectators can be accommodated in temporary seating. However, much larger concerts have been held just outside, using the Colosseum as a backdrop. Performers who have played at the Colosseum in recent years have included Ray Charles (May 2002),[18] Paul McCartney (May 2003),[19] Elton John (September 2005),[20] and Billy Joel (July 2006).

Exterior

Unlike earlier Greek theatres that were built into hillsides, the Colosseum is an entirely free-standing structure. It derives its basic exterior and interior architecture from that of two Roman theatres back to back. It is elliptical in plan and is 189 meters (615 ft / 640 Roman feet) long, and 156 meters (510 ft / 528 Roman feet) wide, with a base area of 6 acres (24,000 m2). The height of the outer wall is 48 meters (157 ft / 165 Roman feet). The perimeter originally measured 545 meters (1,788 ft / 1,835 Roman feet). The central arena is an oval 87 m (287 ft) long and 55 m (180 ft) wide, surrounded by a wall 5 m (15 ft) high, above which rose tiers of seating.

The outer wall is estimated to have required over 100,000 cubic meters (131,000 cu yd) of travertine stone which were set without mortar held together by 300 tons of iron clamps.[12] However, it has suffered extensive damage over the centuries, with large segments having collapsed following earthquakes. The north side of the perimeter wall is still standing; the distinctive triangular brick wedges at each end are modern additions, having been constructed in the early 19th century to shore up the wall. The remainder of the present-day exterior of the Colosseum is in fact the original interior wall.

The surviving part of the outer wall's monumental façade comprises three stories of superimposed arcades surmounted by a podium on which stands a tall attic, both of which are pierced by windows interspersed at regular intervals. The arcades are framed by half-columns of the Tuscan, Ionic, and Corinthian orders, while the attic is decorated with Corinthian pilasters.[21] Each of the arches in the second- and third-floor arcades framed statues, probably honoring divinities and other figures from Classical mythology.

Two hundred and forty mast corbels were positioned around the top of the attic. They originally supported a retractable awning, known as the velarium, that kept the sun and rain off spectators. This consisted of a canvas-covered, net-like structure made of ropes, with a hole in the center.[3] It covered two-thirds of the arena, and sloped down towards the center to catch the wind and provide a breeze for the audience. Sailors, specially enlisted from the Roman naval headquarters at Misenum and housed in the nearby Castra Misenatium, were used to work the velarium.[22]

The Colosseum's huge crowd capacity made it essential that the venue could be filled or evacuated quickly. Its architects adopted solutions very similar to those used in modern stadiums to deal with the same problem. The amphitheatre was ringed by eighty entrances at ground level, 76 of which were used by ordinary spectators.[3] Each entrance and exit was numbered, as was each staircase. The northern main entrance was reserved for the Roman Emperor and his aides, whilst the other three axial entrances were most likely used by the elite. All four axial entrances were richly decorated with painted stucco reliefs, of which fragments survive. Many of the original outer entrances have disappeared with the collapse of the perimeter wall, but entrances XXIII (23) to LIV (54) still survive.[12]

Spectators were given tickets in the form of numbered pottery shards, which directed them to the appropriate section and row. They accessed their seats via vomitoria (singular vomitorium), passageways that opened into a tier of seats from below or behind. These quickly dispersed people into their seats and, upon conclusion of the event or in an emergency evacuation, could permit their exit within only a few minutes. The name vomitoria derived from the Latin word for a rapid discharge, from which English derives the word vomit.

Interior

According to the Codex-Calendar of 354, the Colosseum could accommodate 87,000 people, although modern estimates put the figure at around 50,000. They were seated in a tiered arrangement that reflected the rigidly stratified nature of Roman society. Special boxes were provided at the north and south ends respectively for the Emperor and the Vestal Virgins, providing the best views of the arena. Flanking them at the same level was a broad platform or podium for the senatorial class, who were allowed to bring their own chairs. The names of some 5th century senators can still be seen carved into the stonework, presumably reserving areas for their use.

The tier above the senators, known as the maenianum primum, was occupied by the non-senatorial noble class or knights (equites). The next level up, the maenianum secundum, was originally reserved for ordinary Roman citizens (plebians) and was divided into two sections. The lower part (the immum) was for wealthy citizens, while the upper part (the summum) was for poor citizens. Specific sectors were provided for other social groups: for instance, boys with their tutors, soldiers on leave, foreign dignitaries, scribes, heralds, priests and so on. Stone (and later marble) seating was provided for the citizens and nobles, who presumably would have brought their own cushions with them. Inscriptions identified the areas reserved for specific groups.

Another level, the maenianum secundum in legneis, was added at the very top of the building during the reign of Domitian. This comprised a gallery for the common poor, slaves and women. It would have been either standing room only, or would have had very steep wooden benches. Some groups were banned altogether from the Colosseum, notably gravediggers, actors and former gladiators.

Each tier was divided into sections (maeniana) by curved passages and low walls (praecinctiones or baltei), and were subdivided into cunei, or wedges, by the steps and aisles from the vomitoria. Each row (gradus) of seats was numbered, permitting each individual seat to be exactly designated by its gradus, cuneus, and number.

The arena itself was 83 meters by 48 meters (272 ft by 157 ft / 280 by 163 Roman feet).[12] It comprised a wooden floor covered by sand (the Latin word for sand is harena or arena), covering an elaborate underground structure called the hypogeum (literally meaning "underground"). Little now remains of the original arena floor, but the hypogeum is still clearly visible. It consisted of a two-level subterranean network of tunnels and cages beneath the arena where gladiators and animals were held before contests began. Eighty vertical shafts provided instant access to the arena for caged animals and scenery pieces concealed underneath; larger hinged platforms, called hegmata, provided access for elephants and the like. It was restructured on numerous occasions; at least twelve different phases of construction can be seen.[12]

The hypogeum was connected by underground tunnels to a number of points outside the Colosseum. Animals and performers were brought through the tunnel from nearby stables, with the gladiators' barracks at the Ludus Magnus to the east also being connected by tunnels. Separate tunnels were provided for the Emperor and the Vestal Virgins to permit them to enter and exit the Colosseum without needing to pass through the crowds.[12]

Substantial quantities of machinery also existed in the hypogeum. Elevators and pulleys raised and lowered scenery and props, as well as lifting caged animals to the surface for release. There is evidence for the existence of major hydraulic mechanisms[12] and according to ancient accounts, it was possible to flood the arena rapidly, presumably via a connection to a nearby aqueduct.

The Colosseum and its activities supported a substantial industry in the area. In addition to the amphitheatre itself, many other buildings nearby were linked to the games. Immediately to the east is the remains of the Ludus Magnus, a training school for gladiators. This was connected to the Colosseum by an underground passage, to allow easy access for the gladiators. The Ludus Magnus had its own miniature training arena, which was itself a popular attraction for Roman spectators. Other training schools were in the same area, including the Ludus Matutinus (Morning School), where fighters of animals were trained, plus the Dacian and Gallic Schools.

Also nearby were the Armamentarium, comprising an armory to store weapons; the Summum Choragium, where machinery was stored; the Sanitarium, which had facilities to treat wounded gladiators; and the Spoliarium, where bodies of dead gladiators were stripped of their armor and disposed of.

Around the perimeter of the Colosseum, at a distance of 18 m (59 ft) from the perimeter, was a series of tall stone posts, with five remaining on the eastern side. Various explanations have been advanced for their presence; they may have been a religious boundary, or an outer boundary for ticket checks, or an anchor for the velarium or awning.

Right next to the Colosseum is also the Arch of Constantine.

he Colosseum was used to host gladiatorial shows as well as a variety of other events. The shows, called munera, were always given by private individuals rather than the state. They had a strong religious element but were also demonstrations of power and family prestige, and were immensely popular with the population. Another popular type of show was the animal hunt, or venatio. This utilized a great variety of wild beasts, mainly imported from Africa and the Middle East, and included creatures such as rhinoceros, hippopotamuses, elephants, giraffes, aurochs, wisents, barbary lions, panthers, leopards, bears, caspian tigers, crocodiles and ostriches. Battles and hunts were often staged amid elaborate sets with movable trees and buildings. Such events were occasionally on a huge scale; Trajan is said to have celebrated his victories in Dacia in 107 with contests involving 11,000 animals and 10,000 gladiators over the course of 123 days.

During the early days of the Colosseum, ancient writers recorded that the building was used for naumachiae (more properly known as navalia proelia) or simulated sea battles. Accounts of the inaugural games held by Titus in AD 80 describe it being filled with water for a display of specially trained swimming horses and bulls. There is also an account of a re-enactment of a famous sea battle between the Corcyrean (Corfiot) Greeks and the Corinthians. This has been the subject of some debate among historians; although providing the water would not have been a problem, it is unclear how the arena could have been waterproofed, nor would there have been enough space in the arena for the warships to move around. It has been suggested that the reports either have the location wrong, or that the Colosseum originally featured a wide floodable channel down its central axis (which would later have been replaced by the hypogeum).[12]

Sylvae or recreations of natural scenes were also held in the arena. Painters, technicians and architects would construct a simulation of a forest with real trees and bushes planted in the arena's floor. Animals would be introduced to populate the scene for the delight of the crowd. Such scenes might be used simply to display a natural environment for the urban population, or could otherwise be used as the backdrop for hunts or dramas depicting episodes from mythology. They were also occasionally used for executions in which the hero of the story — played by a condemned person — was killed in one of various gruesome but mythologically authentic ways, such as being mauled by beasts or burned to death.

The Colosseum today is now a major tourist attraction in Rome with thousands of tourists each year paying to view the interior arena, though entrance for EU citizens is partially subsidised, and under-18 and over-65 EU citizens' entrances are free.[24] There is now a museum dedicated to Eros located in the upper floor of the outer wall of the building. Part of the arena floor has been re-floored. Beneath the Colosseum, a network of subterranean passageways once used to transport wild animals and gladiators to the arena opened to the public in summer 2010.[25]

The Colosseum is also the site of Roman Catholic ceremonies in the 20th and 21st centuries. For instance, Pope Benedict XVI leads the Stations of the Cross called the Scriptural Way of the Cross (which calls for more meditation) at the Colosseum[26][27] on Good Fridays.

In the Middle Ages, the Colosseum was clearly not regarded as a sacred site. Its use as a fortress and then a quarry demonstrates how little spiritual importance was attached to it, at a time when sites associated with martyrs were highly venerated. It was not included in the itineraries compiled for the use of pilgrims nor in works such as the 12th century Mirabilia Urbis Romae ("Marvels of the City of Rome"), which claims the Circus Flaminius — but not the Colosseum — as the site of martyrdoms. Part of the structure was inhabited by a Christian order, but apparently not for any particular religious reason.

It appears to have been only in the 16th and 17th centuries that the Colosseum came to be regarded as a Christian site. Pope Pius V (1566–1572) is said to have recommended that pilgrims gather sand from the arena of the Colosseum to serve as a relic, on the grounds that it was impregnated with the blood of martyrs. This seems to have been a minority view until it was popularised nearly a century later by Fioravante Martinelli, who listed the Colosseum at the head of a list of places sacred to the martyrs in his 1653 book Roma ex ethnica sacra.

Martinelli's book evidently had an effect on public opinion; in response to Cardinal Altieri's proposal some years later to turn the Colosseum into a bullring, Carlo Tomassi published a pamphlet in protest against what he regarded as an act of desecration. The ensuing controversy persuaded Pope Clement X to close the Colosseum's external arcades and declare it a sanctuary, though quarrying continued for some time.

At the instance of St. Leonard of Port Maurice, Pope Benedict XIV (1740–1758) forbade the quarrying of the Colosseum and erected Stations of the Cross around the arena, which remained until February 1874. St. Benedict Joseph Labre spent the later years of his life within the walls of the Colosseum, living on alms, prior to his death in 1783. Several 19th century popes funded repair and restoration work on the Colosseum, and it still retains a Christian connection today. Crosses stand in several points around the arena and every Good Friday the Pope leads a Via Crucis procession to the amphitheatre.

 

Coliseu (Colosseo)

A seguir, um texto, em português, da Wikipédia, a enciclopédia livre:

 

O Coliseu, também conhecido como Anfiteatro Flaviano, deve seu nome à expressão latina Colosseum (ou Coliseus, no latim tardio), devido à estátua colossal de Nero, que ficava perto a edificação. Localizado no centro de Roma, é uma excepção de entre os anfiteatros pelo seu volume e relevo arquitectónico. Originalmente capaz de albergar perto de 50 000 pessoas, e com 48 metros de altura, era usado para variados espetáculos. Foi construído a leste do fórum romano e demorou entre 8 a 10 anos a ser construído.

O Coliseu foi utilizado durante aproximadamente 500 anos, tendo sido o último registro efetuado no século VI da nossa era, bastante depois da queda de Roma em 476. O edifício deixou de ser usado para entretenimento no começo da era medieval, mas foi mais tarde usado como habitação, oficina, forte, pedreira, sede de ordens religiosas e templo cristão.

Embora esteja agora em ruínas devido a terremotos e pilhagens, o Coliseu sempre foi visto como símbolo do Império Romano, sendo um dos melhores exemplos da sua arquitectura. Actualmente é uma das maiores atrações turísticas em Roma e em 7 de julho de 2007 foi eleita umas das "Sete maravilhas do mundo moderno". Além disso, o Coliseu ainda tem ligações à igreja, com o Papa a liderar a procissão da Via Sacra até ao Coliseu todas as Sextas-feiras Santas.

O coliseu era um local onde seriam exibidos toda uma série de espectáculos, inseridos nos vários tipos de jogos realizados na urbe. Os combates entre gladiadores, chamados muneras, eram sempre pagos por pessoas individuais em busca de prestígio e poder em vez do estado. A arena (87,5 m por 55 m) possuía um piso de madeira, normalmente coberto de areia para absorver o sangue dos combates (certa vez foi colocada água na representação de uma batalha naval), sob o qual existia um nível subterrâneo com celas e jaulas que tinham acessos diretos para a arena; Alguns detalhes dessa construção, como a cobertura removível que poupava os espectadores do sol, são bastante interessantes, e mostram o refinamento atingido pelos construtores romanos. Formado por cinco anéis concêntricos de arcos e abóbadas, o Coliseu representa bem o avanço introduzido pelos romanos à engenharia de estruturas. Esses arcos são de concreto (de cimento natural) revestidos por alvenaria. Na verdade, a alvenaria era construída simultaneamente e já servia de forma para a concretagem. Outro tipo de espetáculos era a caça de animais, ou venatio, onde eram utilizados animais selvagens importados de África. Os animais mais utilizados eram os grandes felinos como leões, leopardos e panteras, mas animais como rinocerontes, hipopótamos, elefantes, girafas, crocodilos e avestruzes eram também utilizados. As caçadas, tal como as representações de batalhas famosas, eram efetuadas em elaborados cenários onde constavam árvores e edifícios amovíveis.

Estas últimas eram por vezes representadas numa escala gigante; Trajano celebrou a sua vitória em Dácia no ano 107 com concursos envolvendo 11 000 animais e 10 000 gladiadores no decorrer de 123 dias.

Segundo o documentário produzido pelo canal televisivo fechado, History Channel, o Coliseu também era utilizado para a realização de naumaquias, ou batalhas navais. O coliseu era inundado por dutos subterrâneos alimentados pelos aquedutos que traziam água de longe. Passada esta fase, foi construída uma estrutura, que é a que podemos ver hoje nas ruínas do Coliseu, com altura de um prédio de dois andares, onde no passado se concentravam os gladiadores, feras e todo o pessoal que organizava os duelos que ocorreriam na arena. A arena era como um grande palco, feito de madeira, e se chama arena, que em italiano significa areia, porque era jogada areia sob a estrutura de madeira para esconder as imperfeições. Os animais podiam ser inseridos nos duelos a qualquer momento por um esquema de elevadores que surgiam em alguns pontos da arena; o filme "Gladiador" retrata muito bem esta questão dos elevadores. Os estudiosos, há pouco tempo, descobriram uma rede de dutos inundados por baixo da arena do Coliseu. Acredita-se que o Coliseu foi construído onde, outrora, foi o lago do Palácio Dourado de Nero; O imperador Vespasiano escolheu o local da construção para que o mal causado por Nero fosse esquecido por uma construção gloriosa.

Sylvae, ou recreações de cenas naturais eram também realizadas no Coliseu. Pintores, técnicos e arquitectos construiriam simulações de florestas com árvores e arbustos reais plantados no chão da arena. Animais seriam então introduzidos para dar vida à simulação. Esses cenários podiam servir só para agrado do público ou como pano de fundo para caçadas ou dramas representando episódios da mitologia romana, tão autênticos quanto possível, ao ponto de pessoas condenadas fazerem o papel de heróis onde eram mortos de maneiras horríveis mas mitologicamente autênticas, como mutilados por animais ou queimados vivos.

Embora o Coliseu tenha funcionado até ao século VI da nossa Era, foram proibidos os jogos com mortes humanas desde 404, sendo apenas massacrados animais como elefantes, panteras ou leões.

O Coliseu era sobretudo um enorme instrumento de propaganda e difusão da filosofia de toda uma civilização, e tal como era já profetizado pelo monge e historiador inglês Beda na sua obra do século VII "De temporibus liber": "Enquanto o Coliseu se mantiver de pé, Roma permanecerá; quando o Coliseu ruir, Roma ruirá e quando Roma cair, o mundo cairá".

A construção do Coliseu foi iniciada por Vespasiano, nos anos 70 da nossa era. O edifício foi inaugurado por Tito, em 80, embora apenas tivesse sido finalizado poucos anos depois. Empresa colossal, este edifício, inicialmente, poderia sustentar no seu interior cerca de 50 000 espectadores, constando de três andares. Aquando do reinado de Alexandre Severo e Gordiano III, é ampliado com um quarto andar, podendo suster agora cerca de 90 000 espectadores. A grandiosidade deste monumento testemunha verdadeiramente o poder e esplendor de Roma na época dos Flávios.

Os jogos inaugurais do Coliseu tiveram lugar ano 80, sob o mandato de Tito, para celebrar a finalização da construção. Depois do curto reinado de Tito começar com vários meses de desastres, incluindo a erupção do Monte Vesúvio, um incêndio em Roma, e um surto de peste, o mesmo imperador inaugurou o edifício com uns jogos pródigos que duraram mais de cem dias, talvez para tentar apaziguar o público romano e os deuses. Nesses jogos de cem dias terão ocorrido combates de gladiadores, venationes (lutas de animais), execuções, batalhas navais, caçadas e outros divertimentos numa escala sem precedentes.

O Coliseu, como não se encontrava inserido numa zona de encosta, enterrado, tal como normalmente sucede com a generalidade dos teatros e anfiteatros romanos, possuía um “anel” artificial de rocha à sua volta, para garantir sustentação e, ao mesmo tempo, esta substrutura serve como ornamento ao edifício e como condicionador da entrada dos espectadores. Tal como foi referido anteriormente, possuía três pisos, sendo mais tarde adicionado um outro. É construído em mármore, pedra travertina, ladrilho e tufo (pedra calcária com grandes poros). A sua planta elíptica mede dois eixos que se estendem aproximadamente de 190 m por 155 m. A fachada compõe-se de arcadas decoradas com colunas dóricas, jónicas e coríntias, de acordo com o pavimento em que se encontravam. Esta subdivisão deve-se ao facto de ser uma construção essencialmente vertical, criando assim uma diversificação do espaço.

 

Os assentos eram em mármore e a cavea, escadaria ou arquibancada, dividia-se em três partes, correspondentes às diferentes classes sociais: o podium, para as classes altas; as maeniana, sector destinado à classe média; e os portici, ou pórticos, construídos em madeira, para a plebe e as mulheres. O pulvinar, a tribuna imperial, encontrava-se situada no podium e era balizada pelos assentos reservados aos senadores e magistrados. Rampas no interior do edifício facilitavam o acesso às várias zonas de onde podiam visualizar o espectáculo, sendo protegidos por uma barreira e por uma série de arqueiros posicionados numa passagem de madeira, para o caso de algum acidente. Por cima dos muros ainda são visíveis as mísulas, que sustentavam o velarium, enorme cobertura de lona destinada a proteger do sol os espectadores e, nos subterrâneos, ficavam as jaulas dos animais, bem como todas as celas e galerias necessárias aos serviços do anfiteatro.

O monumento permaneceu como sede principal dos espetáculos da urbe romana até ao período do imperador Honorius, no século V. Danificado por um terremoto no começo do mesmo século, foi alvo de uma extensiva restauração na época de Valentinianus III. Em meados do século XIII, a família Frangipani transformou-o em fortaleza e, ao longo dos séculos XV e XVI, foi por diversas vezes saqueado, perdendo grande parte dos materiais nobres com os quais tinha sido construído.

Os relatos romanos referem-se a cristãos sendo martirizados em locais de Roma descritos pouco pormenorizadamente (no anfiteatro, na arena...), quando Roma tinha numerosos anfiteatros e arenas. Apesar de muito provavelmente o Coliseu não ter sido utilizado para martírios, o Papa Bento XIV consagrou-o no século XVII à Paixão de Cristo e declarou-o lugar sagrado. Os trabalhos de consolidação e restauração parcial do monumento, já há muito em ruínas, foram feitos sobretudo pelos pontífices Gregório XVI e Pio IX, no século XIX.

Royal Air Force and French Air Force personnel treat a simulated casualty as part of Exercise Capable Eagle.

 

Royal Air Force medics have been responding after a simulated air attack on a North Yorkshire airfield.

 

RAF Leeming was playing the part of a foreign airbase being used by UK and French forces, as part of Exercise Capable Eagle, a test of the two countries’ ability to mount a combined air operation.

 

The exercise saw personnel planning, preparing for and flying missions, while facing a series of challenges.

 

One of those was an ‘attack’ by aircraft from 100 Squadron – itself normally based at RAF Leeming. 100 Squadron’s main role is to support training for all three services, including acting as an enemy when required. The simulated attack left a number of simulated casualties, giving the RAF’s healthcare experts a chance to test their skills.

 

While their colleagues are operating in Afghanistan daily, there is still a need for military medics to prepare for other possible operations. And Exercise Capable Eagle has given them the opportunity to do that.

-------------------------------------------------------

© Crown Copyright 2013

Photographer: SAC Mark Parkinson

Image 45156308.jpg from www.defenceimages.mod.uk

  

Use of this image is subject to the terms and conditions of the MoD News Licence at www.defenceimagery.mod.uk/fotoweb/20121001_Crown_copyrigh...

 

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From Mad Max Fury Road: One of Immortan Joe's five "wives".

Comikaze Expo, Saturday, October 31, 2015

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

  

Some background:

The Sondergerät SG104 "Münchhausen" was a German airborne recoillless 355.6 mm (14-inch) caliber gun, intended to engage even the roughest enemy battleships, primarily those of the Royal Navy. The design of this unusual and massive weapon began in 1939. The rationale behind it was that a battleship’s most vulnerable part was the deck – a flat surface, with relatively thin armor (as typical hits were expected on the flanks) and ideally with vital targets underneath, so that a single, good hit would cripple of even destroy a ship. The purpose of such a high angle of attack was likely to allow the projectile to penetrate the target ship's deck, where the ship's armor, if there was any, would have been much thinner than the armor on its sidesHowever, hitting the deck properly with another ship’s main gun was not easy, since it could only be affected through indirect hits and the typical angle of the attack from aballistic shot would not necessarily be ideal for deep penetration, esp. at long range.

The solution to this problem: ensure that the heavy projectile would hit its target directly from above, ideally at a very steep angle. To achieve this, the gun with battleship caliber was “relocated” from a carrier ship or a coastal battery onto an aircraft – specifically to a type that was capable of dive-bombing, a feature that almost any German bomber model of the time offered.

 

Firing such a heavy weapon caused a lot fo problems, which were severe even if the gun was mounted on a ship or on land. To compensate for such a large-caliber gun’s recoil and to make firing a 14 in shell (which alone weighed around almost 700 kg/1.550 lb, plus the charge) from a relatively light airframe feasible, the respective gun had to be as light as possible and avoid any recoil, which would easily tear an aircraft – even a bomber – apart upon firing. Therefore, the Gerät 104 was designed as a recoilless cannon. Its firing system involved venting the same amount of the weapon's propellant gas for its round to the rear of the launch tube (which was open at both ends), in the same fashion as a rocket launcher. This created a forward directed momentum which was nearly equal to the rearward momentum (recoil) imparted to the system by accelerating the projectile itself. The balance thus created did not leave much net momentum to be imparted to the weapon's mounting or the carrying airframe in the form of felt recoil. A further share of the recoil induced by the moving round itself could be compensated by a muzzle brake which re-directed a part of the firing gases backwards. Since recoil had been mostly negated, a heavy and complex recoil damping mechanism was not necessary – even though the weapon itself was huge and heavy.

 

Work on the "Münchhausen" device (a secret project handle after a fictional German nobleman created by the German writer Rudolf Erich Raspe in the late 18th century who reputedly had ridden on a cannonball between enemy frontlines), was done by Rheinmetall-Borsig and lasted until 1941. The first test of a prototype weapon was conducted on 9th of September 1940 in Unterlüss with a satisfactory result, even though the weapon was only mounted onto an open rack and not integrated into an airframe yet. At that time, potential carriers were the Ju 88, the Dornier Do 217 and the new Junkers Ju 288. Even though the system’s efficacy was doubted, the prospect of delivering a single, fatal blow to an important , armored arget superseded any doubts at the RLM, and the project was greenlit in early 1942 for the next stage: the integration of the Sondergerät 104 into an existing airframe. The Ju 88 and its successor, the Ju 188, turned out to be too light and lacked carrying capacity for the complete, loaded weapon, and the favored Ju 288 was never produced, so that only the Dornier Do 217 or the bigger He 177 remained as a suitable carriers. The Do 217 was eventually chosen because it had the biggest payload and the airframe was proven and readily available.

 

After calculations had verified that the designed 14 in rifle would have effectively no recoil, preliminary tests with dumm airframes were carried out. After ground trials with a Do 217 E day bomber to check recoil and blast effects on the airframe, the development and production of a limited Nullserie (pre-production series) of the dedicated Do 217 F variant for field tests and eventual operational use against British sea and land targets was ordered in April 1942.

 

The resulting Do 217 F-0 was based on the late “E” bomber variant and powered by a pair of BMW 801 radial engines. It was, however, heavily modified for its unique weapon and the highly specialized mission profile: upon arriving at the zone of operation at high altitude, the aircraft would initiate a dive with an angle of attack between 50° and 80° from the horizontal, firing the SG 104 at an altitude between 6,000 and 2,000 meters. The flight time of the projectile could range from 16.0 seconds for a shot from an altitude of 6,000 meters at a 50° angle to just 4.4 seconds for a shot from 2.000 meters at an almost vertical 80° angle. Muzzle velocity of the SG 104 was only 300 m/s, but, prior to impact, the effective velocity of the projectile was projected to range between 449 and 468 m/s (1,616 to 1,674 km/h). Together with the round's weight of roughly 700 kg (1.550 lb) and a hardened tip, this would still ensure a high penetration potential.

 

The operational Sondergerät 104 had an empty mass of 2.780 kg (6,123 lb) and its complete 14 inch double cartridge weighed around 1.600 kg (3,525 lb). The loaded mass of the weapon was 4,237 kg, stretching the limits of the Do 217’s load capacity to the maximum, so that some armor and less vital pieces of equipment were deleted. Crew and defensive armament were reduced to a minimum.

Even though there had been plans to integrate the wepaon into the airframe (on the Ju 288), the Gerät 104 was on the Do 217 F-0 mounted externally and occupied the whole space under the aircraft, precluding any use of the bomb bay. The latter was occupied by the Gerät 104’s complex mount, which extended to the outside under a streamlined fairing and held the weapon at a distance from the airframe. Between the mount’s struts inside of the fuselage, an additional fuel tank for balance reasons was added, too.

The gun’s center, where the heavy round was carried, was positioned under the aircraft’s center of gravity, so that the gun barrel markedly protruded from under the aircraft’s nose. To make enough space, the Do 217 Es bomb aimer’s ventral gondola and his rearward-facing defensive position under the cockpit were omitted and faired over. The nose section was also totally different: the original extensive glazing (the so-called “Kampfkopf”) was replaced by a smaller, conventional canopy, similar to the later Do 217 J and N night fighter versions, together with a solid nose - the original glass panels would have easily shattered upon firing the gun, esp. in a steep high-speed dive. A "Lotfernrohr" bomb aiming device was still installed in a streamlined and protected fairing, though, so that the navigator could guide the pilot during the approach to the target and during the attack run.

To stabilize the heavy aircraft during its attack and to time- and safely pull out of the dive, a massive mechanical dive brake was mounted at the extended tail tip, which unfolded with four "petals". A charecteristic stabilizing dorsal strake was added between the twin fins, too.

 

The ventral area behind the gun’s rear-facing muzzle received additional metal plating and blast guiding vanes, after trials in late 1940 had revealed that firing the SG 104 could easily damage the Do 217’s tail structure, esp. all of the tail surfaces’ rudders and the fins’ lower ends in particular. Due to all this extra weight, the Do 217 F-0’s defensive armament consisted only of a single 13 mm MG 131 machine gun in a manually operated dorsal position behind the cockpit cabin, which offered space for a crew of three. A fixed 15 mm MG 151 autocannon was mounted in the nose, too, a weapon with a long barrel for extended range and accuracy. It was not an offensive weapon, though, rather intended as an aiming aid for the SG 104 because it was loaded with tracer bullets: during the final phase of the attack dive, the pilot kept firing the MG 151, and the bullet trail showed if he was on target to fire the SG 104 when the right altitude/range had been reached.

 

The first Do 217 F-0 was flown and tested in late 1943, and after some detail changes the type was cleared for a limited production run of ten aircraft in January 1944. The first operational machine was delivered to a dedicated testing commando, the Erprobungskommando 104 “Münchhausen”, also known as “Sonderkommando Münchhausen” or simply “E-Staffel 104”. The unit was based at Bordeaux/Merignac and directly attached to the KG 40's as a staff flight. At that time, KG 40 operated Do 217 and He 177 bombers and frequently flew reconnaissance and anti-shipping missions over the Atlantic west of France, up to the British west and southern coast, equipped with experimental Henschel Hs 293 glide bombs.

 

Initial flights confirmed that the Do 217 airframe was burdened with the SG 104 to its limits, the already rather sluggish aircraft (the Do 217 had generally a high wing loading and was not easy to fly) lost anything that was left of what could be called agility. It needed an experienced pilot to handle it safely, esp. during start and landing. It is no wonder that two Do 217 F-0s suffered ground accidents during the first two weeks of operations, but the machines could be repaired, resume the test program and carry out attack missions.

However, during one of the first test shots with the weapon, one Do 217 F-0 lost its complete tail section though the gun blast, and the aircraft crashed into the Bay of Biscay, killing the complete crew.

 

On 4th or April 1944 the first "hot" attack against an enemy ship was executed in the Celtic Sea off of Brest, against a convoy of 20 ships homeward bound from Gibraltar. The attack was not successful, though, the shot missing its target, and the German bomber was attacked and heavily damaged by British Bristol Beaufighters that had been deployed to protect the ships. The Do 217F-0 eventually crashed and sank into the Atlantic before it could reach land again.

 

A couple of days later, on 10th of April, the first attempt to attack and destroy a land target was undertaken: two Do 217 F-0s took off to attack Bouldnor Battery, an armored British artillery position located on the Isle of Wight. One machine had to abort the attack due to oil leakages, the second Do 217 F-0 eventually reached its target and made a shallow attack run, but heavy fog obscured the location and the otherwise successful shot missed the fortification. Upon return to its home base the aircraft was intercepted by RAF fighters over the Channel and heavily damaged, even though German fighters deployed from France came to the rescue, fought the British attackers off and escorted the limping Do 217 F-0 back to its home base.

 

These events revealed that the overall SG 104 concept was generally feasible, but also showed that the Do 217 F-0 was very vulnerable without air superiority or a suitable escort, so that new tactics had to be developed. One consequence was that further Do 217 F-0 deployments were now supported by V/KG 40, the Luftwaffe's only long range maritime fighter unit. These escorts consisted of Junkers Ju 88C-6s, which were capable of keeping up with the Do 217 F-0 and fend of intercepting RAF Coastal Command’s Beaufighters and later also Mosquitos.

 

In the meantime, tests with the SG 104 progressed and several modifications were tested on different EKdo 104's Do 217 F-0s. One major upgrade was a further strengthening of the tail section, which added another 200 kg (440 lb) to the aircraft's dry weight. Furthermore, at least three aircraft were outfitted with additional dive brakes under the outer wings, so that the dive could be better controlled and intercepted. these aircraft, however, lost their plumbed underwing hardpoints, but these were only ever used for drop tanks during transfer flights - a loaded SG 104 precluded any other ordnance. On two other aircraft the SG 104 was modified to test different muzzle brakes and deflectors for the rear-facing opening, so that the gun blast was more effectively guided away from the airframe to prevent instability and structural damage. For instance, one machine was equipped with a bifurcated blast deflector that directed the rearward gasses partly sideways, away from the fuselage.

 

These tests did not last long, though. During the Allied Normandy landings in June 1944 E-Staffel 104 was hastily thrown into action and made several poorly-prepared attack runs against Allied support ships. The biggest success was a full hit and the resulting sinking of the Norwegian destroyer HNoMS Svenner (G03) by "1A+BA" at dawn on 6th of June, off Sword, one of the Allied landing zones. Other targets were engaged, too, but only with little effect. This involvement, however, led to the loss of three Do 217 F-0s within just two days and four more heavily damaged aircraft – leaving only two of EKdo 104's Do 217 F-0s operational.

 

With the Allied invasion of France and a worsening war condition, the SG 104 program was stopped in August 1944 and the idea of an airborne anti-ship gun axed in favor of more flexible guided weapons like the Hs 293 missile and the Fritz-X glide bomb. Plans for a further developed weapon with a three-round drum magazine were immediately stopped, also because there was no carrier aircraft in sight that could carry and deploy this complex 6.5 tons weapon. However, work on the SG 104 and the experience gained from EKdo 104's field tests were not in vain. The knowledge gathered from the Münchhausen program was directly used for the design of a wide range of other, smaller recoilless aircraft weapons, including the magnetically-triggered SG 113 "Förstersonde" anti-tank weapon or the lightweight SG 118 "Rohrblock" unguided air-to-air missile battery for the Heinkel He 162 "Volksjäger".

  

General characteristics:

Crew: 3 (pilot, navigator, radio operator/gunner)

Length: 20,73 m (67 ft 11 in) overall

18,93 m (62 ft 3/4 in) hull only

Wingspan: 19 m (62 ft 4 in)

Height: 4.97 m (16 ft 4 in)

Wing area: 57 m² (610 sq ft)

Empty weight: 9,065 kg (19,985 lb)

Empty equipped weight:10,950 kg (24,140 lb)

Max takeoff weight: 16,700 kg (36,817 lb)

Fuel capacity: 2,960 l (780 US gal; 650 imp gal) in fuselage tank and four wing tanks

 

Powerplant:

2× BMW 801D-2 14-cylinder air-cooled radial piston engines, delivering

1,300 kW (1,700 hp) each for take-off and 1,070 kW (1,440 hp) at 5,700 m (18,700 ft),

driving 3-bladed VDM constant-speed propellers

 

Performance:

Maximum speed: 475 km/h (295 mph, 256 kn) at sea level

560 km/h (350 mph; 300 kn) at 5,700 m (18,700 ft)

Cruise speed: 400 km/h (250 mph, 220 kn) with loaded Gerät 104 at optimum altitude

Range: 2,180 km (1,350 mi, 1,180 nmi) with maximum internal fuel

Ferry range: 2,500 km (1,600 mi, 1,300 nmi); unarmed, with auxiliary fuel tanks

Service ceiling: 7,370 m (24,180 ft) with loaded Gerät 104,

9,500 m (31,200 ft) after firing

Rate of climb: 3.5 m/s (690 ft/min)

Time to altitude: 1,000 m (3,300 ft) in 4 minutes 10 seconds

2,000 m (6,600 ft) in 8 minutes 20 seconds

6,100 m (20,000 ft) in 24 minutes 40 seconds

 

Armament:

1x 355.6 mm (14-inch) Sondergerät 104 recoilless gun with a single round in ventral position

1x 15 mm (0.787 in) MG 151 machine cannon with 200 rounds, fixed in the nose

1x 13 mm (0.512 in) MG 131 machine gun with 500 rounds, movable in dorsal position

Two underwing hardpoints for a 900 l drop tank each, but only used during unarmed ferry flights

  

The kit and its assembly:

This was another submission to the "Gunships" group build at whatifmodellers.com in late 2021, and inspiration struck when I realized that I had two Italeri Do 217 in The Stash - a bomber and a night fighter - that could be combined into a suitable (fictional) carrier for a Sondergerät 104. This mighty weapon actually existed and even reached the hardware/test stage - but it was never integrated into an airframe and tested in flight. But that's what this model is supposed to depict.

 

On the Do 217, the Sg 104 would have been carried externally under the fuselage, even though there had been plans to integrate this recoilless rifle into airframes, esp. into the Ju 288. Since the latter never made it into production, the Do 217 would have been the most logical alternative, also because it had the highest payload of all German bombers during WWII and probably the only aircraft capable of carrying and deploying the Münchhausen device, as the SG 104 was also known.

 

The fictional Do 217 F-0 is a kitbashing, using a Do 217 N fuselage, combined with the wings from a Do 217 K bomber, plus some modifications. What initially sounded like a simple plan soon turned into a improvisation mess: it took some time to realize that I had already donated the Do 217 K's BMW 801 engines to another project, an upgraded He 115... I did not want to use the nightfighter's more powerful DB 603s, and I was lucky to have an Italeri Ju 188 kit at hand which comes with optional BMW 801s and Jumo 211s. Transplanting these engines onto the Do 217's wings took some tailoring of the adapter plates, but was feasible. However, the BMW 801s from the Ju 188 kit have a flaw: they lack the engine's characteristic cooling fans... Another lucky find: I found two such parts in the scrap box, even though from different kits - one left over from another Italeri Do 217 K, the other one from what I assume is/was an Italeri 1:72 Fw 190 A/F. To make matters worse, one propeller from the Ju 188 kit was missing, so that I had to find a(nother) replacement. :-/

I eventually used something that looked like an 1:72 F6F Hellcat propeller, but I an not certain about this because I have never built this model...? With some trimming on the blades' trailing edges and other mods, the donor's overall look could be adapted to the Ju 188 benchmark. Both propellers were mounted on metal axis' so that they could also carry the cooling fans. Lots of work, but the result looks quite good.

 

The Do 217 N's hull lost the lower rear gunner position and its ventral gondola, which was faired over with a piece of styrene sheet. The pilot was taken OOB, the gunner in the rear position was replaced by a more blob-like crew member from the scrap box. The plan to add a navigator in the seat to the lower right of the pilot did not work out due to space shortage, but this figure would probably have been invisble, anyway.

All gun openings in the nose were filled and PSRed away, and a fairing for a bomb aiming device and a single gun (the barrel is a hollow steel needle) were added.

 

The SG 104 was scratched. Starting point was a white metal replacement barrel for an 1:35 ISU-152 SPG with a brass muzzle brake. However, after dry-fitting the barrel under the hull the barrel turned out to be much too wide, so that only the muzzal brake survived and the rest of the weapon was created from a buddy refueling pod (from an Italeri 1:72 Luftwaffe Tornado, because of its two conical ends) and protective plastic caps from medical canulas. To attach this creation to the hull I abused a conformal belly tank from a Matchbox Gloster Meteor night fighter and tailored it into a streamlined fairing. While this quite a Frankenstein creation, the overall dimensions match the real SG 104 prototype and its look well.

 

Other cosmetic modifications include a pair of underwing dive brakes, translanted from an Italeri 1:72 Ju 88 A-4 kit, an extended (scratched) tail "stinger" which resembles the real dive brake arrangement that was installed on some Do 217 E bombers, and I added blast deflector vanes and a dorsal stabilizer fin.

In order to provide the aircraft with enough ground clearance, the tail wheel was slightly extended. Thanks to the long tail stinger, this is not blatantly obvious.

  

Painting and markings:

This was not an easy choice, but as a kind of prototype I decided that the paint scheme should be rather conservative. However, German aircraft operating over the Atlantic tended to carry rather pale schemes, so that the standard pattern of RLM 70/71/65 (Dunkelgrün, Schwarzgrün and Hellblau) with a low waterline - typical for experimental types - would hardly be appropriate.

I eventually found a compromise on a He 177 bomber (coded 6N+BN) from 1944 that was operated by KG 100: this particular aircraft had a lightened upper camouflage - still a standard splinter scheme but consisting of RLM 71 and 02 (Dunkelgrün and Grau; I used Modelmaster 2081 and Humbrol 240), a combination that had been used on German fighters during the Battle of Britain when the standard colors turned out to be too dark for operations over the Channel. The aircraft also carried standard RLM 65 (or maybe the new RLM76) underneath (Humbrol 65) and on the fin, but with a very high and slightly wavy waterline. As a rather unusual feature, no typical camouflage mottles were carried on the flanks or the fin, giving the aircraft a very bleak and simple look.

 

Despite my fears that this might look rather boring I adapted this scheme for the Do 217 F-0, and once basic painting was completed I was rather pleased by the aircraft's look! As an aircraft operated at the Western front, no additional markings like fuselage bands were carried.

To set the SG 104 apart from the airframe, I painted the weapon's visible parts in RLM 66 (Schwarzgrau, Humbrol 67), because this tone was frequently used for machinery (including the interior surfaces of aircraft towards 1945).

RLM 02 was also used for the interior surfaces and the landing gear, even though I used a slightly different, lighter shade in form of Revell 45 (Helloliv).

 

A light black ink washing was applied and post-shading to emphasize panel lines. Most markings/decals came from a Begemot 1:72 He 11 sheet, including the unusual green tactical code - it belongs to a staff unit, a suitable marking for such an experimental aircraft. The green (Humbrol 2) was carried over to the tips of the propeller spinners. The unit's code "1A" is fictional, AFAIK this combination had never been used by the Luftwaffe.

The small unit badge was alucky find: it actually depicts the fictional Baron von Münchhausen riding on a cannonball, and it comes from an Academy 1:72 Me 163 kit and its respective sheet. The mission markings underneath, depicting two anti-ship missions plus a successful sinking, came from a TL Modellbau 1:72 scale sheet with generic German WWII victory markings.

 

After some soot stains around the engine exhaust and weapon muzzles had been added with graphite, the model was sealed with matt acrylic varnish and final details like position lights and wire antennae (from heated black plastic sprue material) were added.

  

Well, what started as a combination of two kits of the same kind with a simple huge pipe underneath turned out to be more demanding than expected. The (incomplete) replacement engines were quite a challenge, and body work on the hull (tail stinger, fairing for the SG 104 as well as the weapon itself) turned out to be more complex and extensive than initially thought of. The result looks quite convincing, also supported by the rather simple paint scheme which IMHO just "looks right" and very convincing. And the whole thing is probably the most direct representation of the inspiring "Gunship" theme!

 

Whilst 67023 and 67027 were away on RHTT duties the once a month visit to Sheffield Midland on the 1Q50 1340 Derby RTC - Doncaster Wood Yard was covered by 37521 which had lead into Midland and 37116 which will lead out after a reversal..

 

15 11 18

Speeding north through Lichfield Trent Valley with the 1Z53 Willesden Railnet to Shieldmuir Mail Terminal is Royal Mail Class 325, 325009.

 

The Class 325's are yet another one of those Greek tragedies of the British railway scene. These specially built, 100mph units were very capable machines, but sadly the powers that be quickly pulled the rug out from under them, and what would have been the primary motive power for mail traffic across the UK's electric railway network is now only just starting to make a comeback.

 

The origins of the Class 325 go back to the early 1990's. At the time British Rail's parcels and mail arm, Rail Express Systems, was in the process of phasing out the traditional Travelling Post Office as computer sorting removed the need for sorting by-hand aboard the trains. At the same time RES desired a fleet of units that would be much more flexible, efficient and cost effective than the ageing fleet of Class 86 electrics, Class 47 diesels and MkI based coaching stock of the 1960's that it was using presently.

 

Previously, Royal Mail had trialed reusing former London commuter EMU's and re-purposing them as parcels units. Initially, Class 307's built in the 1950's were used on services out of London Liverpool Street, these being designated Class 300. However, these units weren't particularly reliable, and their age meant that they were only a few years away from being life-expired. In 1994, Rail Express Systems placed an order for a set of 100mph electric multiple units to be built on the underpinnings of the Class 319 dual-voltage Thameslink units used in London. Originally, this class was designated Class 350, but was eventually changed to Class 325.

 

Construction of these units was done by ABB at their Derby works between 1995 and 1996, with 16 of these trains eventually built. The construction of the Class 325's coincided with a major refurbishment of the mail-on-rail system, with new distribution centres and sorting offices constructed at major railway locations, this project being dubbed Railnet. For the Class 325's, these included Railnet terminals at Shieldmuir near Glasgow (to serve the lowlands of Scotland), Warrington (to serve North West England), Low Fell near Newcastle, and Willesden in North London. Additional Railnet terminals off the Class 325's network included Tonbridge, Bristol Parkway, Doncaster and Stafford. Willesden Railnet terminal is by far the largest, a 7 platform station under a huge barrel roof which is essentially another London terminus just with no passengers, built at a cost of £30m.

 

The Class 325's eventually began operations after a short period of trials in 1995. The units are fitted with large round oleo buffers, and have no gangways between carriages. Each set is made up of four cars, with roller doors in place of sliding ones and no windows. Each car has two roller shutter sliding doors on each side and is designed to hold up to 12 tonnes. They have a pantograph to pick up power from the 25 kV AC overhead lines, and also a shoe to pick up power off the 750 V DC third rail. They cannot work in multiple with any other multiple unit stock, but are fitted with drop-head buck-eye coupling and can therefore be hauled by locomotives. The units were built in such a way that they could easily be converted for passenger use if no longer required for mail services, and cab fronts designed to look similar to the then recently built Networker Class 165/166 and 365/465 commuter units.

 

Based at Crewe International Electric Maintenance Depot, the Class 325's effects on the mail services up the West and East Coast Mainlines were profound, with turnaround times and flexibility when it came to shunting being among its many advantages. They were also much more reliable than Class 86's or 47's, and could easily be put to work on the 3rd Rail Southern Region without the need for diesels or locomotive changes.

 

However, their tenure on mail services was seriously short lived, as in 2003, Royal Mail decided to cease the Mail Train contract with freight operator EWS after 166 years of operation. The last mail services under the original Victorian contract ended on January 9th, 2004, and the Class 325's, along with the hundreds of carriages of stock and locomotives, entered storage at various locations across the network, while the millions of pounds of infrastructure and the Railnet buildings fell silent after less than 10 years of operation.

 

The Class 325's were thankfully not out of action for long though, as at Christmas 2004, in light of heavy demand and congestion on the roads in bad weather, Royal Mail reluctantly awarded GBRf the contract to run a limited number of Class 325's on services between London and Glasgow over the winter period. GBRf however were not cleared to use the Class 325's on their own, and thus instead chose to drag the units using Class 86's and 87's. After a traction reshuffle the Class 325s resumed service with their power cars and without locomotive haulage.

 

Eventually, GBRf lost the contract in 2010 to EWS's successor, DB Schenker, who now operate both Royal Mail services but the continued maintenance of the Class 325 stock. On an average weekday there are 15 diagrammed services out of Willesden Railnet, 5 to and from Warrington, 3 to Shieldmuir and 3 to Low Fell. Today, 15 out of the original 16 units remain in service, 325010 being scrapped in 2012 after years of neglect in storage.

 

Sadly, like many pieces of the Mail Train puzzle, so many were wasted after less than 10 years of operation, infrastructure built to last for 100 years demolished after no time at all. At least the Class 325's have found their way back into work, doing a job that makes eminent sense over the road haulage alternative Royal Mail hoped would be the better option over the mail train. Instead the Class 325's are proof as to why mail-by-rail is the superior option, no traffic jams, no slippery roads, no 60mph speed limiter on the lorries, just 100mph haulage of your valuables and parcels up and down the country all the way!

Some background:

The VF-1 was developed by Stonewell/Bellcom/Shinnakasu for the U.N. Spacy by using alien Overtechnology obtained from the SDF-1 Macross alien spaceship. Its production was preceded by an aerodynamic proving version of its airframe, the VF-X. Unlike all later VF vehicles, the VF-X was strictly a jet aircraft, built to demonstrate that a jet fighter with the features necessary to convert to Battroid mode was aerodynamically feasible. After the VF-X's testing was finished, an advanced concept atmospheric-only prototype, the VF-0 Phoenix, was flight-tested from 2005 to 2007 and briefly served as an active-duty fighter from 2007 to the VF-1's rollout in late 2008, while the bugs were being worked out of the full-up VF-1 prototype (VF-X-1).

 

The space-capable VF-1's combat debut was on February 7, 2009, during the Battle of South Ataria Island - the first battle of Space War I - and remained the mainstay fighter of the U.N. Spacy for the entire conflict. Introduced in 2008, the VF-1 would be out of frontline service just five years later, though.

 

The VF-1 proved to be an extremely capable craft, successfully combating a variety of Zentraedi mecha even in most sorties which saw UN Spacy forces significantly outnumbered. The versatility of the Valkyrie design enabled the variable fighter to act as both large-scale infantry and as air/space superiority fighter. The signature skills of U.N. Spacy ace pilot Maximilian Jenius exemplified the effectiveness of the variable systems as he near-constantly transformed the Valkyrie in battle to seize advantages of each mode as combat conditions changed from moment to moment.

 

The basic VF-1 was deployed in four minor variants (designated A, D, J, and S) and its success was increased by continued development of various enhancements including the GBP-1S "Armored" Valkyrie, FAST Pack "Super" Valkyrie and the additional RÖ-X2 heavy cannon pack weapon system for the VF-1S for additional firepower.

The FAST Pack system was designed to enhance the VF-1 Valkyrie variable fighter, and the initial V1.0 came in the form of conformal pallets that could be attached to the fighter’s leg flanks for additional fuel – primarily for Long Range Interdiction tasks in atmospheric environment. Later FAST Packs were designed for space operations.

 

After the end of Space War I, the VF-1 continued to be manufactured both in the Sol system and throughout the UNG space colonies. Although the VF-1 would be replaced in 2020 as the primary Variable Fighter of the U.N. Spacy by the more capable, but also much bigger, VF-4 Lightning III, a long service record and continued production after the war proved the lasting worth of the design.

The versatile aircraft also underwent constant upgrade programs. For instance, about a third of all VF-1 Valkyries were upgraded with Infrared Search and Track (IRST) systems from 2016 onwards, placed in a streamlined fairing on the upper side of the nose, just in front of the cockpit. This system allowed for long-range search and track modes, freeing the pilot from the need to give away his position with active radar emissions, and it could also be used for target illumination and guiding precision weapons.

Many Valkyries also received improved radar warning systems, with receivers, depending on the systems, mounted on the wing-tips, on the fins and/or on the LERXs. Improved ECR measures were also mounted on some machines, typically in conformal fairings on the flanks of the legs/engine pods.

 

After joining the global U.N. Spacy union, Germany adopted the VF-1 in late 2008, it replaced the Eurofighter Typhoon interceptors as well as Tornado IDS and ECR fighter bombers. An initial delivery of 120 aircraft was completed until 2011, partially delayed by the outbreak of Space War One in 2009. This initial batch included 85 VF-1A single seaters, fourteen VF-1J fighters for commanders and staff leaders, and twenty VF-1D two-seaters for conversion training over Germany (even though initial Valkyrie training took place at Ataria Island). These machines were erratically registered under the tactical codes 26+01 to 26+99. Additionally, there was a single VF-1S (27+00) as a personal mount for the General der Luftwaffe.

 

The German single-seaters were delivered as multi-role fighters that could operate as interceptors/air superiority fighters as well as attack aircraft. Beyond the standard equipment they also carried a passive IRST sensor in front of the cockpit that allowed target acquisition without emitting radar impulses, a LRMTS (Laser Rangefinder and Marked Target Sensor) under the nose, a Weapon Delivery and Navigation System (WDNS) and an extended suite of radar warning sensors and ECM jammers.

After Space War I, attritions were replaced with a second batch of VF-1 single seaters in 2015, called VF-1L (for “Luftwaffe”). These machines had updated avionics and, among modifications, a laser target designator in a small external pod under the cockpit. About forty VF-1 survivors from the first batch were upgraded to this standard, too, and the VF-1Ls were registered under the codes 27+01 – 90.

 

The VF-1 was without doubt the most recognizable variable fighter of Space War I and was seen as a vibrant symbol of the U.N. Spacy even into the first year of the New Era 0001 in 2013. At the end of 2015 the final rollout of the VF-1 was celebrated at a special ceremony, commemorating this most famous of variable fighters. The VF-1 Valkryie was built from 2006 to 2013 with a total production of 5,459 VF-1 variable fighters with several variants (VF-1A = 5,093, VF-1D = 85, VF-1J = 49, VF-1S = 30, VF-1G = 12, VE-1 = 122, VT-1 = 68)

 

However, the fighter remained active in many second line units and continued to show its worthiness years later, e. g. through Milia Jenius who would use her old VF-1 fighter in defense of the colonization fleet - 35 years after the type's service introduction!

 

General characteristics:

All-environment variable fighter and tactical combat Battroid,

used by U.N. Spacy, U.N. Navy, U.N. Space Air Force

 

Accommodation:

Pilot only in Marty & Beck Mk-7 zero/zero ejection seat

 

Dimensions:

Fighter Mode:

Length 14.23 meters

Wingspan 14.78 meters (at 20° minimum sweep)

Height 3.84 meters

 

Battroid Mode:

Height 12.68 meters

Width 7.3 meters

Length 4.0 meters

 

Empty weight: 13.25 metric tons;

Standard T-O mass: 18.5 metric tons;

MTOW: 37.0 metric tons

 

Power Plant:

2x Shinnakasu Heavy Industry/P&W/Roice FF-2001 thermonuclear reaction turbine engines, output 650 MW each, rated at 11,500 kg in standard or in overboost (225.63 kN x 2)

4x Shinnakasu Heavy Industry NBS-1 high-thrust vernier thrusters (1 x counter reverse vernier thruster nozzle mounted on the side of each leg nacelle/air intake, 1 x wing thruster roll control system on each wingtip);

18x P&W LHP04 low-thrust vernier thrusters beneath multipurpose hook/handles

 

Performance:

Battroid Mode: maximum walking speed 160 km/h

Fighter Mode: at 10,000 m Mach 2.71; at 30,000+ m Mach 3.87

g limit: in space +7

Thrust-to-weight ratio: empty 3.47; standard T-O 2.49; maximum T-O 1.24

 

Design Features:

3-mode variable transformation; variable geometry wing; vertical take-off and landing; control-configurable vehicle; single-axis thrust vectoring; three "magic hand" manipulators for maintenance use; retractable canopy shield for Battroid mode and atmospheric reentry; option of GBP-1S system, atmospheric-escape booster, or FAST Pack system

 

Transformation:

Standard time from Fighter to Battroid (automated): under 5 sec.

Min. time from Fighter to Battroid (manual): 0.9 sec.

 

Armament:

2x internal Mauler RÖV-20 anti-aircraft laser cannon, firing 6,000 pulses per minute

1x Howard GU-11 55 mm three-barrel Gatling gun pod with 200 RPG, fired at 1,200 rds/min

4x underwing hard points for a wide variety of ordnance, including

12x AMM-1 hybrid guided multipurpose missiles (3/point), or

12x MK-82 LDGB conventional bombs (3/point), or

6x RMS-1 large anti-ship reaction missiles (2/outboard point, 1/inboard point), or

4x UUM-7 micro-missile pods (1/point) each carrying 15 x Bifors HMM-01 micro-missiles,

or a combination of above load-outs

  

The kit and its assembly:

This fictional VF-1 is more or less “only” a camouflage experiment, spawned by a recent discussion about the German Luftwaffe’s so-called “Norm ‘81” paint scheme that was carried by the F-4Fs during the Eighties and the early Nineties. It is one of the most complex standardized paint scheme I am aware of, consisting of no less than six basic shades of grey and applied in two different patterns (early variant with angled/splinter camouflage, later this was changed into more organic shapes).

 

I have built a fictional post-GDR MiG-21 with the Norm ’81 scheme some years ago, but had always been curious how a Macross VF-1 would look with it, or how it could be adapted to the F-14esque airframe?

 

Concerning the model, it’s another vintage ARII VF-1, in this case a VF-1J, built OOB and with the landing gear down and an open canopy. However, I added some small details like the sensors in front of the cockpit, RHAWS sensors and bulges for ECM equipment on the lower legs (all canonical). The ordnance was subtly changed, with just two AMM-1 missiles on each outer pylon plus small ECM pods on the lo hardpoint (procured from an 1:144 Tornado). The inner stations were modified to hold quadruple starters for (fictional) air-to-ground missiles, left over from a Zvezda 1:72 Ka-58 helicopter and probably depicting Soviet/Russian 9M119 “Svir” laser-guided anti-tank missiles, or at least something similar. At the model’s 1:100 scale they are large enough to represent domestic alternatives to AGM-65 Maverick missiles – suitable against Zentraedi pods and other large ground targets. The ventral GU-11 pod was modified to hold a scratched wire display for in-flight pictures. Some blade antennae were added as a standard measure to improve the simple kit’s look. The cockpit was taken OOB, I just added a pilot figure for the scenic shots and the thick canopy was later mounted on a small lift arm in open position.

 

Painting and markings:

This was quite a challenge: adapting the Norm’ 81 scheme to the swing-wing Valkyrie, with its folded legs and the twin tail as well as lacking the Phantom’s spine and bulged air intakes, was not easy, and I went for the most straightforward solution and simplified things on the VF-1’s short spine.

 

The Norm ‘81’s “official” colors are all RAL tones, and I decided to use these for an authentic lokk, namely:

RAL 7009 Grüngrau: Revell 67 (acrylic)

RAL 7012 Basaltgrau: Revell 77 (acrylic)

RAL 7039 Quarzgrau: Xtracolor X259 (enamel)

RAL 7037 Staubgrau: Xtracolor X258 (enamel)

RAL 7030 Steingrau: Revell 75 (enamel)

RAL 7035 Lichtgrau: Humbrol 196 (enamel)

 

This basically plan worked and left me with a very murky aircraft: Norm ’81 turned out to be a kind of all-propose camouflage that works well against both sky and ground, at least in the typical German climate, and especially good at medium to low altitude. RAL 7030, 7037 and 7039 appear like gradually darker shades of the basically same brownish grey hue, framed with darker contrast areas that appear either greenish or bluish.

 

However, the Xtracolor enamels turned out to be total sh!t: they lacked pigments in the glossy and translucent base and therefore ANY opacity, esp. on any edge, at least when you use a brush like me. Not certain if using an airbrush improves this? The result were uneven and rather thick areas of paint, not what I had hoped for. And the Revell 75 just did what I hate about the company's enamels: drying up prematurely with a gooey consistency, leaving visible streaks.

 

After a black ink wash, very light post-shading was added. I should have from the start tried to stick to the acrylics and also mix the Xtracolor tones from Revell acrylics, a stunt that turned during the weathering process (trying to hide the many blemishes) out to be quite feasible. RAL 7037 was mixed from Revell 47 plus 89 in a ~1:1 ratio, and RAL 7039 from Revell 47, 77 and 87 with a touch of 09. Nevertheless, the paint finish turned out sub-optimal, but some shading and weathering saved most of the mess – even I am not satisfied with the outcome, the model looks more weathered than intended (even though most operational German F-4Fs with this paint scheme looked quite shaggy and worn, making the different shades of grey almost undiscernible).

 

After some consideration I gave this German VF-1 full-color (yet small) "Kite" roundels, together with a German tactical code. German flags and a vintage JaboG 32 squadron badge decorate the fin - a plausible move, because there are British Valkyries in source books that carry RAF fin flashes. Stencils and other markings came from VF-1 OOB sheets.

Finally, after some typical highlights with clear paint over a silver base were added, and the small VF-1 was sealed with a coat of matt acrylic varnish.

  

A spontaneous interim project, with interesting results. The adapted Norm ’81 scheme works well on the VF-1, and it even is a contemporary design from the era when the original TV series was conceived and aired. With the authentic tones I’d call it quite ugly – even though I was amazed during the photo session how well the different shades of grey (four from above!) blend into each other and break up the aircraft’s outlines. If there were no red-and-white roundels or the orange pilot in the cockpit (chosen intentionally for some color contrast), the camouflage would be very effective! Not perfect, but another special member in my growing VF-1 model fleet. ^^

 

Speeding south through Lichfield Trent Valley with the 1Z56 Warrington Railnet to Willesden Railnet is Royal Mail Class 325, 325009.

 

The Class 325's are yet another one of those Greek tragedies of the British railway scene. These specially built, 100mph units were very capable machines, but sadly the powers that be quickly pulled the rug out from under them, and what would have been the primary motive power for mail traffic across the UK's electric railway network is now only just starting to make a comeback.

 

The origins of the Class 325 go back to the early 1990's. At the time British Rail's parcels and mail arm, Rail Express Systems, was in the process of phasing out the traditional Travelling Post Office as computer sorting removed the need for sorting by-hand aboard the trains. At the same time RES desired a fleet of units that would be much more flexible, efficient and cost effective than the ageing fleet of Class 86 electrics, Class 47 diesels and MkI based coaching stock of the 1960's that it was using presently.

 

Previously, Royal Mail had trialed reusing former London commuter EMU's and re-purposing them as parcels units. Initially, Class 307's built in the 1950's were used on services out of London Liverpool Street, these being designated Class 300. However, these units weren't particularly reliable, and their age meant that they were only a few years away from being life-expired. In 1994, Rail Express Systems placed an order for a set of 100mph electric multiple units to be built on the underpinnings of the Class 319 dual-voltage Thameslink units used in London. Originally, this class was designated Class 350, but was eventually changed to Class 325.

 

Construction of these units was done by ABB at their Derby works between 1995 and 1996, with 16 of these trains eventually built. The construction of the Class 325's coincided with a major refurbishment of the mail-on-rail system, with new distribution centres and sorting offices constructed at major railway locations, this project being dubbed Railnet. For the Class 325's, these included Railnet terminals at Shieldmuir near Glasgow (to serve the lowlands of Scotland), Warrington (to serve North West England), Low Fell near Newcastle, and Willesden in North London. Additional Railnet terminals off the Class 325's network included Tonbridge, Bristol Parkway, Doncaster and Stafford. Willesden Railnet terminal is by far the largest, a 7 platform station under a huge barrel roof which is essentially another London terminus just with no passengers, built at a cost of £30m.

 

The Class 325's eventually began operations after a short period of trials in 1995. The units are fitted with large round oleo buffers, and have no gangways between carriages. Each set is made up of four cars, with roller doors in place of sliding ones and no windows. Each car has two roller shutter sliding doors on each side and is designed to hold up to 12 tonnes. They have a pantograph to pick up power from the 25 kV AC overhead lines, and also a shoe to pick up power off the 750 V DC third rail. They cannot work in multiple with any other multiple unit stock, but are fitted with drop-head buck-eye coupling and can therefore be hauled by locomotives. The units were built in such a way that they could easily be converted for passenger use if no longer required for mail services, and cab fronts designed to look similar to the then recently built Networker Class 165/166 and 365/465 commuter units.

 

Based at Crewe International Electric Maintenance Depot, the Class 325's effects on the mail services up the West and East Coast Mainlines were profound, with turnaround times and flexibility when it came to shunting being among its many advantages. They were also much more reliable than Class 86's or 47's, and could easily be put to work on the 3rd Rail Southern Region without the need for diesels or locomotive changes.

 

However, their tenure on mail services was seriously short lived, as in 2003, Royal Mail decided to cease the Mail Train contract with freight operator EWS after 166 years of operation. The last mail services under the original Victorian contract ended on January 9th, 2004, and the Class 325's, along with the hundreds of carriages of stock and locomotives, entered storage at various locations across the network, while the millions of pounds of infrastructure and the Railnet buildings fell silent after less than 10 years of operation.

 

The Class 325's were thankfully not out of action for long though, as at Christmas 2004, in light of heavy demand and congestion on the roads in bad weather, Royal Mail reluctantly awarded GBRf the contract to run a limited number of Class 325's on services between London and Glasgow over the winter period. GBRf however were not cleared to use the Class 325's on their own, and thus instead chose to drag the units using Class 86's and 87's. After a traction reshuffle the Class 325s resumed service with their power cars and without locomotive haulage.

 

Eventually, GBRf lost the contract in 2010 to EWS's successor, DB Schenker, who now operate both Royal Mail services but the continued maintenance of the Class 325 stock. On an average weekday there are 15 diagrammed services out of Willesden Railnet, 5 to and from Warrington, 3 to Shieldmuir and 3 to Low Fell. Today, 15 out of the original 16 units remain in service, 325010 being scrapped in 2012 after years of neglect in storage.

 

Sadly, like many pieces of the Mail Train puzzle, so many were wasted after less than 10 years of operation, infrastructure built to last for 100 years demolished after no time at all. At least the Class 325's have found their way back into work, doing a job that makes eminent sense over the road haulage alternative Royal Mail hoped would be the better option over the mail train. Instead the Class 325's are proof as to why mail-by-rail is the superior option, no traffic jams, no slippery roads, no 60mph speed limiter on the lorries, just 100mph haulage of your valuables and parcels up and down the country all the way!

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

 

The English Electric Lightning was a supersonic jet fighter aircraft of the Cold War era, noted for its great speed. It was the only all-British Mach 2 fighter aircraft and the first aircraft in the world capable of supercruise. The Lightning was renowned for its capabilities as an interceptor; pilots commonly described it as "being saddled to a skyrocket". Following English Electric's integration into the unified British Aircraft Corporation, the aircraft was marketed as the BAC Lightning.

 

The Lightning was prominently used by the Royal Air Force, but also by Saudi Arabia, Kuwait and Singapore. The first aircraft to enter service with the RAF, three pre-production P.1Bs, arrived at RAF Coltishall in Norfolk on 23 December 1959, and from there the aircraft was permanently developed further.

 

The F.6 was the ultimate Lightning version to see British service. Originally, it was nearly identical to the former F.3A (which introduced a large ventral tank and new cambered wings), with the exception that it had provisions to carry 260 gal (1,180 l) ferry tanks on pylons over the wings. These tanks were jettisonable in an emergency, and gave the F.6 a substantially improved deployment capability. The Ferranti A.I.23B radar supported autonomous search, automatic target tracking, and ranging for all weapons, while the pilot attack sight provided gyroscopically derived lead angle and backup stadiametric ranging for gun firing. The radar and gunsight were collectively designated the AIRPASS: Airborne Interception Radar and Pilot Attack Sight System. Combined with the Red Top missile, the system offered a limited forward hemisphere attack capability.

 

There remained one glaring shortcoming of the late Lightning versions, though: the lack of cannon. This was finally rectified in the form of a modified ventral tank with two ADEN cannon mounted in the front. The addition of the cannon and their ammunition decreased the tank's fuel capacity from 610 gal to 535 gal (2,430 l), but the cannon made the F.6 a 'real fighter' again.

 

Singapore's Lightnings came as a bargain, as they had been taken over directly from RAF stocks. In 1967 No. 74 'Tiger' Squadron was moved to RAF Tengah in Singapore to take over the air defense role from the Gloster Javelin equipped 64 Squadron. When 74 Squadron was disbanded in September 1971, following the withdrawal of British forces from Singapore (in the course of the "East of Suez" campaign, which already started in 1968), Tengah Air Base and many other RAF sites like Seletar, Sembawang and Changi as well as the RAF air defense radar station and Bloodhound II surface-to-air missiles were handed over to the SADC, Singapore’s Air Defense Command, which was suddenly entrusted with a huge responsibility and resources.

 

Anyway, in order to fulfill its aerial defense role, Singapore's air force lacked a potent interceptor, and so it was agreed with the RAF that 74 Squadron would leave fourteen Lightnings (twelve F.6 fighters and two T.5 trainers behind, while the rest was transferred to Akrotiri, Cyprus, where the RAF aircraft were integrated into 56 Squadron.

 

The ex-RAF Lightnings, however, immediately formed the small country's quick alert interceptor backbone and were grouped into the newly established 139th Squadron, “Swifts”. The small squadron kept its base at Tengah, as a sister unit to 140th Squadron which operated the Hawker Hunter FGA.74 in the fighter role since 1971.

 

Singapore's Lightnings differed slightly from the RAF F.6: In order to minimize the maintenance costs of this specialized aircraft, the SADC decided to drop the Red Top missile armament. The Red Top gave all-weather capability, but operating this standalone system for just a dozen of aircraft was deemed cost-inefficient. Keeping the high-performance Lightnings airworthy was already costly and demanding enough.

 

As a cost-effective measure, all SADC Lightnings were modified to carry four AIM-9B and later E Sidewinder AAMs on special, Y-shaped pylons, not unlike those used on the US Navy's F-8 Crusader. In order to enhance all-weather capability, an AAS-15 IRST sensor was added, located in a fairing in front of the wind shield. Its electronics used the space of the omitted, fuselage-mounted cannons of the F.6 variant.

 

Long range and loitering time were only of secondary relevance, so that the Singaporean Lightnings typically carried two 30 mm ADEN cannons with 120 RPG in the lower fuselage, which reduced the internal fuel capacity slightly but made the Lightning a true close combat fighter with high agility, speed and rate of climb. Since the RSAF interceptors would only engage in combat after direct visual contact and target identification, the Sidewinders' short range was no operational problem - and because that missile type was also in use with RSAF's Hawker Hunters, this solution was very cost-efficient.

 

The F.6's ability to carry the overwing ferry tanks (the so-called 'Overburgers') was retained, though, as well as the refueling probe and, and with its modified/updated avionics the RSAF Lightnings received the local designations of F.6S and T.5S. They were exclusively used in the interceptor role and retained their natural metal finish all though their service career.

 

In 1975, the SADC was eventually renamed into ‘Republic of Singapore Air Force’ (RSAF), and the aircraft received appropriate markings.

 

The RSAF Lightnings saw an uneventful career. One aircraft was lost due to hydraulic failure in August 1979 (the pilot ejected safely), and when in 1983 RSAF's F-5S fighters took over the duties of airborne interception from the Royal Australian Air Force's Mirage IIIOs detachment stationed at Tengah, all remaining RSAF Lightnings were retired and phased out of service in March 1984 and scrapped. The type's global career did not last much longer: the last RAF Lightnings were retired in 1988 and replaced by the Panavia Tornado ADV.

  

BAE Lightning F.6S general characteristics

Crew: 1

Length: 55 ft 3 in (16.8 m)

Wingspan: 34 ft 10 in (10.6 m)

Height: 19 ft 7 in (5.97 m)

Wing area: 474.5 ft² (44.08 m²)

Empty weight: 31,068 lb (14.092 kg)

Max. take-off weight: 45,750 lb (20.752 kg)

 

Powerplant:

2× Rolls-Royce Avon 301R afterburning turbojets with 12,530 lbf (55.74 kN) dry thrust each and 16,000 lbf (71.17 kN) with afterburner

 

Performance:

Maximum speed: Mach 2.0 (1.300 mph/2.100 km/h) at 36.000 ft.

Range: 850 mi (1.370 km) Supersonic intercept radius: 155 mi (250 km)

Ferry range: 920 mi (800 NM/ 1.660 km) 1,270 mi (1.100 NM/ 2.040 km) with ferry tanks

Service ceiling: 54.000 ft (16.000 m); zoom ceiling >70.000 ft

Rate of climb: 20.000 ft/min (100 m/s)

Wing loading: 76 lb/ft² (370 kg/m²)

Thrust/weight: 0.78

 

Armament:

2× under-fuselage hardpoints for mounting air-to-air missiles (2 or 4 AIM-9 Sidewinder)

Optional, but typically fitted: 2× 30 mm (1.18 in) ADEN cannons with 120 RPG in the lower fuselage, reducing the ventral tank's fuel capacity from 610 gal to 535 gal (2,430 l)

2× overwing pylon stations for 260 gal ferry tanks

    

The kit and its assembly

The inspiration to this whiffy Lightning came through fellow user Nick at whatifmodelers.com (credits go to him), who brought up the idea of EE/BAC Lightnings in Singapore use: such a small country would be the ideal user of this fast interceptor with its limited range. I found the idea very convincing and plausible, and since I like the Lightning and its unique design very much, I (too) had to make one for the 2013 group build "Asiarama" - even if a respective model would potentially be built twice. But it's always fun to see how the same theme is interpreted by different modelers, I am looking forward to my creation's sister ship.

 

The kit is the Matchbox Lightning F.2A/F.6 (PK-114) from 1976, and only little was changed. Fit is O.K., building the model poses no real problems. But the kit needs some putty work at the fuselage seams, and the many raised panel lines (esp. at the belly tank) and other relatively fine and many details for a Matchbox kit make sanding rather hazardous. Nevertheless, it's a solid kit. A bit toy-like, yes, but good value for the relatively little money. What's saved might be well invested into an extra decal sheet (see below).

 

Internal mods include some added details inside of the cockpit and the landing gear wells, but these were just enhancements to the original parts. The Avons' afterburners were simulated with implanted sprocket wheels from a 1:72 Panzer IV - not intended to be realistic at all, but IMO better than the kit's original, plain end caps!

 

Externally…

· the flaps were lowered

· some antennae and a finer pitot added

· about a dozen small air intakes/outlets were added (cut from styrene) or drilled open

· the IRST sensor fairing added, sculpted from a simple piece of sprue

· a pair of 30mm barrels mounted in the lower fuselage (hollow steel needles)

· the scratch-built quadruple Sidewinder rails are worth mentioning

 

The AIM-9E missiles come from the scrap heap, I was lucky to find a matching set of four. The optional overwing fuel tanks were not fitted, as this was supposed to become a "standard RSAF aircraft". I also did not opt for (popular) weapons mounted above the wings, since this would have called for modifications of the F.6 which did not appear worthwhile to me in context with the envisaged RSAF use. Switching to four Sidewinders on the fuselage hardpoints was IMHO enough.

  

Painting and markings

More effort went into this project part. The end of RAF's 74 Squadron at Tengah and the return of the Lightnings to Europe opened a nice historical window for my whif. Since the Tiger Squadron's aircraft sported a natural metal finish, partly with black fins (accidentally, the Matchbox kit offers just the correct decal/painting option), I decided that the RSAF would keep their aircraft this way: without camouflage, just RSAF markings, with some bold and highly visible colors added.

A SEA scheme (as on the RSAF Hunters, Strikemasters of Skyhawks) would have been another serious option and certainly look weird on a Lightning, as well as a three-tone gray wraparound low-viz scheme as used on the F-5E/S fighters, plausible in the 80ies onwards.

 

Testors Aluminum Metallizer was used as basic color, but several other shades including Steel and Titanium Metallizer, Testors normal Aluminum enamel paint, Humbrol 11 and 56 as well as Revell Aqua Color Aluminum were used for selected surface portions or panels all around the hull.

 

The spine including the cockpit frame was painted black. Using RSAF's 140 Squadron's colors as a benchmark, the fin received a checkered decoration in black and red, reminiscent of RAF 56 Squadron Lightnings. This was created through a black, painted base, onto which decals - every red field was cut from a red surface sheet from TL Modellbau - were transferred. Sounds horrible, but it was easier and more exact than expected. A very convenient solution with sharp edges and good contrast. A red trim line, 1mm wide, was added as a decal along the spine in a similar fashion.

 

The squadron emblem on the Lightning's nose was created through the same scratch method: from colored 1.5mm wide stripes, 3mm pieces were cut and applied one by one to form the checkered bar. The swift emblem comes from a 1:48 sheet for French WWI aircraft, made by Peddinghaus Decals from Germany. The overall look was supposed to be similar to the (real) 140 Squadron badge.

 

As a consequence, this created a logical problem: where to put the national roundel? Lightnings usually wore them on the nose, but unlike RAF style (where a bar was added around the roundel), I used RSAF Hunters as benchmark.

The RSAF roundels were a challenge. In order not to cramp the nose section too much I decided to place the roundels behind the wings. Not the must prominent position, but plausible. I originally wanted to use decals from the current 1:72 Airfix BAC Strikemaster kit, but they turned out to be too small.

After long search I was happy to find a 1:48 aftermarket decal sheet from Morgan Decals for an A-4S, with full color yin-yang roundels - in Canada! It took three weeks to wait for these parts, though, even though work had to wait for this final but vital detail !

 

As a side not, AFAIK any RSAF aircraft only carried and carries these roundels on the fuselage sides, not on the wings' upper or lower surfaces? It leaves the model a bit naked, so I decided to add 'RSAF' letters and the tactical code '237' to the wings' upper and lower sides. But the fin is surely bold enough to compensate ;)

 

The cockpit interior was painted in Medium Sea Gray (Humbrol 27), the landing gear and the wells in a mix of Humbrol 56 and 34, for a light gray with a metallic shimmer.

 

Other details include the white area behind the cockpit, which contained an AVPIN/isopropyl nitrate tank for the Lightning's start engine. Hazardous stuff - the light color was to prevent excessive heating in the sun, a common detail for Lightnings used in Cyprus. Another piece that took some effort was the shaggy nose cone, which was painted in a mix of Humbrol 56 and 86 and received some serious dry painting in light gray and ochre.

 

Stencils etc. were taken from an extensive aftermarket sheet for Lightnings from Xtradecal (X72096). The Matchbox decal sheet of PK-114 just offers the ejection seat warning triangles - that's all! The later T.55 kit is much better in this regard, but still far from being complete.

 

After decal application and to enhance the metallic look, the kit received a careful rubbing with finely grinded graphite, which, as a side effect, also emphasized the raised panel lines. A little dry painting was done around some exhaust openings, but nothing to make the aircraft look really old. This is supposed to be a bright and well-maintained interceptor!

 

Finally, the kit received a thin coat with glossy acrylic varnish, the spine and fin received a semi-matt coat and the black glare shield in front of the cockpit became matt.

   

A pretty straightforward build for the Asiarama group build, and with best regards and credits to Nick who came up with the original idea. Most work went into the decals and the NMF finish. I like the bold colors, and despite being flamboyant, they do not make the Lightning look too far out of place?

 

As a final note: XR773 never ended up in Singapore service, just like any BAC Lightning. In real life, the aircraft (first flight was in February 1966 with Roly Beamont at the controls) was transferred from 74 Squadron at RAF Tengah to Akrotiri in late 1971 and had a pretty long life, further serving with 56, 5 and 11 Squadrons as well as the Lightning Training Flight. And even then it’s life was far from over: XR773 is one of the Lightning survivors; in South Africa it flew in private hands as ZU-BEW until 2010, when it was grounded and the airframe put up to sale.

Robert has always struck me as someone skilled, who was knowledgeable, capable, and understanding. His is a maturity that far outstretches his age. His filters adjust for his company, his views remain logical even when opinionated. He could converse with the friends or parents of any friend he made and hold that relationship long after the fickleness of younger ones. Being able to adapt to any situation even if it isn’t your suit is an incredible trait.

 

I remember the night of this photo, the birthday of my now ex-girlfriend, at Caprice Night club. I was never comfortable in that scene growing up. I thought the idea of a club beneath me, the pretentious, anime watching moron who only listened to hard rock music (AND DUBSTEP, DUH). I enjoyed being near friends, but at parties and the like I’d always find a set away area to go and sit by myself. Robert came to join me and for a little while that night. It was nice having company. I envied that he was able to go out in the fray of it all, though curios that he would come to sit down and enjoy being separated as much as I did. It’s something I’ve worked to exemplify in my self. On that note, catch me photographing MIA nightclub on the 18th and 19th. I’ve grown up a bit. Now I listen to Rock, Dubstep, and Yung Lean too.

 

Kodak Disposable - December, 2012

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

  

Some background:

The Wasp was a transonic British jet-powered fighter aircraft that was developed by Folland for the Royal Air Force (RAF) during the late 1940s and early 1950s. The Wasp’s origins could be traced back to a privately funded 1952 concept for a bigger and more capable day fighter aircraft than Folland’s very light Midget/Gnat. The Wasp’s development had been continued until the Gnat’s service introduction, and by then it had evolved under the handle “Fo-145” into a supersonic aircraft that took advantage of the new Armstrong Siddeley Sapphire turbojet engine, swept wings and area rule. The aircraft was built with the minimum airframe size to take the reheated Saphire and a radar system that would allow it to deploy the new de Havilland Blue Jay (later Firestreak) guided air-to-air missile. In this form the aircraft was expected to surpass the Royal Air Force’s contemporary day fighter, the only gun-armed Hawker Hunter, which had been in service since 1954, while using basically the same engine as its F.2 variant, in both performance and armament aspects. The missile-armed Wasp was also expected to replace the disappointing Supermarine Swift and the Fairey Fireflash AAMs that had been developed for it.

The Wasp strongly resembled the smaller Gnat, with a similar but much thinner shoulder mounted wing, with a sweep of 35° at quarter chord, but the new aircraft featured some innovations. Beyond the area-ruled fuselage, the aircraft had full-span leading edge slats and trailing edge flaps with roll control achieved using spoilers rather than traditional ailerons. Anticipating supersonic performance, the tailplane was all-moving. The cockpit had been raised and offered the pilot a much better all-round field of view.

 

The Wasp was armed with four 30 mm (1.18 in) ADEN cannon, located under the air intakes. Each gun had a provision of 125 rounds, from form a mutual ventral ammunition bay that could be quickly replaced. Four underwing hardpoints could carry an ordnance load of up to 4.000 lb, and the Wasp’s main armament consisted of up to four IR-guided “Firestreak” AAMs. To effectively deploy them, however, a radar system was necessary. For launch, the missile seeker was slaved to the Wasp’s AI.Mk.20 X-band radar until lock was achieved and the weapon was launched, leaving the interceptor free to acquire another target. The AI.Mk.20 had been developed by EKCO since 1953 under the development label “Green Willow” for the upcoming EE Lightning interceptor, should the latter’s more complex and powerful Ferranti AIRPASS system fail. A major advantage of the AI.Mk.20 was that it had been designed as a single unit so it could be fit into the nose of smaller single-seat fighters, despite its total weight of roughly 400 lb (200 kg). For the Firestreak AAM, EKCO had developed a spiral-scan radar with a compact 18 in (460 mm) antenna that offered an effective range of about 10 miles (16 km), although only against targets very close to the centerline of the radar. The radar’s maximum detection range was 25 mi (40 km) and the system also acted as a ranging radar, providing range input to the gyro gunsight for air-to-air gunnery.

Beyond Firestreaks, the Wasp could also carry drop tanks (which were area-ruled and coulc only be carried on the inner pair of pylons), SNEB Pods with eighteen 68 mm (2.68 in) unguided rocket projectiles against air and ground targets, or iron bombs of up to 1.000 lb caliber. Other equipment included a nose-mounted, and a forward-facing gun camera.

 

The Royal Air Force was sufficiently impressed to order two prototypes. Since the afterburning version of the Sapphire was not ready yet, the first prototype flew on 30 July 1954 with a non-afterburning engine, an Armstrong Siddeley Sapphire Sa.6 with 8,000 lbf (35.59 kN). In spite of this lack of power the aircraft nevertheless nearly reached Mach 1 in its maiden flight. The second prototype, equipped with the intended Sapphire Sa.7 afterburning engine with 11,000 lbf (48.9 kN) thrust engine, showed the aircraft’s full potential. The Wasp turned out to have very good handling, and the RAF officially ordered sixty Folland Fo-145 day-fighters under the designation “Wasp F.Mk.1”. The only changes from the prototypes were small leading-edge extensions at the wing roots, improving low speed handling, esp. during landings and at high angles of incidence in flight.

 

Most Wasps were delivered to RAF Germany frontline units, including No. 20 and 92 Squadrons based in Northern Germany. However, the Wasp’s active service did not last long, because technological advancements quickly rendered the aircraft obsolete in its original interceptor role. The Wasp’s performance had not turned out as significantly superior to the Hunter as expected. Range was rather limited, and the aircraft turned out to be underpowered, since the reheated Sapphire Sa6 did not develop as much power as expected. The AI.Mk.20 radar was rather weak and capricious, too, and the Firestreak was an operational nightmare. The missile was, due to its solid Magpie rocket motor and the ammonia coolant for the IR seeker head, highly toxic and RAF armorers had to wear some form of CRBN protection to safely mount the missile onto an aircraft. Furthermore, unlike modern missiles, Firestreak’s effectiveness was very limited since it could only be fired outside cloud - and over Europe or in winter, skies were rarely clear.

 

Plans for a second production run of the Folland Wasp with a more powerful Sapphire Sa7R engine with a raised thrust of 12,300 lbf (54.7 kN) and updated avionics were not carried out. During the 1960s, following the successful introduction of the supersonic English Electric Lightning in the interceptor role, the Wasp, as well as the older but more prosperous and versatile Hunter, transitioned to being operated as a fighter-bomber, advanced trainer and for tactical photo reconnaissance missions.

This led to a limited MLU program for the F.Mk.1s and conversions of the remaining airframes into two new variants: the new main version was the GR.Mk.2, a dedicated CAS/ground attack variant, which had its radar removed and replaced with ballast, outwardly recognizable through a solid metal nose which replaced the original fiberglass radome. Many of these machines also had two of the 30mm guns removed to save weight. Furthermore, a handful Wasps were converted into PR.Mk.3s. These had as set of five cameras in a new nose section with various windows, and all the guns and the ammunition bay were replaced with an additional fuel tank, operating as pure, unarmed reconnaissance aircraft. When Folland was integrated into the Hawker Siddeley Group in 1963 the aircraft’s official name was changed accordingly, even though the Folland name heritage persisted.

 

Most of these aircraft remained allocated to RAF Germany units and retired towards the late Sixties, but four GR.Mk.2s were operated by RAF No. 57 (Reserve) Squadron and based at No. 3 Flying Training School at Cranwell, where they were flown as adversaries in dissimilar aerial combat training. The last of the type was withdrawn from service in 1969, but one aircraft remained flying with the Aeroplane and Armament Experimental Establishment at Boscombe Down until 24 January 1975.

  

General characteristics:

Crew: 1

Length: 45 ft 10.5 in (13.983 m)

Wingspan: 31 ft 7.5 in (9.639 m)

Height: 13 ft 2.75 in (4.0323 m)

Wing area: 250 sq ft (23 m2)

Empty weight: 13,810 lb (6,264 kg)

Gross weight: 21,035 lb (9,541 kg)

Max takeoff weight: 23,459 lb (10,641 kg)

 

Powerplant:

1× Armstrong Siddeley Sapphire Sa.6, producing 7,450 lbf (33.1 kN) thrust at 8,300 rpm,

military power dry, and 11,000 lbf (48.9 kN) with afterburner

 

Performance:

Maximum speed: 631 kn (726 mph, 1,169 km/h) / M1.1 at 35,000 ft (10,668 m)

654 kn (753 mph; 1,211 km/h) at sea level

Cruise speed: 501 kn (577 mph, 928 km/h)

Range: 1,110 nmi (1,280 mi, 2,060 km)

Service ceiling: 49,000 ft (15,000 m)

Rate of climb: 16,300 ft/min (83 m/s)

Wing loading: 84 lb/sq ft (410 kg/m2)

Thrust/weight: 0.5

 

Armament:

4× 30 mm (1.18 in) ADEN cannon, 125 rounds per gun

4× underwing hardpoints for a total external ordnance of 4.000 lb, including Firestreak AAMs,

SNEB pods, bombs of up to 1.000 lb caliber or two 125 imp gal (570 l) drop tanks

  

The kit and its assembly

This kit travesty is a remake of a simple but brilliant idea of fellow modeler chrisonord at whatifmodellers’com (www.whatifmodellers.com/index.php?topic=48434.msg899420#m...), who posted his own build in late 2020: a Grumman Tiger in standard contemporary RAF colors as Folland Wasp GR.Mk.2. The result looked like a highly credible “big brother” or maybe successor of Folland’s diminutive Midge/Gnat fighter, something in the Hawker Hunter’s class. I really like the idea a lot and decided that it was, one and a half years later, to build my personal interpretation of the subject – also because I had a Hasegawa F11F kit in The Stash™ without a proper plan.

 

The Tiger was built basically OOB – a simple and straightforward affair that goes together well, just the fine, raised panel lines show the mould’s age. The only changes I made: the arrester hook disappeared under PSR, small stabilizer fins (from an Italeri BAe Hawk) were added under the tail section, and I replaced the Tiger’s rugged twin wheel front landing gear with a single wheel alternative, left over from a Matchbox T-2 Buckeye. On the main landing gear, the rearward-facing stabilizing struts were deleted (for a lighter look of a land-based aircraft) and their wells filled with putty. A late modification were additional swing arms for the main landing gear, though: once the kit could sit on its own three feet, the stance was odd and low, esp. under the tail – probably due to the new front wheel. As a remedy I glued additional swing arm elements, made from 1mm steel wire, under the original struts, what moved the main wheel a little backwards and raised the main landing gear my 1mm. Does not sound like much, but it was enough to lift the tail and give the aircraft a more convincing stance and ground clearance.

 

The area-ruled drop tanks and their respective pylons were taken from the Hasegawa kit. For a special “British” touch – because the Tiger had a radome (into which no radar was ever fitted, though) – I added a pair of Firestreak AAMs on the outer underwing stations, procured from a Gomix Gloster Javelin (which comes with four of these, plus pylons).

  

Painting and markings:

Since the RAF theme was more or less settled, paintwork revolved around more or less authentical colors and markings. The Wasp received a standard RAF day fighter scheme from the late Fifties, with upper camouflage in RAF Dark Green/Dark Sea Grey and Light Aircraft Grey undersides with a low waterline. I used Humbrol 163, 106 and 166, respectively – Ocean Grey was used because I did not have the proper 164 at hand, but 106 also offered the benefit of a slightly better contrast to the murky Dark Green. A black ink washing was applied plus some panel post-shading. The silver leading edges on wings, stabilizers and fin were created with decal sheet material, avoiding the inconvenience of masking.

 

The cockpit interior was painted in a very dark grey (Revell 09, Anthracite) while the landing gear, wheels and wells received a greyish-metallic finish (Humbrol 56, Aluminum Dope). The air intakes’ interior became bright aluminum (Revell 99), the area around the jet nozzle was painted with Revell 91 (Iron metallic) and later treated with graphite for a dark metallic shine. The drop tanks were camouflaged, the Firestreaks became white so that they would stand out well and add to a certain vintage look.

 

The decals were a mix from various sources. The No. 20 Squadron badges and the Type D high-viz roundels on the wings were left over from an Airfix Hawker Hunter. The fuselage roundels came from an Italeri BAe Hawk sheet, IIRC. The bent fin flash, all the stencils as well as the serial code (which was puzzled together from two real serials and was AFAIK not allocated to any real RAF aircraft) came from an Xtradecal Supermarine Swift sheet. The individual red “B” letter came from a Matchbox A.W. Meteor night fighter.

 

Finally, the kit was sealed with matt acrylic varnish – I considered a glossy finish, since this was typical for RAF aircraft in the Fifties, but eventually just gave the radome a light shine.

  

Basically a simple project, and quickly done in just a couple of days. However, chrisonord’s great eye for similarities makes this “Tiger in disguise” a great fictional aircraft model with only little effort, it’s IMHO very convincing. And the RAF colors and markings suit the F11F very well.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

  

Some background:

The North American FJ-4 Fury was a swept-wing carrier-capable fighter-bomber, originally developed for the United States Navy and Marine Corps. It was the final development in a lineage that included the Air Force's F-86 Sabre. The FJ-4 shared its general layout and engine with the earlier FJ-3, but featured an entirely new wing design. And it was, as a kind of final embodiment with the FJ-4B, a very different aircraft from the F-86 .

 

The first FJ-4 flew on 28 October 1954 and delivery began in February 1955. Of the original order for 221 FJ-4 fighters, the last 71 were modified into the FJ-4B fighter-bomber version, of which the Netherlands received 16 aircraft under the designation FJ-4B from the USA in the course of NATO support. Even though the main roles of the MLD were maritime patrol, anti-submarine warfare and search and rescue, the FJ-4B was a dedicated fighter-bomber, and these aircraft were to be used with the Dutch Navy’s Colossus-Class carrier HNLMS Karel Doorman (R81).

 

Compared to the lighter FJ-4 interceptor, the FJ-4B had a stronger wing with six instead of four underwing stations, a stronger landing gear and additional aerodynamic brakes under the aft fuselage. The latter made landing safer by allowing pilots to use higher thrust settings, and were also useful for dive attacks. Compared to the FJ-4, external load was doubled, and the US FJ-4Bs were capable of carrying a nuclear weapon on the inboard port station, a feature the MLD Furies lacked. The MLD aircraft were still equipped with the corresponding LABS or Low-Altitude Bombing System for accurate delivery of ordnance.

The Dutch Furies were primarily intended for anti-ship missions (toting up to five of the newly developed ASM-N-7 missiles - renamed in AGM-12B Bullpup after 1962 - plus a guidance pod) and CAS duties against coastal targets, as well as for precision strikes. In a secondary role, the FJ-4B could carry Sidewinder AAMs for interception purposes.

 

The MLD's FJ-4B became operational in 1956, just in time to enhance the firepower of the Karel Doorman, which just had its 24 WW-II era propeller driven Fairey Firefly strike fighters and Hawker Sea Fury fighter/anti-ship aircraft backed up with 14 TBF Avenger ASW/torpedo bombers and 10 Hawker Sea Hawk fighters (the MLD owned 22 of these) for an ASW/Strike profile. The Furies joined the carrier in late 1957 and replaced the piston-engined attack aircraft.

 

In 1960, during the Dutch decolonization and planned independence of Western New Guinea, a territory which was also claimed by Indonesia, the Karel Doorman set sail along with two destroyers and a modified oil tanker to 'show the flag'. In order to avoid possible problems with Indonesia's ally Egypt at the Suez Canal, the carrier instead sailed around the horn of Africa. She arrived in Fremantle, Australia, where the local seamen's union struck in sympathy with Indonesia; the crew used the propeller thrust of aircraft chained down on deck to nudge the carrier into dock without tugs! In addition to her air wing, she was ferrying twelve Hawker Hunter fighters to bolster the local Dutch defense forces, which the Karel Doorman delivered when she arrived at Hollandia, New Guinea.

 

During the 1960 crisis, Indonesia prepared for a military action named Operation Trikora (in the Indonesian language, "Tri Komando Rakyat" means "The Three Commands of the People"). In addition to planning for an invasion, the TNI-AU (Indonesian Air Forces) hoped to sink the Karel Doorman with Soviet-supplied Tupolev Tu-16KS-1 Badger naval bombers using AS-1 Kennel/KS-1 Kometa anti-ship missiles. This bomber-launched missile strike mission was cancelled on short notice, though, because of the implementation of the cease-fire between Indonesia and the Netherlands. This led to a Dutch withdrawal and temporary UN peacekeeping administration, followed by occupation and annexation through Indonesia. While the Dutch aircraft served actively during this conflict, flying patrols and demonstrating presence, visibly armed and in alert condition, no 'hot' sortie or casualty occured, even though one aircraft, 10-18, was lost in a start accident. The pilot ejected safely.

 

The MLD FJ-4Bs only served on the carrier until its overhaul in 1964, after which the carrier-borne attack role was eliminated and all aircraft were transferred to land bases (Valkenburg) or in reserve storage. The Seahawks were retired from service by the end of the 1960s after the sale of the Karel Doorman to Argentina, and the FJ-4Bs were returned to the United States, where they were re-integrated into the USMC until the end of the 1960ies, when all FJ-4 aircraft were phased out.

  

General characteristics:

Crew: 1

Length: 36 ft 4 in (11.1 m)

Wingspan: 39 ft 1 in (11.9 m)

Height: 13 ft 11 in (4.2 m)

Wing area: 338.66 ft² (31.46 m²)

Empty weight: 13,210 lb (6,000 kg)

Loaded weight: 20,130 lb (9,200 kg)

Max. take-off weight: 23,700 lb (10,750 kg)

Powerplant: 1 × Wright J65-W-16A turbojet, 7,700 lbf (34 kN)

 

Performance:

Maximum speed: 680 mph (1,090 km/h) at 35,000 ft (10,670 m)

Range: 2,020 mi (3,250 km) with 2× 200 gal (760 l) drop tanks and 2× AIM-9 missiles

Service ceiling: 46,800 ft (14,300 m)

Rate of climb: 7,660 ft/min (38.9 m/s)

Wing loading: 69.9 lb/ft² (341.7 kg/m²)

Thrust/weight: .325

 

Armament:

4× 20 mm (0.787 in) cannon

6× pylons under the wings for 3,000 lb (1,400 kg) external ordnance, including up to 6× AIM-9 Sidewinder AAMs, bombs and guided/unguided ASM, e .g. ASM-N-7 (AGM-12B Bullpup) missiles.

  

The kit and its assembly

Originally, this model project was inspired by a (whiffy) Dutch F3H Demon profile, designed by fellow user Darth Panda at whatifmodelers.com. I found the idea of a foreign/NATO user of one of these early carrier-borne jet fighters very inspiring – not only because of the strange design of many of these aircraft, but also since the USN and USMC had been the only real world users of many of these types.

 

Initially, I planned to convert a F3H accordingly. But with limited storage/display space at home I decided to apply the MLD idea to another smaller, but maybe even more exotic, type: the North American FJ-4B Fury, which was in 1962 recoded into AF-1E.

I like the beefy Sabre cousin very much. It’s one of those aircraft that received little attention, even from model kit manufacturers. In fact, in 1:72 scale there are only vintage vacu kits or the very basic Emhar kit available. Th Emhar kit, which I used here and which is a kind donation of a fellow modeler (Thanks a lot, André!), a rather rough thing with raised panel lines and much room for improvements. As a side note, there's also a FJ-4B from Revell, but it's just a 1996 re-issue with no improvements, whatsoever.

 

Another facet of the model: When I did legwork concerning a possible background story, I was surprised to find out that the Netherlands actually operated aircraft carriers in the 1950s, including carrier-borne, fixed-wing aircraft, even jets in the form of Hawker Sea Hawks. The real life FJ-4Bs service introduction, the naissance of NATO and the Indonesian conflict as well as the corresponding intervention of the Karel Doorman carrier all fell into a very plausible time frame – and so there’s a very good and plausible story why the MLD could actually have used the Fury fighter bomber!

 

The Emhar kit was not modified structurally, but saw some changes in detail. These include a scratch-built cockpit with side walls, side consoles and a new ejection seat, plus a Matchbox pilot figure, a new front wheel (from a Kangnam Yak-38, I believe), plus a lot of added blade aerials and a finer pitot.

The flaps were lowered, for a more lively look- Another new feature is the opened air intake, which features a central splitter - in fact a vertically placed piece of a Vicker Wellesley bomb container from Matchbox. At the rear end, the exhaust pipe was opened and lengthened internally.

 

The six weapon hardpoints were taken from the original kit, but I did not use the four Sidewinder AAMs and the rather bulky drop tanks. So, all ordnance is new: the Bullpups come from the Hasegawa air-to-ground missile set, the drop tanks are leftover pieces from a Hobby Boss F-86. They are much more 'delicate', and make the Fury look less stout and cumbersome. The guidance pod for the Bullpups (a typical FJ-4B feature with these weapons) is a WWII drop tank, shaped with the help of benchmark pictures. Certainly not perfect, but, hey - it's just a MODEL!

  

Painting and markings

I used mid-1950ies MLD Sea Furys and Sea Hawks as a design benchmark, but this Fury is placed just into the time frame around 1960 when the MLD introduced a new 3-digit code system. Before that, a code "6-XX" with the XX somewhere in the 70 region would have been appropriate, and I actually painted the fuselage sides a bit darker so as if the old code had recently been painted over.

 

Dutch MLD aircraft tended to keep their former users’ liveries, but in the FJ-4B’s case I thought that a light grey and white aircraft (USN style) with Dutch roundels would look a bit odd. So I settled for early NATO style with Extra Dark Sea Grey upper sides (Humbrol 123) and Sky from below (Testors 2049 from their Authentic Line).

 

I also went for an early design style with a low waterline - early Hawker Sea Furies were painted this way, and a high waterline would probably be more typical. But in the face of potential seriosu action, who knows...? Things tend to be toned down quickly, just remember the RN Harriers during the Falkland conflict. I'll admit that the aircraft looks a bit simple and dull now, but this IMHO just adds to the plausible look of this whif. I prefer such subtleties to garish designs.

 

The surfaces were weathered with dry-brushed lighter shades of the basic tones (mostly Humbrol 79, but also some 140 and 67, and Humbrol 90 and 166 below), including overpainted old codes in a slightly darker tone of EDSG, done with Revell 77. A light wash with black ink emphasizes edges and some details - the machine was not to look worn.

 

The interior was painted in medium grey (Humbrol 140), the landing gear is white (Humbrol 130), and some details like the air intake rim, the edges of the landing gear covers, the flaps or the tips of the wing fences were painted in bright red (Humbrol 174), for some contrast to the overall grey upper sides.

 

The MLD markings were puzzled together. The roundels come from an Xtradecal sheet for various Hawker Sea Furies, the '202' code comes, among others, from a Grumman Bearcat aftermarket sheet. The 'KON. MARINE' line is hand-made, letter by letter, from a TL Modellbau aftremarket sheet.

Most stencils and warning sign decals come from the original decal sheet, as well as from a FJ-4 Xtradecal aftermarket sheet, from F-86 kits and the scrap box. I wanted these details to provide the color to the aircraft, so that it would not look too uniform, but still without flashy decorations and like a rather utilarian military item.

 

finally, the model received a coat of semi-matt varnish (Tamiya Acryllic), since MLD aircraft had a pretty glossy finish. No dirt or soot stains were added - the Dutch kept their (few) shipborne aircraft very clean and tidy!

  

So, all in all, a simple looking aircraft, but this Dutch Fury has IMHO a certain, subtle charm - probably also because it is a rather rare and unpopular aircraft, which in itself has a certain whiffy aura.

REFLECTING vs BLURRY

 

.

At the time it is all a confusion; in retrospectall a blur. by Schlesinger, Arthur M(eier),Jr

.

“Sometimes in our confusion, we see not the world as it is, but the world though eyes blurred by the mind.” by unknown

.

“Love is like a mirror. When you love another you become his mirror and he becomes yours...And reflecting each other's love you see infinity.” by unknown

.

“A moral being is one who is capable of reflecting on his past actions and their motives - of approving of some and disapproving of others” by Charles Darwin

 

. bacio to a friend...and good night...

  

My old K75S. A good, reliable and capable bike but it was heavy!

Still a capable camera today. Don't underestimate the old black crow. Yes it's limited if you know what those limits are. Expect to sharpen PP a little.

The colors are true.

It has been said it has that transparency film like IQ about it.

The 300 ED IF manual is a beast to keep steady in hand with it's shallow depth of field. This image was cropped at 100%.

So it's a bit gritty when zoomed in, it's still impressive for 4.2mp.

I paid $38.00 for this body it has the early D2h Err hiccup at first start up.

After a two or three shots it's fine not worth sending off to get fixed as you can buy another working one for way less Nikon charges for repair.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

  

Some background:

The North American FJ-4 Fury was a swept-wing carrier-capable fighter-bomber, originally developed for the United States Navy and Marine Corps. It was the final development in a lineage that included the Air Force's F-86 Sabre. The FJ-4 shared its general layout and engine with the earlier FJ-3, but featured an entirely new wing design. And it was, as a kind of final embodiment with the FJ-4B, a very different aircraft from the F-86 .

 

The first FJ-4 flew on 28 October 1954 and delivery began in February 1955. Of the original order for 221 FJ-4 fighters, the last 71 were modified into the FJ-4B fighter-bomber version, of which the Netherlands received 16 aircraft under the designation FJ-4B from the USA in the course of NATO support. Even though the main roles of the MLD were maritime patrol, anti-submarine warfare and search and rescue, the FJ-4B was a dedicated fighter-bomber, and these aircraft were to be used with the Dutch Navy’s Colossus-Class carrier HNLMS Karel Doorman (R81).

 

Compared to the lighter FJ-4 interceptor, the FJ-4B had a stronger wing with six instead of four underwing stations, a stronger landing gear and additional aerodynamic brakes under the aft fuselage. The latter made landing safer by allowing pilots to use higher thrust settings, and were also useful for dive attacks. Compared to the FJ-4, external load was doubled, and the US FJ-4Bs were capable of carrying a nuclear weapon on the inboard port station, a feature the MLD Furies lacked. The MLD aircraft were still equipped with the corresponding LABS or Low-Altitude Bombing System for accurate delivery of ordnance.

The Dutch Furies were primarily intended for anti-ship missions (toting up to five of the newly developed ASM-N-7 missiles - renamed in AGM-12B Bullpup after 1962 - plus a guidance pod) and CAS duties against coastal targets, as well as for precision strikes. In a secondary role, the FJ-4B could carry Sidewinder AAMs for interception purposes.

 

The MLD's FJ-4B became operational in 1956, just in time to enhance the firepower of the Karel Doorman, which just had its 24 WW-II era propeller driven Fairey Firefly strike fighters and Hawker Sea Fury fighter/anti-ship aircraft backed up with 14 TBF Avenger ASW/torpedo bombers and 10 Hawker Sea Hawk fighters (the MLD owned 22 of these) for an ASW/Strike profile. The Furies joined the carrier in late 1957 and replaced the piston-engined attack aircraft.

 

In 1960, during the Dutch decolonization and planned independence of Western New Guinea, a territory which was also claimed by Indonesia, the Karel Doorman set sail along with two destroyers and a modified oil tanker to 'show the flag'. In order to avoid possible problems with Indonesia's ally Egypt at the Suez Canal, the carrier instead sailed around the horn of Africa. She arrived in Fremantle, Australia, where the local seamen's union struck in sympathy with Indonesia; the crew used the propeller thrust of aircraft chained down on deck to nudge the carrier into dock without tugs! In addition to her air wing, she was ferrying twelve Hawker Hunter fighters to bolster the local Dutch defense forces, which the Karel Doorman delivered when she arrived at Hollandia, New Guinea.

 

During the 1960 crisis, Indonesia prepared for a military action named Operation Trikora (in the Indonesian language, "Tri Komando Rakyat" means "The Three Commands of the People"). In addition to planning for an invasion, the TNI-AU (Indonesian Air Forces) hoped to sink the Karel Doorman with Soviet-supplied Tupolev Tu-16KS-1 Badger naval bombers using AS-1 Kennel/KS-1 Kometa anti-ship missiles. This bomber-launched missile strike mission was cancelled on short notice, though, because of the implementation of the cease-fire between Indonesia and the Netherlands. This led to a Dutch withdrawal and temporary UN peacekeeping administration, followed by occupation and annexation through Indonesia. While the Dutch aircraft served actively during this conflict, flying patrols and demonstrating presence, visibly armed and in alert condition, no 'hot' sortie or casualty occured, even though one aircraft, 10-18, was lost in a start accident. The pilot ejected safely.

 

The MLD FJ-4Bs only served on the carrier until its overhaul in 1964, after which the carrier-borne attack role was eliminated and all aircraft were transferred to land bases (Valkenburg) or in reserve storage. The Seahawks were retired from service by the end of the 1960s after the sale of the Karel Doorman to Argentina, and the FJ-4Bs were returned to the United States, where they were re-integrated into the USMC until the end of the 1960ies, when all FJ-4 aircraft were phased out.

  

General characteristics:

Crew: 1

Length: 36 ft 4 in (11.1 m)

Wingspan: 39 ft 1 in (11.9 m)

Height: 13 ft 11 in (4.2 m)

Wing area: 338.66 ft² (31.46 m²)

Empty weight: 13,210 lb (6,000 kg)

Loaded weight: 20,130 lb (9,200 kg)

Max. take-off weight: 23,700 lb (10,750 kg)

Powerplant: 1 × Wright J65-W-16A turbojet, 7,700 lbf (34 kN)

 

Performance:

Maximum speed: 680 mph (1,090 km/h) at 35,000 ft (10,670 m)

Range: 2,020 mi (3,250 km) with 2× 200 gal (760 l) drop tanks and 2× AIM-9 missiles

Service ceiling: 46,800 ft (14,300 m)

Rate of climb: 7,660 ft/min (38.9 m/s)

Wing loading: 69.9 lb/ft² (341.7 kg/m²)

Thrust/weight: .325

 

Armament:

4× 20 mm (0.787 in) cannon

6× pylons under the wings for 3,000 lb (1,400 kg) external ordnance, including up to 6× AIM-9 Sidewinder AAMs, bombs and guided/unguided ASM, e .g. ASM-N-7 (AGM-12B Bullpup) missiles.

  

The kit and its assembly

Originally, this model project was inspired by a (whiffy) Dutch F3H Demon profile, designed by fellow user Darth Panda at whatifmodelers.com. I found the idea of a foreign/NATO user of one of these early carrier-borne jet fighters very inspiring – not only because of the strange design of many of these aircraft, but also since the USN and USMC had been the only real world users of many of these types.

 

Initially, I planned to convert a F3H accordingly. But with limited storage/display space at home I decided to apply the MLD idea to another smaller, but maybe even more exotic, type: the North American FJ-4B Fury, which was in 1962 recoded into AF-1E.

I like the beefy Sabre cousin very much. It’s one of those aircraft that received little attention, even from model kit manufacturers. In fact, in 1:72 scale there are only vintage vacu kits or the very basic Emhar kit available. Th Emhar kit, which I used here and which is a kind donation of a fellow modeler (Thanks a lot, André!), a rather rough thing with raised panel lines and much room for improvements. As a side note, there's also a FJ-4B from Revell, but it's just a 1996 re-issue with no improvements, whatsoever.

 

Another facet of the model: When I did legwork concerning a possible background story, I was surprised to find out that the Netherlands actually operated aircraft carriers in the 1950s, including carrier-borne, fixed-wing aircraft, even jets in the form of Hawker Sea Hawks. The real life FJ-4Bs service introduction, the naissance of NATO and the Indonesian conflict as well as the corresponding intervention of the Karel Doorman carrier all fell into a very plausible time frame – and so there’s a very good and plausible story why the MLD could actually have used the Fury fighter bomber!

 

The Emhar kit was not modified structurally, but saw some changes in detail. These include a scratch-built cockpit with side walls, side consoles and a new ejection seat, plus a Matchbox pilot figure, a new front wheel (from a Kangnam Yak-38, I believe), plus a lot of added blade aerials and a finer pitot.

The flaps were lowered, for a more lively look- Another new feature is the opened air intake, which features a central splitter - in fact a vertically placed piece of a Vicker Wellesley bomb container from Matchbox. At the rear end, the exhaust pipe was opened and lengthened internally.

 

The six weapon hardpoints were taken from the original kit, but I did not use the four Sidewinder AAMs and the rather bulky drop tanks. So, all ordnance is new: the Bullpups come from the Hasegawa air-to-ground missile set, the drop tanks are leftover pieces from a Hobby Boss F-86. They are much more 'delicate', and make the Fury look less stout and cumbersome. The guidance pod for the Bullpups (a typical FJ-4B feature with these weapons) is a WWII drop tank, shaped with the help of benchmark pictures. Certainly not perfect, but, hey - it's just a MODEL!

  

Painting and markings

I used mid-1950ies MLD Sea Furys and Sea Hawks as a design benchmark, but this Fury is placed just into the time frame around 1960 when the MLD introduced a new 3-digit code system. Before that, a code "6-XX" with the XX somewhere in the 70 region would have been appropriate, and I actually painted the fuselage sides a bit darker so as if the old code had recently been painted over.

 

Dutch MLD aircraft tended to keep their former users’ liveries, but in the FJ-4B’s case I thought that a light grey and white aircraft (USN style) with Dutch roundels would look a bit odd. So I settled for early NATO style with Extra Dark Sea Grey upper sides (Humbrol 123) and Sky from below (Testors 2049 from their Authentic Line).

 

I also went for an early design style with a low waterline - early Hawker Sea Furies were painted this way, and a high waterline would probably be more typical. But in the face of potential seriosu action, who knows...? Things tend to be toned down quickly, just remember the RN Harriers during the Falkland conflict. I'll admit that the aircraft looks a bit simple and dull now, but this IMHO just adds to the plausible look of this whif. I prefer such subtleties to garish designs.

 

The surfaces were weathered with dry-brushed lighter shades of the basic tones (mostly Humbrol 79, but also some 140 and 67, and Humbrol 90 and 166 below), including overpainted old codes in a slightly darker tone of EDSG, done with Revell 77. A light wash with black ink emphasizes edges and some details - the machine was not to look worn.

 

The interior was painted in medium grey (Humbrol 140), the landing gear is white (Humbrol 130), and some details like the air intake rim, the edges of the landing gear covers, the flaps or the tips of the wing fences were painted in bright red (Humbrol 174), for some contrast to the overall grey upper sides.

 

The MLD markings were puzzled together. The roundels come from an Xtradecal sheet for various Hawker Sea Furies, the '202' code comes, among others, from a Grumman Bearcat aftermarket sheet. The 'KON. MARINE' line is hand-made, letter by letter, from a TL Modellbau aftremarket sheet.

Most stencils and warning sign decals come from the original decal sheet, as well as from a FJ-4 Xtradecal aftermarket sheet, from F-86 kits and the scrap box. I wanted these details to provide the color to the aircraft, so that it would not look too uniform, but still without flashy decorations and like a rather utilarian military item.

 

finally, the model received a coat of semi-matt varnish (Tamiya Acryllic), since MLD aircraft had a pretty glossy finish. No dirt or soot stains were added - the Dutch kept their (few) shipborne aircraft very clean and tidy!

  

So, all in all, a simple looking aircraft, but this Dutch Fury has IMHO a certain, subtle charm - probably also because it is a rather rare and unpopular aircraft, which in itself has a certain whiffy aura.

From Wikipedia, the free encyclopedia

 

The Hawker Hunter is a transonic British jet-powered fighter aircraft that was developed by Hawker Aircraft for the Royal Air Force (RAF) during the late 1940s and early 1950s. It was designed to take advantage of the newly developed Rolls-Royce Avon turbojet engine and the swept wing, and was the first jet-powered aircraft produced by Hawker to be procured by the RAF. On 7 September 1953, the modified first prototype broke the world air speed record for aircraft, achieving a speed of 727.63 mph (1,171.01 km/h; 632.29 kn).

 

The single-seat "Hunter" was introduced to service in 1954 as a manoeuvrable day interceptor aircraft, quickly succeeding first-generation jet fighters in RAF service such as the Gloster "Meteor" and the de Havilland Venom. The all-weather/night fighter role was filled by the Gloster "Javelin". Successively improved variants of the type were produced, adopting increasingly more capable engine models and expanding its fuel capacity amongst other modifications being implemented. Hunters were also used by two RAF display teams: the "Black Arrows", who on one occasion looped a record-breaking 22 "Hunter's" in formation, and later the "Blue Diamonds", who flew 16 aircraft. The Hunter was also widely exported, serving with a total of 21 overseas air forces.

 

During the 1960s, following the introduction of the supersonic English Electric "Lightning" in the interceptor role, the Hunter transitioned to being operated as a fighter-bomber and for aerial reconnaissance missions, using dedicated variants for these purposes. Two-seat variants remained in use for training and secondary roles with the RAF and the Royal Navy until the early 1990s. Sixty years after its original introduction it was still in active service, being operated by the Lebanese Air Force until 2014.

 

The "Hunter" saw combat service in a range of conflicts with several operators, including the Suez Crisis, the Aden Emergency, the Sino-Indian War, the Indo-Pakistani War of 1965, the Indo-Pakistani War of 1971, the Rhodesian Bush War, the Second Congo War, the Six-Day War, the War of Attrition and the Yom Kippur War. Overall, 1,972 "Hunter's" were manufactured by Hawker Aircraft and its successor, Hawker Siddeley, as well as being produced under licence overseas. In British service, the Hunter was replaced in its principal roles by the Lightning, the Hawker Siddeley "Harrier" and the McDonnell Douglas F-4 "Phantom II".

  

Development

 

Origins

 

During 1945, the Second World War came to a close and a new postwar Labour government, headed by Clement Attlee, came to power in Britain. The incoming Attlee government's initial stance on defence was that no major conflict would occur for at least a decade, and thus there would be no need to develop or to procure any new aircraft until 1957. In accordance with this policy, aside from a small number of exceptions such as what would become the Hawker "Sea Hawk" for the Royal Navy, the majority of Specifications issued by the Air Ministry for fighter-sized aircraft during the late 1940s were restricted to research purposes. Aviation author Derek Wood refers to this policy as being: "a fatal error of judgement which was to cost Britain a complete generation of fighters and heavy bomber aircraft".

 

As the Cold War arose in the late 1940s, the RAF came to recognise that it would urgently require the development and procurement of fighters equipped with features such as swept wings. By this time, it had also become apparent that newly developed jet propulsion would form the future of fighter aircraft development. Many companies were quick to devise their own designs to harness this means of propulsion. Hawker Aviation's chief designer, Sydney Camm, had proposed the Hawker P.1040 for the RAF, but the demonstrator failed to interest them. Further modifications to the basic design resulted in the Hawker "Sea Hawk" carrier-based fighter. However, the "Sea Hawk" possessed a straight wing and was powered by the Rolls-Royce Nene turbojet engine, both features that rapidly became obsolete.

 

Seeking better performance and fulfilment of the Air Ministry Specification E.38/46, Sydney Camm designed the Hawker P.1052, which was essentially a "Sea Hawk" outfitted with a 35-degree swept wing. Performing its first flight in 1948, the P.1052 demonstrated good performance and conducted several carrier trials, but was ultimately determined to not warrant further development into a production aircraft. As a private venture, Hawker proceeded to convert the second P.1052 prototype into the Hawker P.1081 with swept tailplanes, a revised fuselage, and a single jet exhaust at the rear. On 19 June 1950, the P.1081 conducted its maiden flight, and was promising enough to draw interest from the Royal Australian Air Force (RAAF); however, further development was stalled by difficulties with the engine's reheat. In 1951, the sole P.1081 prototype was lost in a crash.

 

P.1067

In 1946, the British Air Ministry issued Specification F.43/46, which sought a daytime jet-powered interceptor aircraft. Camm promptly prepared a new design for a swept-winged fighter that would be powered by the upcoming Rolls-Royce Avon turbojet. The Avon's major advantage over the earlier Nene engine, as used in the earlier "Sea Hawk", was adoption of the axial compressor, which allowed for a much smaller engine diameter and provided greater thrust; this single engine gave roughly the same power as the two Rolls-Royce Derwents of the Gloster "Meteor's", a fighter aircraft that would be replaced by the envisioned new aircraft. In March 1948, the Air Ministry issued a revised Specification F.3/48, which demanded a speed of 629 mph (1,010 km/h) at 45,000 ft (13,700 m) and a high rate of climb, while carrying an armament of four 20 mm (0.79 in) or two 30 mm (1.18 in) cannon (rather than the large-calibre gun demanded by earlier specifications). Initially fitted with a single air intake in the nose and a T-tail, the project rapidly evolved into the more familiar Hunter shape. The intakes were moved to the wing roots to make room for weapons and radar in the nose, and a more conventional tail arrangement was devised as a result of stability concerns.

 

In 1950, the outbreak of the Korean War and Britain's heavy involvement in this conflict led to a flurry of orders being issued; the need for capable modern interceptors was felt to be so pressing that the RAF was willing to consider accepting interim fighter aircraft while more capable fighters would continue to be pursued. In particular, the RAF felt that a pair of proposed fighter aircraft from Hawker Aircraft and Supermarine were of high importance and thus placed orders for these proposed fighters 'off the drawing board' in 1950. The reasoning behind these two aircraft being ordered in 1950 was intended to serve as an insurance policy in the event of either one of these projects failing to produce a viable aircraft; these two aircraft would later become known as the Supermarine "Swift" and the Hawker "Hunter" respectively.

 

On 20 July 1951, the P.1067 made its maiden flight, flown by Neville Duke, from RAF Boscombe Down, powered by a single 6,500 lbf (28.91 kN) Avon 103 engine. The second prototype, which was fitted with production-standard avionics, armament and a 7,550 lbf (33.58 kN) Avon 107 turbojet, first flew on 5 May 1952. As an insurance against development problems on the part of the Avon engine, Hawker modified the design to accommodate another axial turbojet, the 8,000 lbf (35.59 kN) Armstrong Siddeley Sapphire 101. Fitted with a Sapphire, the third prototype flew on 30 November 1952.

 

On 16 March 1953, the first production standard "Hunter F.1", fitted with a single 7,600 lbf (33.80 kN) Avon 113 turbojet, made its first flight. The first 20 aircraft were, in effect, a pre-production series and featured a number of "one-off" modifications such as blown flaps and area ruled fuselage. On 7 September 1953, the sole "Hunter Mk 3" (the modified first prototype, WB 188) flown by Neville Duke broke the world air speed record for jet-powered aircraft, attaining a speed of 727.63 mph (1,171.01 km/h) over Littlehampton, West Sussex. This world record stood for less than three weeks before being broken on 25 September 1953 by the "Hunter's" early rival, the Supermarine "Swift", being flown by Michael Lithgow.

 

Design

 

Overview

 

The "Hunter" entered service with the Royal Air Force as an interceptor aircraft. It was the first jet aircraft produced by Hawker for the RAF. From the outset it was clear that the type had exceptional performance, being the first RAF aircraft capable of effectively matching the English Electric "Canberra" bomber. The "Hunter" also set numerous aviation records, including absolute speed records. The type was also lauded for its quick turnaround time – enabled by features such as its removable gun pack and pressurised fuelling system – and for its easy handling in flight.

 

The definitive version of the Hunter was the FGA.9, on which the majority of export versions were based. Although the Supermarine "Swift" had initially been politically favoured by the British Government, the "Hunter" proved far more successful, and had a lengthy service life with various operators, in part due to its low maintenance requirements and operating costs.

 

As the RAF received newer aircraft capable of supersonic speeds to perform the air interceptor role, many Hunters were modified and re-equipped for undertaking ground-attack and reconnaissance missions instead. "Hunter's" deemed surplus to the RAF's requirements were also quickly refurbished for continued service abroad. The "Hunter" would be procured by a considerable number of foreign nations. In addition to former RAF aircraft, roughly half of the nearly 2,000 "Hunter's" produced had been manufactured specifically for overseas customers. The "Hunter" would be in operational service with the RAF for over 30 years. As late as 1996, hundreds were still in active service with various operators across the world.

 

......................................................................................................................

 

From Wikipedia, the free encyclopedia

 

The Gloster "Meteor" was the first British jet fighter and the Allies' only jet aircraft to achieve combat operations during the Second World War. The "Meteor's" development was heavily reliant on its ground-breaking turbojet engines, pioneered by Sir Frank Whittle and his company, Power Jets Ltd. Development of the aircraft began in 1940, although work on the engines had been under way since 1936. The "Meteor" first flew in 1943 and commenced operations on 27 July 1944 with No. 616 Squadron RAF. The "Meteor" was not a sophisticated aircraft in its aerodynamics, but proved to be a successful combat fighter. Gloster's 1946 civil "Meteor F.4" demonstrator G-AIDC was the first civilian-registered jet aircraft in the world.

 

Several major variants of the "Meteor" incorporated technological advances during the 1940s and 1950s. Thousands of "Meteor's" were built to fly with the RAF and other air forces and remained in use for several decades. The "Meteor" saw limited action in the Second World War. "Meteor's" of the Royal Australian Air Force (RAAF) fought in the Korean War. Several other operators such as Argentina, Egypt and Israel flew "Meteor's" in later regional conflicts. Specialised variants of the "Meteor" were developed for use in photographic aerial reconnaissance and as night fighters.

 

The "Meteor" was also used for research and development purposes and to break several aviation records. On 7 November 1945, the first official airspeed record by a jet aircraft was set by a "Meteor F.3" at 606 miles per hour (975 km/h). In 1946, this record was broken when a "Meteor F.4" reached a speed of 616 miles per hour (991 km/h). Other performance-related records were broken in categories including flight time endurance, rate of climb, and speed. On 20 September 1945, a heavily modified "Meteor I", powered by two Rolls-Royce Trent turbine engines driving propellers, became the first turboprop aircraft to fly. On 10 February 1954, a specially adapted "Meteor F.8", the "Meteor Prone Pilot", which placed the pilot into a prone position to counteract inertial forces, took its first flight.

 

In the 1950s, the "Meteor" became increasingly obsolete as more nations introduced jet fighters, many of these newcomers having adopted a swept wing instead of the "Meteor's" conventional straight wing; in RAF service, the "Meteor" was replaced by newer types such as the Hawker "Hunter and Gloster "Javelin". As of 2018, two "Meteor's", G-JSMA and G-JWMA, remain in active service with the Martin-Baker company as ejection seat testbeds. One further aircraft in the UK remains airworthy, as does another in Australia.

  

Development

 

Origins

 

The development of the turbojet-powered Gloster "Meteor" was a collaboration between the Gloster Aircraft Company and Sir Frank Whittle's firm, Power Jets Ltd. Whittle formed Power Jets Ltd in March 1936 to develop his ideas of jet propulsion, Whittle himself serving as the company's chief engineer. For several years, attracting financial backers and aviation firms prepared to take on Whittle's radical ideas was difficult; in 1931, Armstrong-Siddeley had evaluated and rejected Whittle's proposal, finding it to be technically sound but at the limits of engineering capability. Securing funding was a persistently worrying issue throughout the early development of the engine. The first Whittle prototype jet engine, the Power Jets WU, began running trials in early 1937; shortly afterwards, both Sir Henry Tizard, chairman of the Aeronautical Research Committee, and the Air Ministry gave the project their support.

 

On 28 April 1939, Whittle made a visit to the premises of the Gloster Aircraft Company, where he met several key figures, such as George Carter, Gloster's chief designer. Carter took a keen interest in Whittle's project, particularly when he saw the operational Power Jets W.1 engine; Carter quickly made several rough proposals of various aircraft designs powered by the engine. Independently, Whittle had also been producing several proposals for a high-altitude jet-powered bomber; following the start of the Second World War and the Battle for France, a greater national emphasis on fighter aircraft arose. Power Jets and Gloster quickly formed a mutual understanding around mid-1939.

 

In spite of ongoing infighting between Power Jets and several of its stakeholders, the Air Ministry contracted Gloster in late 1939 to manufacture a prototype aircraft powered by one of Whittle's new turbojet engines. The single-engined proof-of-concept Gloster E28/39, the first British jet-powered aircraft, conducted its maiden flight on 15 May 1941, flown by Gloster's chief test pilot, Flight Lieutenant Philip "Gerry" Sayer. The success of the E.28/39 proved the viability of jet propulsion, and Gloster pressed ahead with designs for a production fighter aircraft. Due to the limited thrust available from early jet engines, it was decided that subsequent production aircraft would be powered by a pair of turbojet engines.

 

In 1940, for a "military load" of 1,500 lb (680 kg), the Royal Aircraft Establishment (RAE) had advised that work on an aircraft of 8,500 lb (3,900 kg) all-up weight, with a total static thrust of 3,200 lbf (14 kN) should be started, with an 11,000 lb (5,000 kg) design for the expected, more powerful, W.2 and axial engine designs. George Carter's calculations based on the RAE work and his own investigations was that a 8,700-to-9,000-pound (3,900-to-4,100-kilogram) aircraft with two or four 20 mm cannons and six 0.303 machine guns would have a top speed of 400–431 miles per hour (644–694 km/h) at sea level and 450–470 miles per hour (720–760 km/h) at 30,000 feet (9,100 m). In January 1941 Gloster were told by Lord Beaverbrook that the twin jet fighter was of "unique importance", and that the company was to stop work on a night-fighter development of their F.9/37 to Specification F.18/40.

 

Prototypes

 

In August 1940, Carter presented Gloster's initial proposals for a twin-engined jet fighter with a tricycle undercarriage. On 7 February 1941, Gloster received an order for twelve prototypes (later reduced to eight) under Specification F9/40. A letter of intent for the production of 300 of the new fighter, initially to be named Thunderbolt, was issued on 21 June 1941; to avoid confusion with the USAAF Republic P-47 "Thunderbolt" which had been issued with the same name to the RAF in 1944, the aircraft's name was subsequently changed to Meteor. During the aircraft's secretive development, employees and officials made use of the codename Rampage to refer to the "Meteor", as similarly the de Havilland "Vampire" would initially be referred to as the "Spider Crab". Test locations and other key project information was similarly obscured.

 

Although taxiing trials were carried out in 1942, it was not until the following year that any flights took place due to production and approval holdups with the Power Jets W.2 engine powering the "Meteor". Due to the delays at subcontractor Rover, who was struggling to manufacture the W.2 engines on schedule, on 26 November 1942, production of the "Meteor" was ordered to stop; considerable interest was shown in Gloster's E.1/44 proposal for a single-engine fighter, unofficially named Ace. Gloster continued development work on the "Meteor" and the production-stop order was overturned in favour of the construction of six (later increased to eight) F9/40 prototypes alongside three E.1/44 prototypes. Rover's responsibilities for development and production of the W.2B engine were also transferred to Rolls-Royce that year.

 

On 5 March 1943, the fifth prototype, serial DG206, powered by two substituted de Havilland Halford H.1 engines owing to problems with the intended W.2 engines, became the first "Meteor" to become airborne at RAF Cranwell, piloted by Michael Daunt. On the initial flight, an uncontrollable yawing motion was discovered, which led to a redesigned larger rudder; however, no difficulties had been attributed to the groundbreaking turbojet propulsion. Only two prototypes flew with de Havilland engines because of the low flight endurance they were capable of providing. Before the first prototype aircraft had even undertaken its first flight, an extended order for 100 production-standard aircraft had already been placed by the RAF.

 

The first Whittle-engined aircraft, DG205/G, flew on 12 June 1943 (later crashing during takeoff on 27 April 1944) and was followed by DG202/G on 24 July. DG202/G was later used for deck handling tests aboard aircraft carrier HMS Pretoria Castle. DG203/G made its first flight on 9 November 1943, later becoming a ground instructional airframe. DG204/G, powered by Metrovick F.2 engines, first flew on 13 November 1943; DG204/G was lost in an accident on 4 January 1944, the cause believed to have been an engine compressor failure due to overspeed. DG208/G made its début on 20 January 1944, by which time the majority of design problems had been overcome and a production design had been approved. DG209/G was used as an engine testbed by Rolls-Royce, first flying on 18 April 1944. DG207/G was intended to be the basis for the "Meteor F.2" with de Havilland engines, but it did not fly until 24 July 1945, at which time the "Meteor 3" was in full production and de Havilland's attention was being redirected to the incoming de Havilland "Vampire", thus the F.2 was cancelled.

  

Into production

 

On 12 January 1944, the first "Meteor F.1", serial EE210/G, took to the air from Moreton Valence. It was essentially identical to the F9/40 prototypes except for the addition of four nose-mounted 20 mm (.79 in) Hispano Mk V cannons and some changes to the canopy to improve all-round visibility. Due to the F.1's similarity to the prototypes, they were frequently operated in the test program to progress British understanding of jet propulsion, and it took until July 1944 for the aircraft to enter squadron service. EE210/G was later sent to the U.S. for evaluation in exchange for a pre-production Bell XP-59A "Airacomet", the "Meteor" being flown first by John Grierson at Muroc Army Airfield on 15 April 1944.

 

Originally 300 F.1s were ordered, but the total produced was reduced to 20 aircraft as the follow-on orders had been converted to the more advanced models. Some of the last major refinements to the "Meteor's" early design were trialled using this first production batch, and what was to become the long-term design of the engine nacelles was introduced upon EE211. The original nacelles had been discovered by the RAE to suffer from compressibility buffeting at higher speeds, causing increased drag, and the re-designed longer nacelles eliminated this and provided an increase in the "Meteor's" maximum speed. The lengthened nacelles were introduced on the final fifteen "Meteor III's". EE215 was the first "Meteor" to be fitted with guns; EE215 was also used in engine reheat trials, the addition of reheat increasing top speed from 420 mph to 460 mph. and was later converted into the first two-seat "Meteor". Due to the radical differences between jet-powered aircraft and those that preceded, to prepare the "Meteor" for squadron service, led by Group Captain Hugh Joseph Wilson. The Tactical Flight was formed at Farnborough in May 1944, the first "Meteor's" arriving the following month, upon which both tactical applications and limitations were extensively explored.

 

On 17 July 1944, the "Meteor F.1" was cleared for service use. Shortly afterwards, elements of the Tactical Flight and their aircraft were transferred to operational RAF squadrons. The first deliveries to No. 616 Squadron RAF, the first operational squadron to receive the "Meteor", began in July 1944. When the F.2 was cancelled, the "Meteor F.3" became the immediate successor to the F.1 and alleviated some of the shortcomings of the F.1. In August 1944, the first F.3 prototype flew; early F.3 production aircraft were still fitted with the Welland engine as the Derwent engine's production line was only just starting at this point. A total of 210 F.3 aircraft were produced before they were in turn superseded by production of the "Meteor F.4" in 1945.

 

Several "Meteor F.3"s were converted into navalised aircraft. The adaptations included a strengthened undercarriage and arrester hook. Operational trials of the type took place aboard HMS Implacable. The trials included carrier landings and takeoffs. Performance of these naval prototype "Meteor's" proved to be favourable, including takeoff performance, leading to further trials with a modified "Meteor F.4" fitted with folding wings; a 'clipped wing' was also adopted. The "Meteor" later entered service with the Royal Navy, but only as a land-based trainer, the "Meteor T.7", to prepare pilots of the Fleet Air Arm for flying other jet aircraft such as the de Havilland "Sea Vampire".

 

While various marks of "Meteor" had been introduced by 1948, they had remained very similar to the prototypes of the "Meteor"; consequently, the performance of the "Meteor F.4" was beginning to be eclipsed by new jet designs. Gloster therefore embarked on a redesign programme to produce a new version of the "Meteor" with better performance. Designated "Meteor F.8", this upgraded variant was a potent fighter aircraft, forming the bulk of RAF Fighter Command between 1950 and 1955. The "Meteor" continued to be operated in a military capacity by several nations into the 1960s.

 

Night fighter

 

To replace the increasingly obsolete de Havilland "Mosquito" as a night fighter, the "Meteor" was adapted to serve in the role as an interim aircraft. Gloster had initially proposed a night fighter design to meet the Air Ministry specification for the "Mosquito" replacement, based on the two seater trainer variant of the "Meteor", with the pilot in the front seat and the navigator in the rear. Once accepted however, work on the project was swiftly transferred to Armstrong Whitworth to perform both the detailed design process and production of the type; the first prototype flew on 31 May 1950. Although based on the T.7 twin seater, it used the fuselage and tail of the F.8, and the longer wings of the F.3. An extended nose contained the AI Mk 10 (the 1940s Westinghouse SCR-720) Air Intercept radar. As a consequence the 20 mm cannons were moved into the wings, outboard of the engines. A ventral fuel tank and wing mounted drop tanks completed the Armstrong Whitworth "Meteor NF.11".

 

As radar technology developed, a new "Meteor" night fighter was developed to use the improved US-built APS-21 system. The NF.12 first flew on 21 April 1953. It was similar to the NF 11 but had a nose section 17 inches (43 cm) longer; the fin was enlarged to compensate for the greater keel area of the enlarged nose and to counter the airframe reaction to the "wig-wag" scan of the radar which affected the gunsighting, an anti-tramp motor operating on the rudder was fitted midway up the front leading edge of the fin. The NF.12 also had the new Rolls-Royce Derwent 9 engines and the wings were reinforced to handle the new engine. Deliveries of the NF.12 started in 1953, with the type entering squadron service in early 1954, equipping seven squadrons (Nos 85, 25, 152, 46, 72, 153 and 64); the aircraft was replaced over 1958–1959.

 

The final "Meteor" night fighter was the NF.14. First flown on 23 October 1953, the NF.14 was based on the NF.12 but had an even longer nose, extended by a further 17 inches to accommodate new equipment, increasing the total length to 51 ft 4 in (15.65 m) and a larger bubble canopy to replace the framed T.7 version. Just 100 NF.14s were built; they first entered service in February 1954 beginning with No. 25 Squadron and were being replaced as early as 1956 with the Gloster "Javelin". Overseas, they remained in service a little longer, serving with No. 60 Squadron at Tengah, Singapore until 1961. As the NF.14 was replaced, some 14 were converted to training aircraft as the NF(T).14 and given to No. 2 Air Navigation School on RAF Thorney Island until transferring to No. 1 Air Navigation School at RAF Stradishall where they served until 1965.

 

Design

 

Overview

 

The first operational version of the "Meteor", designated as the "Meteor F.1", apart from the minor airframe refinements, was a straightforward 'militarisation' of the earlier F9/40 prototypes. The dimensions of the standard "Meteor F.1" were 41 ft 3 in (12.57 m) long with a span of 43 ft 0 in (13.11 m), with an empty weight of 8,140 lb (3,690 kg) and a maximum takeoff weight of 13,795 lb (6,257 kg). Despite the revolutionary turbojet propulsion used, the design of the "Meteor" was relatively orthodox and did not take advantage of many aerodynamic features used on other, later jet fighters, such as swept wings; the "Meteor" shared a broadly similar basic configuration to its German equivalent, the Messerschmitt "Me 262", which was also aerodynamically conventional.

 

It was an all-metal aircraft with a tricycle undercarriage and conventional low, straight wings with mid-mounted turbojet engines and a high-mounted tailplane clear of the jet exhaust. The "Meteor F.1" exhibited some problematic flying characteristics typical of early jet aircraft; it suffered from stability problems at high transonic speeds, large trim changes, high stick forces and self-sustained yaw instability (snaking) caused by airflow separation over the thick tail surfaces. The longer fuselage of the "Meteor T.7", a two-seater trainer, significantly reduced the aerodynamic instability that the early "Meteor's" were known for.

 

Later "Meteor" variants would see a large variety of changes from the initial "Meteor F.1" introduced to service in 1944. Much attention was given to raising the aircraft's top speed, often by improving the airframe's aerodynamic qualities, incorporating the latest engine developments, and increasing the strength of the airframe. The "Meteor F.8", which emerged in the late 1940s, was considered to have substantially improved performance over prior variants; the F.8 was reportedly the most powerful single-seat aircraft flying in 1947, capable of ascending to 40,000 feet (12,000 m) within five minutes.

 

Construction

 

From the outset, each "Meteor" was constructed from several modular sections or separately produced units, a deliberate design choice to allow for production to be dispersed and for easy disassembly for transport. Each aircraft comprised five main sections: nose, forward fuselage, central section, rear fuselage and tail units; the wings were also built out of lengthwise sections. The forward section contained the pressure cabin, gun compartments, and forward undercarriage. The centre section incorporated much of the structural elements, including the inner wing, engine nacelles, fuel tank, ammunition drums, and main undercarriage. The rear fuselage was of a conventional semi-monocoque structure. Various aluminium alloys were the primary materials used throughout the structure of the "Meteor", such as the stressed duralumin skin.

 

Across the "Meteor's" production life, various different companies were subcontracted to manufacture aircraft sections and major components; due to the wartime workload on producing fighter aircraft such as the Hawker "Hurricane" and Hawker "Typhoon", neither Gloster nor the wider Hawker Siddeley Group were able to internally meet the production demand of 80 aircraft per month. Bristol Tramways produced the forward fuselage of the aircraft, the Standard Motor Company manufactured the central fuselage and inner wing sections, the Pressed Steel Company produced the rear fuselage, and Parnall Aircraft made the tail unit. Other main subcontractors included Boulton Paul Aircraft, Excelsior Motor Radiator Company, Bell Punch, Turner Manufacturing Company, and Charlesworth Bodies; as many of these firms had little or no experience producing aircraft, both quality and interchangeability of components were maintained by contractually enforced adherence to Gloster's original drawings.

 

From the "Meteor F.4" onwards, Armstrong Whitworth began completing whole units at their Coventry facility in addition to Gloster's own production line. Belgian aviation firm Avions Fairey would also produce the "Meteor F.8" under licence from Gloster for the Belgian Air Force; a similar licence manufacturing arrangement was made with Dutch company Fokker to meet the Royal Netherlands Air Force's order.

 

Engines

 

The "Meteor F.1" was powered by two Rolls-Royce Welland turbojet engines, Britain's first production jet engines, which were built under licence from Whittle's designs. The "Meteor" embodied the advent of practical jet propulsion; in the type's service life, both military and civil aviation manufacturers would rapidly integrate turbine engines into their designs, favouring its advantages such as smoother running and greater power output. The "Meteor's" engines were considerably more practical than those of the German "Me 262", as unlike the "Me 262", the engines were embedded into the wing in nacelles between the front and rear spars rather than underslung, and thus saving some weight due to shorter landing gear legs and less massive spars.

 

The W.2B/23C engines upon which the Welland was based produced 1,700 lbf (7.6 kN) of thrust each, giving the aircraft a maximum speed of 417 mph (671 km/h) at 9,800 feet (3,000 m) and a range of 1,000 miles (1,600 km). It incorporated a hydraulically driven engine starter developed by Rolls-Royce, which was automated following the press of a starter button in the cockpit. The engines also drove hydraulic and vacuum pumps as well as a generator via a Rotol gearbox fixed on the forward wing spar; the cockpit was also heated by bleed air from one of the engines. The acceleration rate of the engines was manually controlled by the pilot; rapid engine acceleration would frequently induce compressor stalls early on; the likelihood of compressor stalls was effectively eliminated upon further design refinements of both the Welland engine and the "Meteor" itself. At high speeds, the "Meteor" had a tendency to lose directional stability, often during unfavourable weather conditions, leading to a 'snaking' motion; this could be easily resolved by throttling back to reduce speed.

 

Based upon designs produced by Power Jets, Rolls-Royce produced more advanced and powerful turbojet engines. Beyond numerous improvements made to the Welland engine that powered the early "Meteor's", Rolls-Royce and Power Jets collaborated to develop the more capable Derwent engine, which as the Rover B.26 had undergone a radical re-design from the W.2B/500 while at Rover. The Derwent engine, and the re-designed Derwent V based on the Nene, was installed on many of the later production "Meteor's", the adoption of this new powerplant led to considerable performance increases. The "Meteor" often served as the basis for the development of other early turbojet designs; a pair of "Meteor F.4s" were sent to Rolls-Royce to aid in their experimental engine trials, RA435 being used for reheat testing, and RA491 being fitted with the Rolls-Royce Avon, an axial-flow engine. From their involvement in the development of the "Meteor's" engines, Armstrong-Siddeley, Bristol Aircraft, Metropolitan-Vickers, and de Havilland would also independently develop their own gas turbine engines.

 

Performance

 

During development, sceptical elements of the Air Ministry had expected mature piston-powered aircraft types to exceed the capabilities of the "Meteor" in all respects except that of speed; thus, the performance of early "Meteor's" was considered favourable for the interceptor mission, being capable of out-diving the majority of enemy aircraft. The conclusion of in-service trials conducted between the "Meteor F.3." and the Hawker "Tempest V" was that the performance of the "Meteor" exceeded the "Tempest" in almost all respects and that, barring some manoeuvrability issues, the "Meteor" could be considered a capable all-round fighter. Pilots formerly flying piston-engine aircraft often described the "Meteor" as being exciting to fly. Ex-RAF pilot Norman Tebbit stated of his experience of the "Meteor": "Get airborne, up with the wheels, hold it low until you were about 380 knots, pull it up and she would go up, well we thought then, like a rocket".

 

As a general rule, the jet engine consumes more fuel than its piston-engine counterparts; the fuel-hungry Welland engines imposed considerable limitations on the "Meteor F.1", leading to the type being used for local interception duties only. In the post-war environment, there was considerable pressure to increase the range of interceptors to counter the threat of bombers armed with nuclear weapons. The long-term answer to this question was in-flight refuelling; several "Meteor's" were provided to Flight Refuelling Limited for trials of the newly developed probe-and-drogue refuelling techniques. This capability was not rolled out to service "Meteor's", having already been supplanted by more modern interceptor aircraft at this point.

 

In May 1951, it was reported that the "Meteor 4's" tail unit lost half its strength when the skin tore. The skin tearing was found to originate at rivet holes, access panels or discontinuous stringers (stress risers) due to metal fatigue.

 

A total of 890 "Meteor's" were lost in RAF service (145 of these crashes occurring in 1953 alone), resulting in the deaths of 450 pilots. Contributory factors in the number of crashes were the poor brakes, failure of the landing gear, the high fuel consumption and consequent short flight endurance (less than one hour), causing pilots to run out of fuel, and difficult handling with one engine out due to the widely set engines. The casualty rate was exacerbated by the lack of ejection seats in early series "Meteor's"; the ground-breaking high speed that the aircraft was capable of meant that, during the bailing out process, pilots were typically subject to high g forces hindering movement and the effect of slipstream winds; there was also a greater likelihood of the pilot striking the horizontal tailplane. Ejection seats were fitted in the later F.8, FR.9, PR.10 and some experimental "Meteor's". The difficulty of bailing out of the Meteor has been noted by pilots during development, reporting several contributing design factors such as the limited size and relative position of the cockpit to the rest of the aircraft, and difficulty in using the two-lever jettisonable hood mechanism.

I am capable of posting something other than Norway...

 

This is the Philadelphia instantiation of The Thinker. On a related note, the art scene in Philadelphia is fantastic. If you've never been, there is much to see, including the wonderful Art Museum(s).

 

More Norway coming up.... ;)

 

Thanks for looking!

 

_________________________________________________

Comments and constructive criticism always appreciated.

Stream on Black....Follow on Facebook....My Profile (to get to webpage)

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

The CAC Sabre, sometimes known as the Avon Sabre or CA-27, was an Australian variant of the North American Aviation F-86F Sabre fighter aircraft. In 1951, Commonwealth Aircraft Corporation obtained a license agreement to build the F-86F Sabre. In a major departure from the North American blueprint, it was decided that the CA-27 would be powered by a license-built version of the Rolls-Royce Avon R.A.7, rather than the General Electric J47. In theory, the Avon was capable of more than double the maximum thrust and double the thrust-to-weight ratio of the US engine. This necessitated a re-design of the fuselage, as the Avon was shorter, wider and lighter than the J47.

 

To accommodate the Avon, over 60 percent of the fuselage was altered and there was a 25 percent increase in the size of the air intake. Another major revision was in replacing the F-86F's six machine guns with two 30mm ADEN cannon, while other changes were also made to the cockpit and to provide an increased fuel capacity.

 

The prototype aircraft first flew on 3 August 1953. The production aircrafts' first deliveries to the Royal Australian Air Force began in 1954. The first batch of aircraft were powered by the Avon 20 engine and were designated the Sabre Mk 30. Between 1957 and 1958 this batch had the wing slats removed and were re-designated Sabre Mk 31. These Sabres were supplemented by 20 new-built aircraft. The last batch of aircraft were designated Sabre Mk 32 and used the Avon 26 engine, of which 69 were built up to 1961.

 

Beyond these land-based versions, an indigenous version for carrier operations had been developed and built in small numbers, too, the Sea Sabre Mk 40 and 41. The roots of this aircraft, which was rather a prestigious idea than a sensible project, could be traced back to the immediate post WWII era. A review by the Australian Government's Defence Committee recommended that the post-war forces of the RAN be structured around a Task Force incorporating multiple aircraft carriers. Initial plans were for three carriers, with two active and a third in reserve, although funding cuts led to the purchase of only two carriers in June 1947: Majestic and sister ship HMS Terrible, for the combined cost of AU£2.75 million, plus stores, fuel, and ammunition. As Terrible was the closer of the two ships to completion, she was finished without modification, and was commissioned into the RAN on 16 December 1948 as HMAS Sydney. Work progressed on Majestic at a slower rate, as she was upgraded with the latest technology and equipment. To cover Majestic's absence, the Colossus-class carrier HMS Vengeance was loaned to the RAN from 13 November 1952 until 12 August 1955.

 

Labour difficulties, late delivery of equipment, additional requirements for Australian operations, and the prioritization of merchant ships over naval construction delayed the completion of Majestic. Incorporation of new systems and enhancements caused the cost of the RAN carrier acquisition program to increase to AU£8.3 million. Construction and fitting out did not finish until October 1955. As the carrier neared completion, a commissioning crew was formed in Australia and first used to return Vengeance to the United Kingdom.

The completed carrier was commissioned into the RAN as HMAS Majestic on 26 October 1955, but only two days later, the ship was renamed Melbourne and recommissioned.

 

In the meantime, the rather political decision had been made to equip Melbourne with an indigenous jet-powered aircraft, replacing the piston-driven Hawker Fury that had been successfully operated from HMAS Sydney and HMAS Vengeance, so that the "new jet age" was even more recognizable. The choice fell on the CAC Sabre, certainly inspired by North American's successful contemporary development of the navalized FJ-2 Fury from the land-based F-86 Sabre. The CAC 27 was already a proven design, and with its more powerful Avon engine it even offered a better suitability for carrier operations than the FJ-2 with its rather weak J47 engine.

 

Work on this project, which was initially simply designated Sabre Mk 40, started in 1954, just when the first CAC 27's were delivered to operative RAAF units. While the navalized Avon Sabre differed outwardly only little from its land-based brethren, many details were changed and locally developed. Therefore, there was also, beyond the general outlines, little in common with the North American FJ-2 an -3 Fury.

Externally, a completely new wing with a folding mechanism was fitted. It was based on the F-86's so-called "6-3" wing, with a leading edge that was extended 6 inches at the root and 3 inches at the tip. This modification enhanced maneuverability at the expense of a small increase in landing speed due to deletion of the leading edge slats, a detail that was later introduced on the Sabre Mk 31, too. As a side benefit, the new wing leading edges without the slat mechanisms held extra fuel. However, the Mk 40's wing was different as camber was applied to the underside of the leading edge to improve low-speed handling for carrier operations. The wings were provided with four stations outboard of the landing gear wells for up to 1000 lb external loads on the inboard stations and 500 lb on the outboard stations.

 

Slightly larger stabilizers were fitted and the landing gear was strengthened, including a longer front wheel strut. The latter necessitated an enlarged front wheel well, so that the front leg’s attachment point had to be moved forward. A ventral launch cable hook was added under the wing roots and an external massive arrester hook under the rear fuselage.

Internally, systems were protected against salt and humidity and a Rolls-Royce Avon 211 turbojet was fitted, a downrated variant of the already navalized Avon 208 from the British DH Sea Vixen, but adapted to the different CAC 27 airframe and delivering 8.000 lbf (35.5 kN) thrust – slightly more than the engines of the land-based CAC Sabres, but also without an afterburner.

 

A single Mk 40 prototype was built from a new CAC 27 airframe taken directly from the production line in early 1955 and made its maiden flight on August 20th of the same year. In order to reflect its naval nature and its ancestry, this new CAC 27 variant was officially christened “Sea Sabre”.

Even though the modified machine handled well, and the new, cambered wing proved to be effective, many minor technical flaws were discovered and delayed the aircraft's development until 1957. These included the wing folding mechanism and the respective fuel plumbing connections, the landing gear, which had to be beefed up even more for hard carrier landings and the airframe’s structural strength for catapult launches, esp. around the ventral launch hook.

 

In the meantime, work on the land-based CAC 27 progressed in parallel, too, and innovations that led to the Mk 31 and 32 were also incorporated into the naval Mk 40, leading to the Sea Sabre Mk 41, which became the effective production aircraft. These updates included, among others, a detachable (but fixed) refueling probe under the starboard wing, two more pylons for light loads located under the wing roots and the capability to carry and deploy IR-guided AIM-9 Sidewinder air-to-air missiles, what significantly increased the Mk 41's efficiency as day fighter. With all these constant changes it took until April 1958 that the Sabre Mk 41, after a second prototype had been directly built to the new standard, was finally approved and cleared for production. Upon delivery, the RAN Sea Sabres carried a standard NATO paint scheme with Extra Dark Sea Grey upper surfaces and Sky undersides.

 

In the meantime, the political enthusiasm concerning the Australian carrier fleet had waned, so that only twenty-two aircraft were ordered. The reason behind this decision was that Australia’s carrier fleet and its capacity had become severely reduced: Following the first decommissioning of HMAS Sydney in 1958, Melbourne became the only aircraft carrier in Australian service, and she was unavailable to provide air cover for the RAN for up to four months in every year; this time was required for refits, refueling, personnel leave, and non-carrier duties, such as the transportation of troops or aircraft. Although one of the largest ships to serve in the RAN, Melbourne was one of the smallest carriers to operate in the post-World War II period, so that its contribution to military actions was rather limited. To make matters worse, a decision was made in 1959 to restrict Melbourne's role to helicopter operations only, rendering any carrier-based aircraft in Australian service obsolete. However, this decision was reversed shortly before its planned 1963 implementation, but Australia’s fleet of carrier-borne fixed-wing aircraft would not grow to proportions envisioned 10 years ago.

 

Nevertheless, on 10 November 1964, an AU£212 million increase in defense spending included the purchase of new aircraft for Melbourne. The RAN planned to acquire 14 Grumman S-2E Tracker anti-submarine aircraft and to modernize Melbourne to operate these. The acquisition of 18 new fighter-bombers was suggested (either Sea Sabre Mk 41s or the American Douglas A-4 Skyhawk), too, but these were dropped from the initial plan. A separate proposal to order 10 A-4G Skyhawks, a variant of the Skyhawk designed specifically for the RAN and optimized for air defense, was approved in 1965, but the new aircraft did not fly from Melbourne until the conclusion of her refit in 1969. This move, however, precluded the production of any new and further Sea Sabre.

 

At that time, the RAN Sea Sabres received a new livery in US Navy style, with upper surfaces in Light Gull Gray with white undersides. The CAC Sea Sabres remained the main day fighter and attack aircraft for the RAN, after the vintage Sea Furies had been retired in 1962. The other contemporary RAN fighter type in service, the Sea Venom FAW.53 all-weather fighter that had replaced the Furies, already showed its obsolescence.

In 1969, the RAN purchased another ten A-4G Skyhawks, primarily in order to replace the Sea Venoms on the carriers, instead of the proposed seventh and eighth Oberon-class submarines. These were operated together with the Sea Sabres in mixed units on board of Melbourne and from land bases, e.g. from NAS Nowra in New South Wales, where a number of Sea Sabres were also allocated to 724 Squadron for operational training.

 

Around 1970, Melbourne operated a standard air group of four jet aircraft, six Trackers, and ten Wessex helicopters until 1972, when the Wessexes were replaced with ten Westland Sea King anti-submarine warfare helicopters and the number of jet fighters doubled. Even though the A-4G’s more and more took over the operational duties on board of Melbourne, the Sea Sabres were still frequently deployed on the carrier, too, until the early Eighties, when both the Skyhawks and the Sea Sabres received once more a new camouflage, this time a wraparound scheme in two shades of grey, reflecting their primary airspace defense mission.

 

The CAC 27 Mk 41s’ last carrier operations took place in 1981 in the course of Melbourne’s involvements in two major exercises, Sea Hawk and Kangaroo 81, the ship’s final missions at sea. After Melbourne was decommissioned in 1984, the Fleet Air Arm ceased fixed-wing combat aircraft operation. This was the operational end of the Sabre Mk 41, which had reached the end of their airframe lifetime, and the Sea Sabre fleet had, during its career, severely suffered from accidents and losses: upon retirement, only eight of the original twenty-two aircraft still existed in flightworthy condition, so that the aircraft were all scrapped. The younger RAN A-4Gs were eventually sold to New Zealand, where they were kept in service until 2002.

  

General characteristics:

Crew: 1

Length: 37 ft 6 in (11.43 m)

Wingspan: 37 ft 1 in (11.3 m)

Height: 14 ft 5 in (4.39 m)

Wing area: 302.3 sq ft (28.1 m²)

Empty weight: 12,000 lb (5,443 kg)

Loaded weight: 16,000 lb (7,256 kg)

Max. takeoff weight: 21,210 lb (9,621 kg)

 

Powerplant:

1× Rolls-Royce Avon 208A turbojet engine with 8,200 lbf (36.44 kN)

 

Performance:

Maximum speed: 700 mph (1,100 km/h) (605 knots)

Range: 1,153 mi, (1,000 NM, 1,850 km)

Service ceiling: 52,000 ft (15,850 m)

Rate of climb: 12,000 ft/min at sea level (61 m/s)

 

Armament:

2× 30 mm ADEN cannons with 150 rounds per gun

5,300 lb (2,400 kg) of payload on six external hardpoints;

Bombs were usually mounted on outer two pylons as the mid pair were wet-plumbed pylons for

2× 200 gallons drop tanks, while the inner pair was usually occupied by a pair of AIM-9 Sidewinder

AAMs

A wide variety of bombs could be carried with maximum standard loadout being 2x 1,000 lb bombs

or 2x Matra pods with unguided SURA missiles plus 2 drop tanks for ground attacks, or 2x AIM-9 plus

two drop tanks as day fighter

  

The kit and its assembly:

This project was initially inspired by a set of decals from an ESCI A-4G which I had bought in a lot – I wondered if I could use it for a submission to the “In the navy” group build at whatifmodelers.com in early 2020. I considered an FJ-3M in Australian colors on this basis and had stashed away a Sword kit of that aircraft for this purpose. However, I had already built an FJ variant for the GB (a kitbashed mix of an F-86D and an FJ-4B in USMC colors), and was reluctant to add another Fury.

 

This spontaneously changed after (thanks to Corona virus quarantine…) I cleaned up one of my kit hoards and found a conversion set for a 1:72 CAC 27 from JAYS Model Kits which I had bought eons ago without a concrete plan. That was the eventual trigger to spin the RAN Fury idea further – why not a navalized version of the Avon Sabre for HMAS Melbourne?

 

The result is either another kitbash or a highly modified FJ-3M from Sword. The JAYS Model Kits set comes with a THICK sprue that carries two fuselage halves and an air intake, and it also offers a vacu canopy as a thin fallback option because the set is actually intended to be used together with a Hobby Craft F-86F.

 

While the parts, molded in a somewhat waxy and brittle styrene, look crude on the massive sprue, the fuselage halves come with very fine recessed engravings. And once you have cleaned the parts (NOTHING for people faint at heart, a mini drill with a saw blade is highly recommended), their fit is surprisingly good. The air intake was so exact that no putty was needed to blend it with the rest of the fuselage.

 

The rest came from the Sword kit and integrating the parts into the CAC 27 fuselage went more smoothly than expected. For instance, the FJ-3M comes with a nice cockpit tub that also holds a full air intake duct. Thanks to the slightly wider fuselage of the CAC 27, it could be mounted into the new fuselage halves without problems and the intake duct almost perfectly matches the intake frame from the conversion set. The tailpipe could be easily integrated without any mods, too. The fins had to be glued directly to the fuselage – but this is the way how the Sword kit is actually constructed! Even the FJ-3M’s wings match the different fuselage perfectly. The only modifications I had to make is a slight enlargement of the ventral wing opening at the front and at the read in order to take the deeper wing element from the Sword kit, but that was an easy task. Once in place, the parts blend almost perfectly into each other, just minor PSR was necessary to hide the seams!

 

Other mods include an extended front wheel well for the longer leg from the FJ-3M and a scratched arrester hook installation, made from wire, which is on purpose different from the Y-shaped hook of the Furies.

 

For the canopy I relied on the vacu piece that came with the JAYS set. Fitting it was not easy, though, it took some PSR to blend the windscreen into the rest of the fuselage. Not perfect, but O.K. for such a solution from a conversion set.

 

The underwing pylons were taken from the Sword kit, including the early Sidewinders. I just replaced the drop tanks – the OOB tanks are very wide, and even though they might be authentic for the FJ-3, I was skeptical if they fit at all under the wings with the landing gear extended? In order to avoid trouble and for a more modern look, I replaced them outright with more slender tanks, which were to mimic A-4 tanks (USN FJ-4s frequently carried Skyhawk tanks). They actually come from a Revell F-16 kit, with modified fins. The refueling probe comes from the Sword kit.

 

A last word about the Sword kit: much light, but also much shadow. While I appreciate the fine surface engravings, the recognizably cambered wings, a detailed cockpit with a two-piece resin seat and a pretty landing gear as well as the long air intake, I wonder why the creators totally failed to provide ANY detail of the arrester hook (there is literally nothing, as if this was a land-based Sabre variant!?) or went for doubtful solutions like a front landing gear that consists of five(!) single, tiny parts? Sadism? The resin seat was also broken (despite being packed in a seperate bag), and it did not fit into the cockpit tub at all. Meh!

  

Painting and markings:

From the start I planned to give the model the late RAN A-4Gs’ unique air superiority paint scheme, which was AFAIK introduced in the late Seventies: a two-tone wraparound scheme consisting of “Light Admiralty Grey” (BS381C 697) and “Aircraft Grey” (BS 381C 693). Quite simple, but finding suitable paints was not an easy task, and I based my choice on pictures of the real aircraft (esp. from "buzz" number 880 at the Fleet Air Arm Museum, you find pics of it with very good light condition) rather than rely on (pretty doubtful if not contradictive) recommendations in various painting instructions from models or decal sets.

 

I wanted to keep things simple and settled upon Dark Gull Grey (FS 36231) and Light Blue (FS 35414), both enamel colors from Modelmaster, since both are rather dull interpretations of these tones. Esp. the Light Blue comes quite close to Light Admiralty Grey, even though it should be lighter for more contrast to the darker grey tone. But it has that subtle greenish touch of the original BS tone, and I did not want to mix the colors.

 

The pattern was adapted from the late A-4Gs’ scheme, and the colors were dulled down even more through a light black ink wash. Some post-shading with lighter tones emphasized the contrast between the two colors again. And while it is not an exact representation of the unique RAN air superiority scheme, I think that the overall impression is there.

 

The cockpit interior was painted in very dark grey, while the landing gear, its wells and the inside of the air intake became white. A red rim was painted around the front opening, and the landing gear covers received a red outline, too. The white drop tanks are a detail I took from real world RAN A-4Gs - in the early days of the air superiority scheme, the tanks were frequently still finished in the old USN style livery, hence the white body but fins and tail section already in the updated colors.

 

The decals became a fight, though. As mentioned above, the came from an ESCI kit – and, as expected, the were brittle. All decals with a clear carrier film disintegrated while soaking in water, only those with a fully printed carrier film were more or less usable. One roundel broke and had to be repaired, and the checkered fin flash was a very delicate affair that broke several times, even though I tried to save and repair it with paint. But you can unfortunately see the damage.

 

Most stencils and some replacements (e. g. the “Navy” tag) come from the Sword FJ-3. While these decals are crisply printed, their carrier film is utterly thin, so thin that applying esp. the larger decals turned out to be hazardous and complicated. Another point that did not really convince me about the Sword kit.

 

Finally, the kit was sealed with matt acrylic varnish (Italeri) and some soot stains were added around the exhaust and the gun ports with graphite.

  

In the end, this build looks, despite the troubles and the rather exotic ingredients like a relatively simple Sabre with Australian markings, just with a different Navy livery. You neither immediately recognize the FJ-3 behind it, nor the Avon Sabre’s bigger fuselage, unless you take a close and probably educated look. Very subtle, though.

The RAN air superiority scheme from the late Skyhawks suits the Sabre/Fury-thing well – I like the fact that it is a modern fighter scheme, but, thanks to the tones and the colorful other markings, not as dull and boring like many others, e. g. the contemporary USN "Ghost" scheme. Made me wonder about an early RAAF F-18 in this livery - should look very pretty, too?

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

The McDonnell Douglas (now Boeing) T-45 Goshawk was a highly modified version of the BAe Hawk land-based training jet aircraft. Manufactured by McDonnell Douglas (now Boeing) and British Aerospace (now BAe Systems), the T-45 was used by the United States Navy and the United States Marine Corps (USMC) as an aircraft carrier-capable trainer.

The Goshawk's origins began in the mid-1970s, when the US Navy began looking for a single aircraft replacement for both its T-2 and TA-4 jet trainers. The US Navy started the VTXTS advanced trainer program in 1978. Several companies made submissions, e. g. North American or Northrop/Vought. Due to the size of the potential contract, European companies made submissions, too, including a navalized Alpha Jet from Dassault/Dornier and a fully carrier-capable version of the BAe Hawk Mk.60, mutually proposed by British Aerospace (BAe) and McDonnell Douglas (MDC). The latter eventually won the competition and BAe and MDC were awarded the T-45 contract in 1981.

 

The Hawk had not been designed for carrier operations and numerous modifications were required to make it suitable for use on carriers. These included improvements to the low-speed handling characteristics and a reduction in the approach speed. It was found that the aircraft was apt to stall at the low approach speed required. Modifications were designed by BAe in England; most notably a simple slat system was devised, operated by an actuator and linkage mechanism to fit into the small space available. Strakes were also added on the fuselage to improve airflow. Other changes were a strengthened airframe, a more robust and wider landing gear with a two-wheel nose landing gear, a catapult tow bar attachment and an arresting hook. The modified aircraft was christened “Goshawk”, flew in 1988 for the first time and became operational in 1991.

 

Beyond being a naval trainer the T-45 was also adapted for first-line duty with strike capabilities, in the form of the OA-45 for the USMC. The role of this aircraft dated back to the Vietnam War when twenty-three A-4 two-seaters were converted into OA-4Ms for “FastFAC” (Fast Forward Air Controller) missions, in order to control interdiction sorties dedicated to shaping the battlefield for future operations. Basically, the OA-4M was a TA-4F equipped with A-4M electronics. The most visible and characteristic change was the fitting of the A-4M’s dorsal electronics hump, neatly faired into the rear of the two-seat canopy. The nose sensor group of the OA-4M was basically the same as that of the A-4M, but the Angle/Rate Bombing system was not installed as it would not be needed.

 

When the T-45 was introduced in the early Nineties, the USMCs OA-4Ms had reached the end of their service life and the USMC started looking for a replacement, wanting a comparable, light and fast fixed-wing aircraft. The USMC did not accept the LTV A-7 as an A-4 replacement (even though a two-seater version was available), because it was already dated, too, and not part of the USMC inventory. The USMC's A-4Ms were supposed to be replaced by the VTOL AV-8 by the mid-nineties, but the AV-8, even as a two-seater, was deemed unsuitable for FFAC duties. The new T-45 looked like a good and economical alternative with future potential, since the airframe was brand new and the type's infrastructure was fully established, so that a small number of specialized aircraft could easily be supported without much extra cost.

 

With fresh experience from the 1st Gulf War in 1990-91 the decision was made to buy 25 extra T-45A airframes and convert them to OA-45A standard. Most important change were modified wings, using structures and systems from the BAe Hawk 100 series. While the T-45 only had two underwing and a single ventral hardpoint, the OA-45A featured a total of seven: four underwing and one ventral hardpoints, plus wingtip stations for defensive air-to-air missiles. Upgraded avionics allowed the deployment of a wide range of external stores, including air-to-ground missiles and rocket launchers, a reconnaissance pod, retarded and free-fall bombs of up to 1,000 pounds (450 kg) caliber, runway cratering, anti-personnel and light armor bombs, cluster bombs, practice bombs as well as external fuel tanks and ECM pods. This was a vital asset, since Desert Storm had proved that FFAC aircraft had to have an offensive capability to handle targets of opportunity on their own, when no air assets to control were available. A total ordnance load of up to 6,800 lb (3,085 kg) was possible, even though the aircraft was not supposed to play an offensive role and rather act from a distance, relying on its small size and agility.

 

Communication modifications for the FastFAC role included a KY-28 secure voice system, an ARC-159 radio and an ARC-114 VHF radio. Similar to the Skyhawk, a hump behind the cockpit had to be added to make room for the additional electronic equipment and a heat exchanger. Other additions were a continuous-wave Doppler navigation radar under a shallow ventral radome underneath the cockpit, a ground control bombing system, an APN-194 altimeter, an ALR-45 radar warning suite, a retrofitted, fixed midair refueling probe and cockpit armor plating that included Kevlar linings on the floor and the lower side walls as well as externally mounted armor plates for the upper areas.

 

VMA-131 of Marine Aircraft Group 49 (the Diamondbacks) retired its last four OA-4Ms on 22 June 1994, and the new OA-45A arrived just in time to replace the venerable Skyhawk two-seaters in the FastFAC role. Trainer versions of the Skyhawk remained in Navy service, however, finding a new lease on life with the advent of "adversary training". OA-45A deliveries were finished in 1996 and the 25 aircraft were distributed among the newly established Marine Aviation Logistics Squadron (MALS, formerly Headquarters & Maintenance Squadron/H&MS) 12 & 13. The USMC crews soon nicknamed their new mounts "GosHog", to underlöine ist offensive capabilities and to set themselves apart from the USN's "tame" trainers. Even though thos name was never officially approved it caught on quickly.

 

After initial experience with the new aircraft and in the wake of technological advances, the USMC decided to upgrade the OA-45As in 2000 to improve its effectiveness and interaction capabilities with ground troops. This primarily resulted in the addition of a forward-looking infrared camera laser in the aircraft’s nose section, which enabled the aircraft to execute all-weather/night reconnaissance and to illuminate targets for laser-guided infantry shells or ordnance launched by the OA-45 itself or by other aircraft. Through this measure the OA-45 became capable of carrying and independently deploying light laser-guided smart weapons like the GBU-12 and -16 “Paveway II” glide bombs or the laser-guided AGM-65E “Maverick” variant. The update was gradually executed during regular overhauls in the course of 2001 and 2002 (no new airframes were built/converted), the modified machines received the new designation OA-45B.

 

After this update phase, the OA-45Bs were deployed in several global conflicts and saw frequent use in the following years. For instance, MALS 13 used its OA-45Bs operationally for the first time in October 2002 when the squadron was tasked with providing support to six AV-8B Harrier aircraft in combat operations in Afghanistan during Operation Enduring Freedom. This mission lasted until October 2003, four aircraft were allocated and one OA-45B was lost during a landing accident.

On 15 January 2003, MALS 13 embarked 205 Marines and equipment aboard the USS Bonhomme Richard in support of combat operations in Southwest Asia during Operation Southern Watch. Four OA-45Bs successfully supported these troops from land bases, marking targets and flying reconnaissance missions.

Furthermore, six MALS 13 OA-45Bs took actively part in Operation Iraqi Freedom from Al Jaber Air Base, Kuwait, and An Numiniyah Expeditionary Air Field, Iraq, where the aircraft worked closely together with the advancing ground troops of the USMC’s 15th Marine Expeditionary Unit. They successfully illuminated targets for US Navy fighter bombers, which were launched from USS Abraham Lincoln (CVN-72) in the Persian Gulf, and effectively guided these aircraft to their targets. Two OA-45Bs were lost during this conflict, one through enemy MANPADS, the other through friendly AA fire. In late May 2003 the surviving machines and their crews returned to MCAS Yuma.

 

On 16 March 2007, the 200th T-45 airframe was delivered to the US Navy. From this final batch, six airframes were set aside and modified into OA-45Bs in order to fill the losses over the past years.

Later T-45 production aircraft were built with enhanced avionics systems for a heads-up display (HUD) and glass cockpit standard, while all extant T-45A aircraft were eventually converted to a T-45C configuration under the T-45 Required Avionics Modernization Program (T-45 RAMP), bringing all aircraft to same HUD plus glass cockpit standard. These updates, esp. concerning the cockpit, were introduced to the OA-45Bs, too, and they were re-designated again, now becoming OA-45Cs, to reflect the commonality with the Navy’s Goshawk trainers. Again, these modifications were gradually introduced in the course of the OA-45s’ normal maintenance program.

 

In 2007, an engine update of the whole T-45 fleet, including the OA-45s, with the Adour F405-RR-402 was considered. This new engine was based on the British Adour Mk 951, designed for the latest versions of the BAe Hawk and powering the BAe Taranis and Dassault nEUROn UCAV technology demonstrators. The Adour Mk 951 offered 6,500 lbf (29 kN) thrust and up to twice the service life of the F405-RR-401. It featured an all-new fan and combustor, revised HP and LP turbines, and introduced Full Authority Digital Engine Control (FADEC). The Mk 951 was certified in 2005, the F405-RR-402 derived from it was certified in 2008, but it did not enter service due to funding issues, so that this upgrade was not carried out.

 

The final delivery of the 246th T-45 airframe took place in November 2009, and both T-45 and the OA-45 "GosHog" are supposed to remain in service until 2035.

  

General characteristics:

Crew: 2 (pilot, observer)

Length: 39 ft 4 in (11.99 m)

Wingspan: 30 ft 10 in (9.39 m)

Height: 13 ft 5 in (4.08 m)

Wing area: 190.1 ft² (17.7 m²)

Empty weight: 10,403 lb (4,460 kg)

Max. takeoff weight: 14,081 lb (6,387 kg)

 

Powerplant:

1× Rolls-Royce Turbomeca F405-RR-401 (Adour) non-afterburning turbofan with 5,527 lbf (26 kN)

 

Performance:

Maximum speed: Mach 2 (2,204 km/h (1,190 kn; 1,370 mph) at high altitude

Combat radius: 800 km (497 mi, 432 nmi)

Ferry range: 3,200 km (1,983 mi) with drop tanks

Service ceiling: 15,240 m (50,000 ft)

Wing loading: 283 kg/m² (58 lb/ft²)

Thrust/weight: 0.97

Maximum g-load: +9 g

 

Armament:

No internal gun; seven external hardpoints (three on each wing and one under fuselage)

for a wide range of ordnance of up to 6,800 lb (3,085 kg), including up to six AIM-9 Sidewinder for

self-defense, pods with unguided rockets for target marking or ECM pods, but also offensive weapons

of up to 1.000 lb (454 kg) weight, including iron/cluster bombs and guided AGM-65, GBU-12 and -16.

  

The kit and its assembly:

This fictional T-45 variant is actually the result of a long idea evolution, and simply rooted in the idea of a dedicated OA-4M replacement for the USMC; in real life, the FFAC role has been transferred to F-18 two-seaters, though, but the T-45 appeared like a sound alternative to me.

 

There's only one T-45 kit available, a dubious T-45A from Italeri with poor wings and stabilizers. Wolfpack also offers a T-45, but it’s just a re-boxing of the Italeri kit with some PE parts and a price tag twice as big – but it does not mend the original kit’s issues… After reading the A-4 Skyhawk book from the French "Planes & Pilots" series, I was reminded of the USMC's special OA-4M FAC two-seaters (and the fact that it is available in kit form from Italeri and Hasegawa), and, cross-checking the real-world timeline of the T-45, I found that it could have been a suitable successor. The ide of the USMC’s OA-45 was born! :D

 

Building-wise the Italeri T-45 remained close to OOB, even though I transplanted several parts from an Italeri BAe Hawk Mk. 100 to create a different look. I modified the nose with the Mk. 100’s laser fairing and added some radar warning sensor bumps. This transplantation was not as easy as it might seem because the T-45’s nose is, due to the different and more massive front landing gear quite different from the Hawk’s. Took some major PSR to integrate the laser nose.

An ALR-45 “hot dog” fairing from a late A-4M (Italeri kit) was added to the fin, together with a small styrene wedge extending the fin’s leading edge. This small detail markedly changes the aircraft’s look. I furthermore added a refueling probe, scratched from coated wire and some white glue, as well as a low “camel back” fairing behind the cockpit, created from a streamlined bomb half with air outlets for an integrated heat exchanger. Blade antennae were relocated and added. A shallow bump for the Doppler radar was added under the fuselage behind the landing gear well – left over from an Airfix A-4B (from an Argentinian A-4P, to be correct, actually a dorsal fairing).

 

On the wings, a tailored pair of pylons and wing tip launch rails from the Italeri BAe Hawk Mk. 100 kit were added, too, as well as the donor kit’s pair of Sidewinders. The rest of the ordnance consists of drop tanks and LAU-19 pods for target marking missiles. The tanks were taken from the Hawk Mk. 100 kit, too, the rocket launchers came from an Italeri NATO aircraft weapons set. The centerline position carries an ALQ-131 ECM pod from a Hasegawa US aircraft weapons set on a pylon from the scrap box.

  

Painting and markings:

The low-viz idea prevailed, since I had some leftover OA-4M decals from Italeri kits in store, as well as some other suitable low-viz decals from a Revell A-4F kit. However, an all-grey livery was IMHO not enough, and when I came across a picture of a USN low-viz A-7E with an improvised desert camouflage in sand and reddish brown applied over the grey (even partly extending over its markings) from Operation Iraqi Freedom, I had that extra twist that would set the OA-45 apart. MALS-13 was chosen as operator because I had matching codes, and, as another benefit, the unit had actually been deployed overseas during the 2003 Iraq War, so that the whif’’s time frame was easily settled, adding to its credibility.

 

The livery was built up just like on the real aircraft: on top of a basic scheme in FS 36320 and 36375 (Humbrol 128 and 127) with a slightly darker anti-glare panel in front of the cockpit (FS 35237, I used Revell 57 as a slightly paler alternative) I applied the low-viz marking decals, which were protected with a coat of acrylic varnish. Next, additional desert camouflage was added with dry-brushed sand and millitary brown (supposedly FS 33711 and 30400 in real life, I used, after consulting pictures of aircraft from both Gulf Wars, Humbrol 103 (Cream) and 234 (Dark Flesh). They were applied with a kind of a dry-brushing technique, for a streaky and worn look, leaving out the codes and other markings. The pattern itself was inspired by an USMC OV-10 Bronco in desert camouflage from the 1st Gulf War.

On top of that a black ink washing was applied. Once things had thoroughly dried over night, I wet-sanded the additional desert camouflage away, carefully from front to back, so that the edges became blurred and the underlying grey became visible again.

 

The cockpit interior was painted in standard Dark Gull Grey (Humbrol 140), while the air intakes and the landing gear became white, the latter with red trim on the covers’ edges – just standard. Finally, the model was sealed with a coat of matt acrylic varnish (Italeri).

  

The upgraded T-45 is an interesting result. The add-ons suit the aircraft, which already looks sturdier than its land-based ancestor, well. The improvised desert paint scheme with the additional two-tone camouflage over the pale grey base really makes the aircraft an unusual sight, adding to its credibility.

Hardware-wise I am really happy how the added dorsal hump blends into the overall lines – in a profile view it extends the canopy’s curve and blends into the fin, much like the A-4F/M’s arrangement. And the modified fin yields a very different look, even though not much was changed. The T-45 looks much beefier now, and from certain angles really reminds of the OA-4M and sometimes even of a diminutive Su-25?

en.wikipedia.org/wiki/Supermarine_Spitfire_

 

en.wikipedia.org/wiki/Yorkshire_Air_Museum#Collection

 

Supermarine Spitfire variants powered by early model Rolls-Royce Merlin engines mostly utilised single-speed, single-stage superchargers. The British Supermarine Spitfire was the only Allied fighter aircraft of the Second World War to fight in front line service from the beginnings of the conflict, in September 1939, through to the end in August 1945. Post-war, the Spitfire's service career continued into the 1950s. The basic airframe proved to be extremely adaptable, capable of taking far more powerful engines and far greater loads than its original role as a short-range interceptor had called for. This would lead to 19 marks of Spitfire and 52 sub-variants being produced throughout the Second World War, and beyond. The many changes were made in order to fulfil Royal Air Force requirements and to successfully engage in combat with ever-improving enemy aircraft. With the death of the original designer, Reginald J. Mitchell, in June 1937, all variants of the Spitfire were designed by his successor, Joseph Smith, and a team of engineers and draftsmen.

 

In 1936, before the first flight of the prototype, the Air Ministry placed an order for 310 Spitfires. However, in spite of the promises made by the Chairman of Vickers-Armstrongs (the parent company of Supermarine) that the company would be able to deliver Spitfire at a rate of five a week, it soon became clear that this would not happen. In 1936 the Supermarine company employed 500 people and was already engaged in fulfilling orders for 48 Walrus amphibian reconnaissance aircraft and 17 Stranraer patrol flying boats. In addition the small design staff, which would have to draft the blueprints for the production aircraft, was already working at full stretch. Although it was obvious that most of the work would have to be sub-contracted to outside sources, the Vickers-Armstrongs board was reluctant to allow this to happen. When other companies were able to start building Spitfire components there were continual delays because either parts provided to them would not fit, or the blueprints were inadequate; the sub-contractors themselves faced numerous problems building components which in many cases were more advanced and complicated than anything they had faced before.

 

As a consequence of the delays, the RAF received the first two Spitfires off the production line in July 1938, while the first Spitfire to enter squadron service was received by 19 Squadron in early August. For a time the future of the Spitfire was in serious doubt, with the Air Ministry suggesting that the programme be abandoned and that Supermarine change over to building the Bristol Beaufighter under licence. The managements of Supermarine and Vickers were eventually able to convince the Air Ministry that production would be sorted out and, in 1938, an order was placed with Morris Motors Limited for an additional 1,000 Spitfires to be built at huge new factory which was to be built at Castle Bromwich. This was followed in 1939 by an order for another 200 from Woolston and, only a few months later, another 450. This brought the total to 2,160, making it one of the largest orders in RAF history. Over the next three years a large number of modifications were made, most as a result of wartime experience.

 

Early in the Spitfire's operational life a major problem became apparent; at altitudes above about 15,000 ft (4,572 m), any condensation could freeze in the guns. Because of this the system of gun heating first fitted to K5054 was introduced on the 61st production Mk I. At the outset of World War II, the flash-hiders on the gun muzzles were removed and the practice of sealing the gun ports with fabric patches was instituted. The patches kept the gun barrels free of dirt and debris and allowed the hot air to heat the guns more efficiently. Early production aircraft were fitted with a ring and bead gunsight, although provision had been made for a reflector sight to be fitted once one had been selected. In July 1938, the Barr and Stroud GM 2 was selected as the standard RAF reflector gunsight and was fitted to the Spitfire from late 1938. These first production Mk Is were able to reach a maximum speed of 362 mph (583 km/h) at 18,500 ft (5,600 m), with a maximum rate of climb of 2,490 ft/min at 10,000 ft (3,000 m). The service ceiling (where the climb rate drops to 100 ft/min) was 31,900 ft (9,700 m).

 

All Merlin I to III series engines relied on external electric power to start; a well known sight on RAF fighter airfields was the "trolley acc" (trolley accumulator) which was a set of powerful batteries which could be wheeled up to aircraft. The lead from the "Trolley Acc" was plugged into a small recess on the starboard side cowling of the Spitfire. On Supermarine-built aircraft a small brass instruction plate was secured to the side cowling, just beneath the starboard exhausts.

 

The early Mk Is were powered by the 1,030 hp (768 kW) Merlin Mk II engine driving an Aero-Products "Watts" 10 ft 8 in (3.3 m) diameter two-blade wooden fixed-pitch propeller, weighing 83 lb (38 kg). From the 78th production airframe, the Aero Products propeller was replaced by a 350 lb (183 kg) de Havilland 9 ft 8 in (2.97 m) diameter, three-bladed, two-position, metal propeller, which greatly improved take-off performance, maximum speed and the service ceiling. From the 175th production aircraft, the Merlin Mk III, with a "universal" propeller shaft able to take a de Havilland or Rotol propeller, was fitted. Following complaints from pilots a new form of "blown" canopy was manufactured and started replacing the original "flat" version in early 1939. This canopy improved headroom and enabled better vision laterally, and to the rear. At the same time the manual hand-pump for operating the undercarriage was replaced by a hydraulic system driven by a pump mounted in the engine bay. Spitfire Is incorporating these modifications were able to achieve a maximum speed of 367 mph (591 km/h) at 18,600 ft (5,700 m), with a maximum rate of climb of 2,150 ft/min at 10,000 ft (3,000 m). The service ceiling was 34,400 ft (10,500 m).

 

A voltage regulator under a black, cylindrical cover was mounted low on the back of frame 11, directly behind the pilot's seat:[nb 3]starting in the N30xx series this was repositioned higher, appearing low in the rear transparency. From N32xx the regulator was mounted directly behind the pilot's headrest on frame 11. Other changes were made later in 1939 when a simplified design of pitot tube was introduced and the "rod" aerial mast was replaced by a streamlined, tapered design. To improve protection for the pilot and fuel tanks a thick laminated glass bulletproof plate was fitted to the curved, one piece windscreen and a 3 mm thick cover of light alloy, capable of deflecting small calibre rounds, was fitted over the top of the two fuel tanks. From about mid-1940, 73 pounds (33 kg) of armoured steel plating was provided in the form of head and back protection on the seat bulkhead and covering the forward face of the glycol header tank. In addition, the lower petrol tank was fitted with a fire-resistant covering called "Linatex", which was later replaced with a layer of self-sealing rubber.

 

In June 1940 de Havilland began manufacturing a kit to convert their two pitch propeller unit to a constant speed propeller. Although this propeller was a great deal heavier than the earlier types (500 lb (227 kg) compared with 350 lb (183 kg)) it provided another substantial improvement in take-off distance and climb rate. Starting on 24 June de Havilland engineers began fitting all Spitfires with these units and by 16 August every Spitfire and Hurricane had been modified. "Two step" rudder pedals were fitted to all frontline Spitfires; these allowed the pilot to lift his feet and legs higher during combat, improving his "blackout" threshold and allowing him to pull tighter sustained turns. Another modification was the small rear view mirror which was added to the top of the windscreen: an early "shrouded" style was later replaced by a simplified, rectangular, adjustable type.

 

Starting in September 1940, IFF equipment was installed. This weighed about 40 lb (18 kg) and could be identified by wire aerials strung between the tailplane tips and rear fuselage. Although the added weight and the aerials reduced maximum speed by about two mph (three km/h), it allowed the aircraft to be identified as "friendly" on radar: lack of such equipment was a factor leading to the Battle of Barking Creek. At about the same time new VHF T/R Type 1133 radios started replacing the HF TR9 sets. These had first been fitted to Spitfires of 54 and 66 Squadrons in May 1940, but ensuing production delays meant the bulk of Spitfires and Hurricanes were not fitted for another five months. The pilots enjoyed a much clearer reception which was a big advantage with the adoption of Wing formations throughout the RAF in 1941. The new installation meant that the wire running between the aerial mast and rudder could be removed, as could the triangular "prong" on the mast.

 

Weight increases and aerodynamic changes led to later Spitfire Is having a lower maximum speed than the early production versions. This was more than offset by the improvements in take-off distance and rate of climb brought about by the constant speed propeller units. During the Battle of Britain Spitfire Is equipped with constant-speed propellers had a maximum speed of 353 mph (568 km/h) at 20,000 ft (6,100 m), with a maximum rate of climb of 2,895 ft/min at 10,000 ft (3,000 m).

 

Although the Merlin III engine of Spitfire Is had a power rating of 1,030 hp (768 kW), supplies of 100 octane fuel from the United States started reaching Britain in early 1940. This meant that an "emergency boost" of +12 pounds per square inch was available for five minutes, with pilots able to call on 1,310 hp (977 kW) at 3,000 rpm at 9,000 feet (2,743 m). This boosted the maximum speed by 25 mph (40 km/h) at sea level and 34 mph (55 km/h) at 10,000 ft (3,000 m) and improved the climbing performance between sea level and full throttle height. The extra boost wasn't damaging as long as the limitations set forth in the pilot's notes were followed. As a precaution if the pilot had resorted to emergency boost, he had to report this on landing and it had to be noted in the engine log book. There was a wire 'gate' fitted, which the pilot had to break to set the engine to emergency power, this acted as an indicator that emergency power had been used and would be replaced by mechanics on the ground. The extra boost was also available for the Merlin XII fitted to the Spitfire II.

 

Late in 1940, a Martin-Baker designed quick-release canopy mechanism began to be retroactively fitted to all Spitfires. The system employed unlocking pins, actuated by cables operated by the pilot pulling a small, red rubber ball mounted on the canopy arch. When freed, the canopy was taken away by the slipstream. One of the most important modifications to the Spitfire was to replace the machine gun armament with wing mounted Hispano 20 mm cannon. In December 1938, Joseph Smith was instructed to prepare a scheme to equip a Spitfire with a single Hispano mounted under each wing. Smith objected to the idea and designed an installation in which the cannon were mounted on their sides within the wing, with only small external blisters on the upper and lower wing surfaces covering the 60 round drum magazine. The first Spitfire armed with a single Hispano in each wing was L1007 which was posted to Drem in January 1940 for squadron trials. On 13 January, this aircraft, piloted by Plt Off Proudman of 602 Squadron took part in an engagement when a Heinkel He 111 was shot down. Soon after this Supermarine was contracted to convert 30 Spitfires to take the cannon armed wing; 19 Squadron received the first of these in June 1940 and by 16 August 24 cannon armed Spitfires had been delivered. These were known as the Mk Ib: Mk Is armed with eight Brownings were retrospectively called the Mk Ia. With the early cannon installation, jamming was a serious problem. In one engagement, only two of the 12 aircraft had been able to fire off all of their ammunition. Further cannon-armed Spitfires, with improvements to the cannon mounts, were later issued to 92 Squadron, but due to the limited magazine capacity it was eventually decided the best armament mix was two cannon and four machine guns (most of these were later converted to the first Mk Vbs).

 

Sergeant Jennings in September 1940. The absence of a triangular prong on the rear of the mast indicates that VHF radio was fitted. The voltage regulator can be seen under the rear transparency. This photo makes a good comparison with K9795.

From November 1940, a decision was taken that Supermarine would start producing light-alloy covered ailerons which would replace the original fabric covered versions. However, seven months after the decision was taken to install them on all marks, Spitfires were still being delivered with the original fabric covered ailerons. From May 1941 metal ailerons were fitted to all Spitfires coming off the production lines.

 

The Yorkshire Air Museum & Allied Air Forces Memorial is an aviation museum in Elvington, York on the site of the former RAF Elvington airfield, a Second World War RAF Bomber Command station. The museum was founded, and first opened to the public, in the mid 1980s.

 

The museum is one of the largest independent air museums in Britain. It is also the only Allied Air Forces Memorial in Europe. The museum is an accredited museum under Arts Council accreditation scheme. It is a Member of Friends of the Few (Battle of Britain Memorial), the Royal Aeronautical Society, the Museums Association and the Association of Independent Museums.

 

The Museum is a registered charity (No. 516766) dedicated to the history of aviation and was also set up as a Memorial to all allied air forces personnel, particularly those who served in the Royal Air Force during the Second World War.

 

Site

Further information: RAF Elvington

The 20-acre (81,000 m2) parkland site includes buildings and hangars, some of which are listed. It incorporates a 7-acre (28,000 m2) managed environment area and a DEFRA and Environment Agency supported self sustainability project called "Nature of Flight". The museum is situated next to a 10,000 ft runway, which is privately owned.

 

History

Whilst the Royal Air Force carried on using the runway for aircraft landing and take off training until 1992, the buildings and hangars had long been abandoned. In 1980 Rachel Semlyen approached the owners of "what was then an abandoned and derelict wartime site, with the idea of restoring the buildings and creating a museum". In 1983, a group started clearing the undergrowth and the site was ready to be unveiled as the Yorkshire Air Museum in 1986.

 

Events

The Museum undertakes several annual events each year within the general attraction / entertainment area as well as educational / academic events for specific audiences, plus several corporate events in association with companies such as Bentley, Porsche, banking, government agencies etc. The unique annual Allied Air Forces Memorial Day takes place in September.

 

Exhibits

The Museum has over 50 aircraft spanning the development of aviation from 1853 up to the latest GR4 Tornado. Several aircraft including Victor, Nimrod, Buccaneer, Sea Devon, SE5a, Eastchurch Kitten, DC3 Dakota are kept live and operated on special "Thunder Days" during the year. Over 20 historic vehicles and a Registered Archive containing over 500,000 historic artefacts and documents are also preserved at the Museum, which is also the Official Archive for the National Aircrew Association and National Air Gunners Association. It is nationally registered and accredited through DCMS/Arts Council England and is a registered charity.

 

A permanent exhibition on RAF Bomber Command was opened at the museum by life member, Sir David Jason. In 2010 a new exhibition called "Pioneers of Aviation", and funded by the Heritage Lottery Fund, was opened featuring the lives and achievements of Sir George Cayley, Sir Barnes Wallis, Robert Blackburn, Nevil Shute and Amy Johnson.

 

Principal on-site businesses include: Restaurant, Retail Shop, Events, Aircraft Operation Engineering Workshops, Archives and Corporate Business Suite. The museum is also a location for TV and film companies.

 

Building 1 – Airborne Forces Display & No. 609 Squadron RAF Room

Building 2 – Uniform Display

Building 3 – Air Gunners' Exhibition

Building 4 – Archives & Reference Library

Building 5 – Museum Shop

Building 7 – Memorial Garden

Building 8 – Museum HQ, Main Entrance

Building 9 – Against the Odds

Building 10 – Elvington Corporate Room

Building 11 – Museum NAAFI Restaurant

Building 12 – Control Tower

Building 13 – French Officers' Mess

Building 14 – Airmens Billet and Station MT Display

Building 15 – Royal Observer Corp

Building 16 – Signal Square

Building 17 – Hangar T2 Main Aircraft exhibition

Building 18 – Archive & Collections Building

Building 19 – Handley Page Aircraft Workshop

Building 20 – Pioneer of Aviation Exhibition

 

Collection

Aircraft on display

Pre-World War II

Avro 504K – Replica

Blackburn Mercury – Replica

Cayley Glider – Replica

Mignet HM.14 Pou-du-Ciel

Port Victoria P.V.8 Eastchurch Kitten Replica

Royal Aircraft Factory BE.2c – Replica

Royal Aircraft Factory SE.5a – Replica

Wright Flyer – Replica

 

World War II

Avro Anson T.21 VV901

Douglas Dakota IV KN353

Fairchild Argus II FK338

Gloster Meteor F.8 WL168

Gloster Meteor NF.14 WS788

Handley Page Halifax III LV907

Hawker Hurricane I – Replica

Messerschmitt Bf 109 G-6 – Replica

Slingsby T.7 Kirby Cadet RA854

Supermarine Spitfire I – Replica

Waco Hadrian 237123

 

Post World War II

Air Command Commander Elite

Beagle Terrier 2 TJ704

Canadair CT-133 Silver Star 133417

de Havilland Devon C.2 VP967

de Havilland Vampire T.11 XH278

Europa Prototype 001

Mainair Demon

Saunders-Roe Skeeter AOP.12 XM553

Westland Dragonfly HR.5 WH991

 

Cold War

BAC Jet Provost T.4 XP640

Blackburn Buccaneer S.2 XN974

Blackburn Buccaneer S.2B XX901

British Aerospace Harrier GR.3 XV748

British Aerospace Nimrod MR.2 XV250

Dassault Mirage IIIE 538

Dassault Mirage IVA 45/BR

English Electric Canberra T.4 WH846

English Electric Lightning F.6 XS903 which arrived during June 1988.

Fairey Gannet AEW.3 XL502

Gloster Javelin FAW.9 XH767

Handley Page Victor K.2 XL231

Hawker Hunter FGA.78 QA10

Hawker Hunter T.7 XL572

Panavia Tornado GR.1 ZA354

Panavia Tornado GR.4 XZ631

 

Ground vehicles

Second World War

Thompson Brothers Aircraft Refueller

1938 Ford Model E

1940 "Tilly" Standard 12 hp Mkl RAF Utility Vehicle

1941 Chevrolet 4x4 CMP

1942 Austin K2 NAAFI Wagon

1942 Thornycroft ‘Amazon’ Coles Crane

 

Cold War

1947 Commer one and a half deck airport coach

1949 Citroen 11BL

1948 David Brown VIG.2 Aircraft Tractor

1949 David Brown VIG.3 Aircraft Tractor

1951 David Brown GP Airfield Tractor

1953 Alvis Saracen 12ton APC

1953 Austin Champ Cargo 4x4 General Purpose Vehicle

1956 Green Goddess Self Propelled Pump

1958 Commer Q4 Bikini Fire Pump Unit

1958 Lansing Aircraft Carrier Type Tug

1959 Daimler Ferret ASC MK.2/3/7

1966 Chieftain Main Battle Tank

1970 Douglas P3 nuclear aircraft 25 tonne tug

1971 Pathfinder Fire Engine 35ton (ex. Manchester Airport)

1972 TACR2 Range Rover - 6 wheeled fast response fire unit

1974 GMC 6 wheeled fast response airfield fire truck

1976 Dennis Mercury 17.5 tonne aircraft tug

Pathfinder Fire Engine

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

The CAC Sabre, sometimes known as the Avon Sabre or CA-27, was an Australian variant of the North American Aviation F-86F Sabre fighter aircraft. In 1951, Commonwealth Aircraft Corporation obtained a license agreement to build the F-86F Sabre. In a major departure from the North American blueprint, it was decided that the CA-27 would be powered by a license-built version of the Rolls-Royce Avon R.A.7, rather than the General Electric J47. In theory, the Avon was capable of more than double the maximum thrust and double the thrust-to-weight ratio of the US engine. This necessitated a re-design of the fuselage, as the Avon was shorter, wider and lighter than the J47.

 

To accommodate the Avon, over 60 percent of the fuselage was altered and there was a 25 percent increase in the size of the air intake. Another major revision was in replacing the F-86F's six machine guns with two 30mm ADEN cannon, while other changes were also made to the cockpit and to provide an increased fuel capacity.

 

The prototype aircraft first flew on 3 August 1953. The production aircrafts' first deliveries to the Royal Australian Air Force began in 1954. The first batch of aircraft were powered by the Avon 20 engine and were designated the Sabre Mk 30. Between 1957 and 1958 this batch had the wing slats removed and were re-designated Sabre Mk 31. These Sabres were supplemented by 20 new-built aircraft. The last batch of aircraft were designated Sabre Mk 32 and used the Avon 26 engine, of which 69 were built up to 1961.

 

Beyond these land-based versions, an indigenous version for carrier operations had been developed and built in small numbers, too, the Sea Sabre Mk 40 and 41. The roots of this aircraft, which was rather a prestigious idea than a sensible project, could be traced back to the immediate post WWII era. A review by the Australian Government's Defence Committee recommended that the post-war forces of the RAN be structured around a Task Force incorporating multiple aircraft carriers. Initial plans were for three carriers, with two active and a third in reserve, although funding cuts led to the purchase of only two carriers in June 1947: Majestic and sister ship HMS Terrible, for the combined cost of AU£2.75 million, plus stores, fuel, and ammunition. As Terrible was the closer of the two ships to completion, she was finished without modification, and was commissioned into the RAN on 16 December 1948 as HMAS Sydney. Work progressed on Majestic at a slower rate, as she was upgraded with the latest technology and equipment. To cover Majestic's absence, the Colossus-class carrier HMS Vengeance was loaned to the RAN from 13 November 1952 until 12 August 1955.

 

Labour difficulties, late delivery of equipment, additional requirements for Australian operations, and the prioritization of merchant ships over naval construction delayed the completion of Majestic. Incorporation of new systems and enhancements caused the cost of the RAN carrier acquisition program to increase to AU£8.3 million. Construction and fitting out did not finish until October 1955. As the carrier neared completion, a commissioning crew was formed in Australia and first used to return Vengeance to the United Kingdom.

The completed carrier was commissioned into the RAN as HMAS Majestic on 26 October 1955, but only two days later, the ship was renamed Melbourne and recommissioned.

 

In the meantime, the rather political decision had been made to equip Melbourne with an indigenous jet-powered aircraft, replacing the piston-driven Hawker Fury that had been successfully operated from HMAS Sydney and HMAS Vengeance, so that the "new jet age" was even more recognizable. The choice fell on the CAC Sabre, certainly inspired by North American's successful contemporary development of the navalized FJ-2 Fury from the land-based F-86 Sabre. The CAC 27 was already a proven design, and with its more powerful Avon engine it even offered a better suitability for carrier operations than the FJ-2 with its rather weak J47 engine.

 

Work on this project, which was initially simply designated Sabre Mk 40, started in 1954, just when the first CAC 27's were delivered to operative RAAF units. While the navalized Avon Sabre differed outwardly only little from its land-based brethren, many details were changed and locally developed. Therefore, there was also, beyond the general outlines, little in common with the North American FJ-2 an -3 Fury.

Externally, a completely new wing with a folding mechanism was fitted. It was based on the F-86's so-called "6-3" wing, with a leading edge that was extended 6 inches at the root and 3 inches at the tip. This modification enhanced maneuverability at the expense of a small increase in landing speed due to deletion of the leading edge slats, a detail that was later introduced on the Sabre Mk 31, too. As a side benefit, the new wing leading edges without the slat mechanisms held extra fuel. However, the Mk 40's wing was different as camber was applied to the underside of the leading edge to improve low-speed handling for carrier operations. The wings were provided with four stations outboard of the landing gear wells for up to 1000 lb external loads on the inboard stations and 500 lb on the outboard stations.

 

Slightly larger stabilizers were fitted and the landing gear was strengthened, including a longer front wheel strut. The latter necessitated an enlarged front wheel well, so that the front leg’s attachment point had to be moved forward. A ventral launch cable hook was added under the wing roots and an external massive arrester hook under the rear fuselage.

Internally, systems were protected against salt and humidity and a Rolls-Royce Avon 211 turbojet was fitted, a downrated variant of the already navalized Avon 208 from the British DH Sea Vixen, but adapted to the different CAC 27 airframe and delivering 8.000 lbf (35.5 kN) thrust – slightly more than the engines of the land-based CAC Sabres, but also without an afterburner.

 

A single Mk 40 prototype was built from a new CAC 27 airframe taken directly from the production line in early 1955 and made its maiden flight on August 20th of the same year. In order to reflect its naval nature and its ancestry, this new CAC 27 variant was officially christened “Sea Sabre”.

Even though the modified machine handled well, and the new, cambered wing proved to be effective, many minor technical flaws were discovered and delayed the aircraft's development until 1957. These included the wing folding mechanism and the respective fuel plumbing connections, the landing gear, which had to be beefed up even more for hard carrier landings and the airframe’s structural strength for catapult launches, esp. around the ventral launch hook.

 

In the meantime, work on the land-based CAC 27 progressed in parallel, too, and innovations that led to the Mk 31 and 32 were also incorporated into the naval Mk 40, leading to the Sea Sabre Mk 41, which became the effective production aircraft. These updates included, among others, a detachable (but fixed) refueling probe under the starboard wing, two more pylons for light loads located under the wing roots and the capability to carry and deploy IR-guided AIM-9 Sidewinder air-to-air missiles, what significantly increased the Mk 41's efficiency as day fighter. With all these constant changes it took until April 1958 that the Sabre Mk 41, after a second prototype had been directly built to the new standard, was finally approved and cleared for production. Upon delivery, the RAN Sea Sabres carried a standard NATO paint scheme with Extra Dark Sea Grey upper surfaces and Sky undersides.

 

In the meantime, the political enthusiasm concerning the Australian carrier fleet had waned, so that only twenty-two aircraft were ordered. The reason behind this decision was that Australia’s carrier fleet and its capacity had become severely reduced: Following the first decommissioning of HMAS Sydney in 1958, Melbourne became the only aircraft carrier in Australian service, and she was unavailable to provide air cover for the RAN for up to four months in every year; this time was required for refits, refueling, personnel leave, and non-carrier duties, such as the transportation of troops or aircraft. Although one of the largest ships to serve in the RAN, Melbourne was one of the smallest carriers to operate in the post-World War II period, so that its contribution to military actions was rather limited. To make matters worse, a decision was made in 1959 to restrict Melbourne's role to helicopter operations only, rendering any carrier-based aircraft in Australian service obsolete. However, this decision was reversed shortly before its planned 1963 implementation, but Australia’s fleet of carrier-borne fixed-wing aircraft would not grow to proportions envisioned 10 years ago.

 

Nevertheless, on 10 November 1964, an AU£212 million increase in defense spending included the purchase of new aircraft for Melbourne. The RAN planned to acquire 14 Grumman S-2E Tracker anti-submarine aircraft and to modernize Melbourne to operate these. The acquisition of 18 new fighter-bombers was suggested (either Sea Sabre Mk 41s or the American Douglas A-4 Skyhawk), too, but these were dropped from the initial plan. A separate proposal to order 10 A-4G Skyhawks, a variant of the Skyhawk designed specifically for the RAN and optimized for air defense, was approved in 1965, but the new aircraft did not fly from Melbourne until the conclusion of her refit in 1969. This move, however, precluded the production of any new and further Sea Sabre.

 

At that time, the RAN Sea Sabres received a new livery in US Navy style, with upper surfaces in Light Gull Gray with white undersides. The CAC Sea Sabres remained the main day fighter and attack aircraft for the RAN, after the vintage Sea Furies had been retired in 1962. The other contemporary RAN fighter type in service, the Sea Venom FAW.53 all-weather fighter that had replaced the Furies, already showed its obsolescence.

In 1969, the RAN purchased another ten A-4G Skyhawks, primarily in order to replace the Sea Venoms on the carriers, instead of the proposed seventh and eighth Oberon-class submarines. These were operated together with the Sea Sabres in mixed units on board of Melbourne and from land bases, e.g. from NAS Nowra in New South Wales, where a number of Sea Sabres were also allocated to 724 Squadron for operational training.

 

Around 1970, Melbourne operated a standard air group of four jet aircraft, six Trackers, and ten Wessex helicopters until 1972, when the Wessexes were replaced with ten Westland Sea King anti-submarine warfare helicopters and the number of jet fighters doubled. Even though the A-4G’s more and more took over the operational duties on board of Melbourne, the Sea Sabres were still frequently deployed on the carrier, too, until the early Eighties, when both the Skyhawks and the Sea Sabres received once more a new camouflage, this time a wraparound scheme in two shades of grey, reflecting their primary airspace defense mission.

 

The CAC 27 Mk 41s’ last carrier operations took place in 1981 in the course of Melbourne’s involvements in two major exercises, Sea Hawk and Kangaroo 81, the ship’s final missions at sea. After Melbourne was decommissioned in 1984, the Fleet Air Arm ceased fixed-wing combat aircraft operation. This was the operational end of the Sabre Mk 41, which had reached the end of their airframe lifetime, and the Sea Sabre fleet had, during its career, severely suffered from accidents and losses: upon retirement, only eight of the original twenty-two aircraft still existed in flightworthy condition, so that the aircraft were all scrapped. The younger RAN A-4Gs were eventually sold to New Zealand, where they were kept in service until 2002.

  

General characteristics:

Crew: 1

Length: 37 ft 6 in (11.43 m)

Wingspan: 37 ft 1 in (11.3 m)

Height: 14 ft 5 in (4.39 m)

Wing area: 302.3 sq ft (28.1 m²)

Empty weight: 12,000 lb (5,443 kg)

Loaded weight: 16,000 lb (7,256 kg)

Max. takeoff weight: 21,210 lb (9,621 kg)

 

Powerplant:

1× Rolls-Royce Avon 208A turbojet engine with 8,200 lbf (36.44 kN)

 

Performance:

Maximum speed: 700 mph (1,100 km/h) (605 knots)

Range: 1,153 mi, (1,000 NM, 1,850 km)

Service ceiling: 52,000 ft (15,850 m)

Rate of climb: 12,000 ft/min at sea level (61 m/s)

 

Armament:

2× 30 mm ADEN cannons with 150 rounds per gun

5,300 lb (2,400 kg) of payload on six external hardpoints;

Bombs were usually mounted on outer two pylons as the mid pair were wet-plumbed pylons for

2× 200 gallons drop tanks, while the inner pair was usually occupied by a pair of AIM-9 Sidewinder

AAMs

A wide variety of bombs could be carried with maximum standard loadout being 2x 1,000 lb bombs

or 2x Matra pods with unguided SURA missiles plus 2 drop tanks for ground attacks, or 2x AIM-9 plus

two drop tanks as day fighter

  

The kit and its assembly:

This project was initially inspired by a set of decals from an ESCI A-4G which I had bought in a lot – I wondered if I could use it for a submission to the “In the navy” group build at whatifmodelers.com in early 2020. I considered an FJ-3M in Australian colors on this basis and had stashed away a Sword kit of that aircraft for this purpose. However, I had already built an FJ variant for the GB (a kitbashed mix of an F-86D and an FJ-4B in USMC colors), and was reluctant to add another Fury.

 

This spontaneously changed after (thanks to Corona virus quarantine…) I cleaned up one of my kit hoards and found a conversion set for a 1:72 CAC 27 from JAYS Model Kits which I had bought eons ago without a concrete plan. That was the eventual trigger to spin the RAN Fury idea further – why not a navalized version of the Avon Sabre for HMAS Melbourne?

 

The result is either another kitbash or a highly modified FJ-3M from Sword. The JAYS Model Kits set comes with a THICK sprue that carries two fuselage halves and an air intake, and it also offers a vacu canopy as a thin fallback option because the set is actually intended to be used together with a Hobby Craft F-86F.

 

While the parts, molded in a somewhat waxy and brittle styrene, look crude on the massive sprue, the fuselage halves come with very fine recessed engravings. And once you have cleaned the parts (NOTHING for people faint at heart, a mini drill with a saw blade is highly recommended), their fit is surprisingly good. The air intake was so exact that no putty was needed to blend it with the rest of the fuselage.

 

The rest came from the Sword kit and integrating the parts into the CAC 27 fuselage went more smoothly than expected. For instance, the FJ-3M comes with a nice cockpit tub that also holds a full air intake duct. Thanks to the slightly wider fuselage of the CAC 27, it could be mounted into the new fuselage halves without problems and the intake duct almost perfectly matches the intake frame from the conversion set. The tailpipe could be easily integrated without any mods, too. The fins had to be glued directly to the fuselage – but this is the way how the Sword kit is actually constructed! Even the FJ-3M’s wings match the different fuselage perfectly. The only modifications I had to make is a slight enlargement of the ventral wing opening at the front and at the read in order to take the deeper wing element from the Sword kit, but that was an easy task. Once in place, the parts blend almost perfectly into each other, just minor PSR was necessary to hide the seams!

 

Other mods include an extended front wheel well for the longer leg from the FJ-3M and a scratched arrester hook installation, made from wire, which is on purpose different from the Y-shaped hook of the Furies.

 

For the canopy I relied on the vacu piece that came with the JAYS set. Fitting it was not easy, though, it took some PSR to blend the windscreen into the rest of the fuselage. Not perfect, but O.K. for such a solution from a conversion set.

 

The underwing pylons were taken from the Sword kit, including the early Sidewinders. I just replaced the drop tanks – the OOB tanks are very wide, and even though they might be authentic for the FJ-3, I was skeptical if they fit at all under the wings with the landing gear extended? In order to avoid trouble and for a more modern look, I replaced them outright with more slender tanks, which were to mimic A-4 tanks (USN FJ-4s frequently carried Skyhawk tanks). They actually come from a Revell F-16 kit, with modified fins. The refueling probe comes from the Sword kit.

 

A last word about the Sword kit: much light, but also much shadow. While I appreciate the fine surface engravings, the recognizably cambered wings, a detailed cockpit with a two-piece resin seat and a pretty landing gear as well as the long air intake, I wonder why the creators totally failed to provide ANY detail of the arrester hook (there is literally nothing, as if this was a land-based Sabre variant!?) or went for doubtful solutions like a front landing gear that consists of five(!) single, tiny parts? Sadism? The resin seat was also broken (despite being packed in a seperate bag), and it did not fit into the cockpit tub at all. Meh!

  

Painting and markings:

From the start I planned to give the model the late RAN A-4Gs’ unique air superiority paint scheme, which was AFAIK introduced in the late Seventies: a two-tone wraparound scheme consisting of “Light Admiralty Grey” (BS381C 697) and “Aircraft Grey” (BS 381C 693). Quite simple, but finding suitable paints was not an easy task, and I based my choice on pictures of the real aircraft (esp. from "buzz" number 880 at the Fleet Air Arm Museum, you find pics of it with very good light condition) rather than rely on (pretty doubtful if not contradictive) recommendations in various painting instructions from models or decal sets.

 

I wanted to keep things simple and settled upon Dark Gull Grey (FS 36231) and Light Blue (FS 35414), both enamel colors from Modelmaster, since both are rather dull interpretations of these tones. Esp. the Light Blue comes quite close to Light Admiralty Grey, even though it should be lighter for more contrast to the darker grey tone. But it has that subtle greenish touch of the original BS tone, and I did not want to mix the colors.

 

The pattern was adapted from the late A-4Gs’ scheme, and the colors were dulled down even more through a light black ink wash. Some post-shading with lighter tones emphasized the contrast between the two colors again. And while it is not an exact representation of the unique RAN air superiority scheme, I think that the overall impression is there.

 

The cockpit interior was painted in very dark grey, while the landing gear, its wells and the inside of the air intake became white. A red rim was painted around the front opening, and the landing gear covers received a red outline, too. The white drop tanks are a detail I took from real world RAN A-4Gs - in the early days of the air superiority scheme, the tanks were frequently still finished in the old USN style livery, hence the white body but fins and tail section already in the updated colors.

 

The decals became a fight, though. As mentioned above, the came from an ESCI kit – and, as expected, the were brittle. All decals with a clear carrier film disintegrated while soaking in water, only those with a fully printed carrier film were more or less usable. One roundel broke and had to be repaired, and the checkered fin flash was a very delicate affair that broke several times, even though I tried to save and repair it with paint. But you can unfortunately see the damage.

 

Most stencils and some replacements (e. g. the “Navy” tag) come from the Sword FJ-3. While these decals are crisply printed, their carrier film is utterly thin, so thin that applying esp. the larger decals turned out to be hazardous and complicated. Another point that did not really convince me about the Sword kit.

 

Finally, the kit was sealed with matt acrylic varnish (Italeri) and some soot stains were added around the exhaust and the gun ports with graphite.

  

In the end, this build looks, despite the troubles and the rather exotic ingredients like a relatively simple Sabre with Australian markings, just with a different Navy livery. You neither immediately recognize the FJ-3 behind it, nor the Avon Sabre’s bigger fuselage, unless you take a close and probably educated look. Very subtle, though.

The RAN air superiority scheme from the late Skyhawks suits the Sabre/Fury-thing well – I like the fact that it is a modern fighter scheme, but, thanks to the tones and the colorful other markings, not as dull and boring like many others, e. g. the contemporary USN "Ghost" scheme. Made me wonder about an early RAAF F-18 in this livery - should look very pretty, too?

Robber Flies are quite capable of handling large prey, and they will even take on large, dangerous prey like bees and wasps. However, unlike bees and wasps, Robber Flies do not sting. Although they do not sting, Robber Flies do bite and their saliva contains neurotoxins to quickly immobilize prey and proteolytic enzymes to dissolve its internal organs so that they can later be easily sucked out. The proboscis of a Robber Fly is specialized for stabbing and sucking, and after one of these flies captures something, it will return to a perch in its territory to suck out its liquefied meal.

  

Mohandas Karamchand Gandhi 2 October 1869 – 30 January 1948) was an Indian lawyer, anti-colonial nationalist and political ethicist who employed nonviolent resistance to lead the successful campaign for India's independence from British rule. He inspired movements for civil rights and freedom across the world. The honorific Mahātmā (from Sanskrit 'great-souled, venerable'), first applied to him in South Africa in 1914, is now used throughout the world.

 

Born and raised in a Hindu family in coastal Gujarat, Gandhi trained in the law at the Inner Temple in London, and was called to the bar in June 1891, at the age of 22. After two uncertain years in India, where he was unable to start a successful law practice, he moved to South Africa in 1893 to represent an Indian merchant in a lawsuit. He went on to live in South Africa for 21 years. There, Gandhi raised a family and first employed nonviolent resistance in a campaign for civil rights. In 1915, aged 45, he returned to India and soon set about organising peasants, farmers, and urban labourers to protest against discrimination and excessive land-tax.

 

Assuming leadership of the Indian National Congress in 1921, Gandhi led nationwide campaigns for easing poverty, expanding women's rights, building religious and ethnic amity, ending untouchability, and, above all, achieving swaraj or self-rule. Gandhi adopted the short dhoti woven with hand-spun yarn as a mark of identification with India's rural poor. He began to live in a self-sufficient residential community, to eat simple food, and undertake long fasts as a means of both introspection and political protest. Bringing anti-colonial nationalism to the common Indians, Gandhi led them in challenging the British-imposed salt tax with the 400 km (250 mi) Dandi Salt March in 1930 and in calling for the British to quit India in 1942. He was imprisoned many times and for many years in both South Africa and India.

 

Gandhi's vision of an independent India based on religious pluralism was challenged in the early 1940s by a Muslim nationalism which demanded a separate homeland for Muslims within British India. In August 1947, Britain granted independence, but the British Indian Empire was partitioned into two dominions, a Hindu-majority India and a Muslim-majority Pakistan. As many displaced Hindus, Muslims, and Sikhs made their way to their new lands, religious violence broke out, especially in the Punjab and Bengal. Abstaining from the official celebration of independence, Gandhi visited the affected areas, attempting to alleviate distress. In the months following, he undertook several hunger strikes to stop the religious violence. The last of these was begun in Delhi on 12 January 1948, when he was 78. The belief that Gandhi had been too resolute in his defense of both Pakistan and Indian Muslims spread among some Hindus in India. Among these was Nathuram Godse, a militant Hindu nationalist from Pune, western India, who assassinated Gandhi by firing three bullets into his chest at an interfaith prayer meeting in Delhi on 30 January 1948.

 

Gandhi's birthday, 2 October, is commemorated in India as Gandhi Jayanti, a national holiday, and worldwide as the International Day of Nonviolence. Gandhi is considered to be the Father of the Nation in post-colonial India. During India's nationalist movement and in several decades immediately after, he was also commonly called Bapu (Gujarati endearment for "father", roughly "papa", "daddy"[

 

Gandhi's father, Karamchand Uttamchand Gandhi (1822–1885), served as the dewan (chief minister) of Porbandar state. His family originated from the then village of Kutiana in what was then Junagadh State. Although he only had been a clerk in the state administration and had an elementary education, Karamchand proved a capable chief minister.

 

During his tenure, Karamchand married four times. His first two wives died young, after each had given birth to a daughter, and his third marriage was childless. In 1857, he sought his third wife's permission to remarry; that year, he married Putlibai (1844–1891), who also came from Junagadh, and was from a Pranami Vaishnava family. Karamchand and Putlibai had four children: a son, Laxmidas (c. 1860–1914); a daughter, Raliatbehn (1862–1960); a second son, Karsandas (c. 1866–1913). and a third son, Mohandas Karamchand Gandhi who was born on 2 October 1869 in Porbandar (also known as Sudamapuri), a coastal town on the Kathiawar Peninsula and then part of the small princely state of Porbandar in the Kathiawar Agency of the British Raj.

 

In 1874, Gandhi's father Karamchand left Porbandar for the smaller state of Rajkot, where he became a counsellor to its ruler, the Thakur Sahib; though Rajkot was a less prestigious state than Porbandar, the British regional political agency was located there, which gave the state's diwan a measure of security. In 1876, Karamchand became diwan of Rajkot and was succeeded as diwan of Porbandar by his brother Tulsidas. His family then rejoined him in Rajkot.

 

As a child, Gandhi was described by his sister Raliat as "restless as mercury, either playing or roaming about. One of his favourite pastimes was twisting dogs' ears." The Indian classics, especially the stories of Shravana and king Harishchandra, had a great impact on Gandhi in his childhood. In his autobiography, he states that they left an indelible impression on his mind. He writes: "It haunted me and I must have acted Harishchandra to myself times without number." Gandhi's early self-identification with truth and love as supreme values is traceable to these epic characters.

 

The family's religious background was eclectic. Mohandas was born into a Gujarati Hindu Modh Bania family. Gandhi's father Karamchand was Hindu and his mother Putlibai was from a Pranami Vaishnava Hindu family. Gandhi's father was of Modh Baniya caste in the varna of Vaishya. His mother came from the medieval Krishna bhakti-based Pranami tradition, whose religious texts include the Bhagavad Gita, the Bhagavata Purana, and a collection of 14 texts with teachings that the tradition believes to include the essence of the Vedas, the Quran and the Bible. Gandhi was deeply influenced by his mother, an extremely pious lady who "would not think of taking her meals without her daily prayers... she would take the hardest vows and keep them without flinching. To keep two or three consecutive fasts was nothing to her."

  

Gandhi (right) with his eldest brother Laxmidas in 1886

At age 9, Gandhi entered the local school in Rajkot, near his home. There, he studied the rudiments of arithmetic, history, the Gujarati language and geography. At the age of 11, he joined the High School in Rajkot, Alfred High School. He was an average student, won some prizes, but was a shy and tongue tied student, with no interest in games; his only companions were books and school lessons.

 

In May 1883, the 13-year-old Mohandas was married to 14-year-old Kasturbai Gokuldas Kapadia (her first name was usually shortened to "Kasturba", and affectionately to "Ba") in an arranged marriage, according to the custom of the region at that time. In the process, he lost a year at school but was later allowed to make up by accelerating his studies. His wedding was a joint event, where his brother and cousin were also married. Recalling the day of their marriage, he once said, "As we didn't know much about marriage, for us it meant only wearing new clothes, eating sweets and playing with relatives." As was the prevailing tradition, the adolescent bride was to spend much time at her parents' house, and away from her husband.

 

Writing many years later, Mohandas described with regret the lustful feelings he felt for his young bride: "even at school I used to think of her, and the thought of nightfall and our subsequent meeting was ever haunting me." He later recalled feeling jealous and possessive of her, such as when she would visit a temple with her girlfriends, and being sexually lustful in his feelings for her.

 

In late 1885, Gandhi's father Karamchand died. Gandhi, then 16 years old, and his wife of age 17 had their first baby, who survived only a few days. The two deaths anguished Gandhi. The Gandhi couple had four more children, all sons: Harilal, born in 1888; Manilal, born in 1892; Ramdas, born in 1897; and Devdas, born in 1900.

 

In November 1887, the 18-year-old Gandhi graduated from high school in Ahmedabad. In January 1888, he enrolled at Samaldas College in Bhavnagar State, then the sole degree-granting institution of higher education in the region. However, he dropped out, and returned to his family in Porbandar.

 

Gandhi had dropped out of the cheapest college he could afford in Bombay. Mavji Dave Joshiji, a Brahmin priest and family friend, advised Gandhi and his family that he should consider law studies in London. In July 1888, his wife Kasturba gave birth to their first surviving son, Harilal. His mother was not comfortable about Gandhi leaving his wife and family, and going so far from home. Gandhi's uncle Tulsidas also tried to dissuade his nephew. Gandhi wanted to go. To persuade his wife and mother, Gandhi made a vow in front of his mother that he would abstain from meat, alcohol and women. Gandhi's brother Laxmidas, who was already a lawyer, cheered Gandhi's London studies plan and offered to support him. Putlibai gave Gandhi her permission and blessing.

 

On 10 August 1888, Gandhi, aged 18, left Porbandar for Mumbai, then known as Bombay. Upon arrival, he stayed with the local Modh Bania community whose elders warned him that England would tempt him to compromise his religion, and eat and drink in Western ways. Despite Gandhi informing them of his promise to his mother and her blessings, he was excommunicated from his caste. Gandhi ignored this, and on 4 September, he sailed from Bombay to London, with his brother seeing him off. Gandhi attended University College, London, where he took classes in English literature with Henry Morley in 1888–1889.

 

He also enrolled at the Inns of Court School of Law in Inner Temple with the intention of becoming a barrister.[38] His childhood shyness and self-withdrawal had continued through his teens. He retained these traits when he arrived in London, but joined a public speaking practice group and overcame his shyness sufficiently to practise law.

 

He demonstrated a keen interest in the welfare of London's impoverished dockland communities. In 1889, a bitter trade dispute broke out in London, with dockers striking for better pay and conditions, and seamen, shipbuilders, factory girls and other joining the strike in solidarity. The strikers were successful, in part due to the mediation of Cardinal Manning, leading Gandhi and an Indian friend to make a point of visiting the cardinal and thanking him for his work.

 

Gandhi's time in London was influenced by the vow he had made to his mother. He tried to adopt "English" customs, including taking dancing lessons. However, he did not appreciate the bland vegetarian food offered by his landlady and was frequently hungry until he found one of London's few vegetarian restaurants. Influenced by Henry Salt's writing, he joined the London Vegetarian Society, and was elected to its executive committee under the aegis of its president and benefactor Arnold Hills. An achievement while on the committee was the establishment of a Bayswater chapter. Some of the vegetarians he met were members of the Theosophical Society, which had been founded in 1875 to further universal brotherhood, and which was devoted to the study of Buddhist and Hindu literature. They encouraged Gandhi to join them in reading the Bhagavad Gita both in translation as well as in the original.

 

Gandhi had a friendly and productive relationship with Hills, but the two men took a different view on the continued LVS membership of fellow committee member Thomas Allinson. Their disagreement is the first known example of Gandhi challenging authority, despite his shyness and temperamental disinclination towards confrontation.

 

Allinson had been promoting newly available birth control methods, but Hills disapproved of these, believing they undermined public morality. He believed vegetarianism to be a moral movement and that Allinson should therefore no longer remain a member of the LVS. Gandhi shared Hills' views on the dangers of birth control, but defended Allinson's right to differ. It would have been hard for Gandhi to challenge Hills; Hills was 12 years his senior and unlike Gandhi, highly eloquent. He bankrolled the LVS and was a captain of industry with his Thames Ironworks company employing more than 6,000 people in the East End of London. He was also a highly accomplished sportsman who later founded the football club West Ham United. In his 1927 An Autobiography, Vol. I, Gandhi wrote:

 

The question deeply interested me...I had a high regard for Mr. Hills and his generosity. But I thought it was quite improper to exclude a man from a vegetarian society simply because he refused to regard puritan morals as one of the objects of the society

 

A motion to remove Allinson was raised, and was debated and voted on by the committee. Gandhi's shyness was an obstacle to his defence of Allinson at the committee meeting. He wrote his views down on paper but shyness prevented him from reading out his arguments, so Hills, the President, asked another committee member to read them out for him. Although some other members of the committee agreed with Gandhi, the vote was lost and Allinson excluded. There were no hard feelings, with Hills proposing the toast at the LVS farewell dinner in honour of Gandhi's return to India.

 

Gandhi, at age 22, was called to the bar in June 1891 and then left London for India, where he learned that his mother had died while he was in London and that his family had kept the news from him. His attempts at establishing a law practice in Bombay failed because he was psychologically unable to cross-examine witnesses. He returned to Rajkot to make a modest living drafting petitions for litigants, but he was forced to stop when he ran afoul of British officer Sam Sunny.

 

In 1893, a Muslim merchant in Kathiawar named Dada Abdullah contacted Gandhi. Abdullah owned a large successful shipping business in South Africa. His distant cousin in Johannesburg needed a lawyer, and they preferred someone with Kathiawari heritage. Gandhi inquired about his pay for the work. They offered a total salary of £105 (~$4,143.31 2023 money) plus travel expenses. He accepted it, knowing that it would be at least a one-year commitment in the Colony of Natal, South Africa, also a part of the British Empire.

 

In April 1893, Gandhi, aged 23, set sail for South Africa to be the lawyer for Abdullah's cousin. He spent 21 years in South Africa, where he developed his political views, ethics and politics.

 

Immediately upon arriving in South Africa, Gandhi faced discrimination because of his skin colour and heritage. He was not allowed to sit with European passengers in the stagecoach and told to sit on the floor near the driver, then beaten when he refused; elsewhere he was kicked into a gutter for daring to walk near a house, in another instance thrown off a train at Pietermaritzburg after refusing to leave the first-class. He sat in the train station, shivering all night and pondering if he should return to India or protest for his rights. He chose to protest and was allowed to board the train the next day. In another incident, the magistrate of a Durban court ordered Gandhi to remove his turban, which he refused to do. Indians were not allowed to walk on public footpaths in South Africa. Gandhi was kicked by a police officer out of the footpath onto the street without warning.

 

When Gandhi arrived in South Africa, according to Herman, he thought of himself as "a Briton first, and an Indian second". However, the prejudice against him and his fellow Indians from British people that Gandhi experienced and observed deeply bothered him. He found it humiliating, struggling to understand how some people can feel honour or superiority or pleasure in such inhumane practices. Gandhi began to question his people's standing in the British Empire.

 

The Abdullah case that had brought him to South Africa concluded in May 1894, and the Indian community organised a farewell party for Gandhi as he prepared to return to India. However, a new Natal government discriminatory proposal led to Gandhi extending his original period of stay in South Africa. He planned to assist Indians in opposing a bill to deny them the right to vote, a right then proposed to be an exclusive European right. He asked Joseph Chamberlain, the British Colonial Secretary, to reconsider his position on this bill. Though unable to halt the bill's passage, his campaign was successful in drawing attention to the grievances of Indians in South Africa. He helped found the Natal Indian Congress in 1894, and through this organisation, he moulded the Indian community of South Africa into a unified political force. In January 1897, when Gandhi landed in Durban, a mob of white settlers attacked him and he escaped only through the efforts of the wife of the police superintendent. However, he refused to press charges against any member of the mob.

 

During the Boer War, Gandhi volunteered in 1900 to form a group of stretcher-bearers as the Natal Indian Ambulance Corps. According to Arthur Herman, Gandhi wanted to disprove the British colonial stereotype that Hindus were not fit for "manly" activities involving danger and exertion, unlike the Muslim "martial races". Gandhi raised eleven hundred Indian volunteers, to support British combat troops against the Boers. They were trained and medically certified to serve on the front lines. They were auxiliaries at the Battle of Colenso to a White volunteer ambulance corps. At the battle of Spion Kop Gandhi and his bearers moved to the front line and had to carry wounded soldiers for miles to a field hospital because the terrain was too rough for the ambulances. Gandhi and thirty-seven other Indians received the Queen's South Africa Medal.

 

In 1906, the Transvaal government promulgated a new Act compelling registration of the colony's Indian and Chinese populations. At a mass protest meeting held in Johannesburg on 11 September that year, Gandhi adopted his still evolving methodology of Satyagraha (devotion to the truth), or nonviolent protest, for the first time. According to Anthony Parel, Gandhi was also influenced by the Tamil moral text Tirukkuṛaḷ after Leo Tolstoy mentioned it in their correspondence that began with "A Letter to a Hindu". Gandhi urged Indians to defy the new law and to suffer the punishments for doing so. Gandhi's ideas of protests, persuasion skills and public relations had emerged. He took these back to India in 1915.

 

Gandhi focused his attention on Indians and Africans while he was in South Africa. He initially was not interested in politics. This changed, however, after he was discriminated against and bullied, such as by being thrown out of a train coach because of his skin colour by a white train official. After several such incidents with Whites in South Africa, Gandhi's thinking and focus changed, and he felt he must resist this and fight for rights. He entered politics by forming the Natal Indian Congress. According to Ashwin Desai and Goolam Vahed, Gandhi's views on racism are contentious in some cases, but that changed afterward.[further explanation needed] Gandhi suffered persecution from the beginning in South Africa. Like with other coloured people, white officials denied him his rights, and the press and those in the streets bullied and called him a "parasite", "semi-barbarous", "canker", "squalid coolie", "yellow man", and other epithets. People would spit on him as an expression of racial hate.

 

While in South Africa, Gandhi focused on the racial persecution of Indians before he started to focus on racism against Africans. In some cases, state Desai and Vahed, his behaviour was one of being a willing part of racial stereotyping and African exploitation. During a speech in September 1896, Gandhi complained that the whites in the British colony of South Africa were "degrading the Indian to the level of a raw Kaffir". Scholars cite it as an example of evidence that Gandhi at that time thought of Indians and black South Africans differently. As another example given by Herman, Gandhi, at the age of 24, prepared a legal brief for the Natal Assembly in 1895, seeking voting rights for Indians. Gandhi cited race history and European Orientalists' opinions that "Anglo-Saxons and Indians are sprung from the same Aryan stock or rather the Indo-European peoples", and argued that Indians should not be grouped with the Africans.

 

Years later, Gandhi and his colleagues served and helped Africans as nurses and by opposing racism. The Nobel Peace Prize winner Nelson Mandela is among admirers of Gandhi's efforts to fight against racism in Africa. The general image of Gandhi, state Desai and Vahed, has been reinvented since his assassination as though he was always a saint, when in reality his life was more complex, contained inconvenient truths, and was one that changed over time.[68] Scholars have also pointed the evidence to a rich history of co-operation and efforts by Gandhi and Indian people with nonwhite South Africans against persecution of Africans and the Apartheid.

 

In 1906, when the Bambatha Rebellion broke out in the colony of Natal, the then 36-year-old Gandhi, despite sympathising with the Zulu rebels, encouraged Indian South Africans to form a volunteer stretcher-bearer unit. Writing in the Indian Opinion, Gandhi argued that military service would be beneficial to the Indian community and claimed it would give them "health and happiness". Gandhi eventually led a volunteer mixed unit of Indian and African stretcher-bearers to treat wounded combatants during the suppression of the rebellion.

 

The medical unit commanded by Gandhi operated for less than two months before being disbanded.[72] After the suppression of the rebellion, the colonial establishment showed no interest in extending to the Indian community the civil rights granted to white South Africans. This led Gandhi to becoming disillusioned with the Empire and aroused a spiritual awakening with him; historian Arthur L. Herman wrote that his African experience was a part of his great disillusionment with the West, transforming him into an "uncompromising non-cooperator".

 

By 1910, Gandhi's newspaper, Indian Opinion, was covering reports on discrimination against Africans by the colonial regime. Gandhi remarked that the Africans are "alone are the original inhabitants of the land. … The whites, on the other hand, have occupied the land forcibly and appropriated it to themselves."

 

In 1910, Gandhi established, with the help of his friend Hermann Kallenbach, an idealistic community they named Tolstoy Farm near Johannesburg. There he nurtured his policy of peaceful resistance.

 

In the years after black South Africans gained the right to vote in South Africa (1994), Gandhi was proclaimed a national hero with numerous monuments.

 

At the request of Gopal Krishna Gokhale, conveyed to him by C. F. Andrews, Gandhi returned to India in 1915. He brought an international reputation as a leading Indian nationalist, theorist and community organiser.

 

Gandhi joined the Indian National Congress and was introduced to Indian issues, politics and the Indian people primarily by Gokhale. Gokhale was a key leader of the Congress Party best known for his restraint and moderation, and his insistence on working inside the system. Gandhi took Gokhale's liberal approach based on British Whiggish traditions and transformed it to make it look Indian.

 

Gandhi took leadership of the Congress in 1920 and began escalating demands until on 26 January 1930 the Indian National Congress declared the independence of India. The British did not recognise the declaration but negotiations ensued, with the Congress taking a role in provincial government in the late 1930s. Gandhi and the Congress withdrew their support of the Raj when the Viceroy declared war on Germany in September 1939 without consultation. Tensions escalated until Gandhi demanded immediate independence in 1942 and the British responded by imprisoning him and tens of thousands of Congress leaders. Meanwhile, the Muslim League did co-operate with Britain and moved, against Gandhi's strong opposition, to demands for a totally separate Muslim state of Pakistan. In August 1947 the British partitioned the land with India and Pakistan each achieving independence on terms that Gandhi disapproved.

 

In April 1918, during the latter part of World War I, the Viceroy invited Gandhi to a War Conference in Delhi. Gandhi agreed to actively recruit Indians for the war effort. In contrast to the Zulu War of 1906 and the outbreak of World War I in 1914, when he recruited volunteers for the Ambulance Corps, this time Gandhi attempted to recruit combatants. In a June 1918 leaflet entitled "Appeal for Enlistment", Gandhi wrote "To bring about such a state of things we should have the ability to defend ourselves, that is, the ability to bear arms and to use them... If we want to learn the use of arms with the greatest possible despatch, it is our duty to enlist ourselves in the army." He did, however, stipulate in a letter to the Viceroy's private secretary that he "personally will not kill or injure anybody, friend or foe."

 

Gandhi's war recruitment campaign brought into question his consistency on nonviolence. Gandhi's private secretary noted that "The question of the consistency between his creed of 'Ahimsa' (nonviolence) and his recruiting campaign was raised not only then but has been discussed ever since."

 

In July 1918, Gandhi admitted that he couldn't persuade even one individual to enlist for the world war. "So far I have not a single recruit to my credit apart," Gandhi wrote. He added: "They object because they fear to die."

 

Gandhi's first major achievement came in 1917 with the Champaran agitation in Bihar. The Champaran agitation pitted the local peasantry against largely Anglo-Indian plantation owners who were backed by the local administration. The peasants were forced to grow indigo (Indigofera sp.), a cash crop for Indigo dye whose demand had been declining over two decades, and were forced to sell their crops to the planters at a fixed price. Unhappy with this, the peasantry appealed to Gandhi at his ashram in Ahmedabad. Pursuing a strategy of nonviolent protest, Gandhi took the administration by surprise and won concessions from the authorities.

 

In 1918, Kheda was hit by floods and famine and the peasantry was demanding relief from taxes. Gandhi moved his headquarters to Nadiad, organising scores of supporters and fresh volunteers from the region, the most notable being Vallabhbhai Patel. Using non-co-operation as a technique, Gandhi initiated a signature campaign where peasants pledged non-payment of revenue even under the threat of confiscation of land. A social boycott of mamlatdars and talatdars (revenue officials within the district) accompanied the agitation. Gandhi worked hard to win public support for the agitation across the country. For five months, the administration refused, but by the end of May 1918, the Government gave way on important provisions and relaxed the conditions of payment of revenue tax until the famine ended. In Kheda, Vallabhbhai Patel represented the farmers in negotiations with the British, who suspended revenue collection and released all the prisoners.

 

In 1919, following World War I, Gandhi (aged 49) sought political co-operation from Muslims in his fight against British imperialism by supporting the Ottoman Empire that had been defeated in the World War. Before this initiative of Gandhi, communal disputes and religious riots between Hindus and Muslims were common in British India, such as the riots of 1917–18. Gandhi had already supported the British crown with resources and by recruiting Indian soldiers to fight the war in Europe on the British side. This effort of Gandhi was in part motivated by the British promise to reciprocate the help with swaraj (self-government) to Indians after the end of World War I. The British government had offered, instead of self-government, minor reforms instead, disappointing Gandhi. Gandhi announced his satyagraha (civil disobedience) intentions. The British colonial officials made their counter move by passing the Rowlatt Act, to block Gandhi's movement. The Act allowed the British government to treat civil disobedience participants as criminals and gave it the legal basis to arrest anyone for "preventive indefinite detention, incarceration without judicial review or any need for a trial".

 

Gandhi felt that Hindu-Muslim co-operation was necessary for political progress against the British. He leveraged the Khilafat movement, wherein Sunni Muslims in India, their leaders such as the sultans of princely states in India and Ali brothers championed the Turkish Caliph as a solidarity symbol of Sunni Islamic community (ummah). They saw the Caliph as their means to support Islam and the Islamic law after the defeat of Ottoman Empire in World War I. Gandhi's support to the Khilafat movement led to mixed results. It initially led to a strong Muslim support for Gandhi. However, the Hindu leaders including Rabindranath Tagore questioned Gandhi's leadership because they were largely against recognising or supporting the Sunni Islamic Caliph in Turkey.

 

The increasing Muslim support for Gandhi, after he championed the Caliph's cause, temporarily stopped the Hindu-Muslim communal violence. It offered evidence of inter-communal harmony in joint Rowlatt satyagraha demonstration rallies, raising Gandhi's stature as the political leader to the British. His support for the Khilafat movement also helped him sideline Muhammad Ali Jinnah, who had announced his opposition to the satyagraha non-co-operation movement approach of Gandhi. Jinnah began creating his independent support, and later went on to lead the demand for West and East Pakistan. Though they agreed in general terms on Indian independence, they disagreed on the means of achieving this. Jinnah was mainly interested in dealing with the British via constitutional negotiation, rather than attempting to agitate the masses.

 

In 1922 the Khilafat movement gradually collapsed following the end of the non-cooperation movement with the arrest of Gandhi. A number of Muslim leaders and delegates abandoned Gandhi and Congress. Hindu-Muslim communal conflicts reignited. Deadly religious riots re-appeared in numerous cities, with 91 in United Provinces of Agra and Oudh alone.

 

With his book Hind Swaraj (1909) Gandhi, aged 40, declared that British rule was established in India with the co-operation of Indians and had survived only because of this co-operation. If Indians refused to co-operate, British rule would collapse and swaraj (Indian independence) would come.

 

In February 1919, Gandhi cautioned the Viceroy of India with a cable communication that if the British were to pass the Rowlatt Act, he would appeal to Indians to start civil disobedience. The British government ignored him and passed the law, stating it would not yield to threats. The satyagraha civil disobedience followed, with people assembling to protest the Rowlatt Act. On 30 March 1919, British law officers opened fire on an assembly of unarmed people, peacefully gathered, participating in satyagraha in Delhi.

 

People rioted in retaliation. On 6 April 1919, a Hindu festival day, he asked a crowd to remember not to injure or kill British people, but to express their frustration with peace, to boycott British goods and burn any British clothing they owned. He emphasised the use of non-violence to the British and towards each other, even if the other side used violence. Communities across India announced plans to gather in greater numbers to protest. Government warned him to not enter Delhi. Gandhi defied the order. On 9 April, Gandhi was arrested.

 

On 13 April 1919, people including women with children gathered in an Amritsar park, and British Indian Army officer Reginald Dyer surrounded them and ordered troops under his command to fire on them. The resulting Jallianwala Bagh massacre (or Amritsar massacre) of hundreds of Sikh and Hindu civilians enraged the subcontinent, but was supported by some Britons and parts of the British media as a necessary response. Gandhi in Ahmedabad, on the day after the massacre in Amritsar, did not criticise the British and instead criticised his fellow countrymen for not exclusively using 'love' to deal with the 'hate' of the British government. Gandhi demanded that the Indian people stop all violence, stop all property destruction, and went on fast-to-death to pressure Indians to stop their rioting.

 

The massacre and Gandhi's non-violent response to it moved many, but also made some Sikhs and Hindus upset that Dyer was getting away with murder. Investigation committees were formed by the British, which Gandhi asked Indians to boycott.[109] The unfolding events, the massacre and the British response, led Gandhi to the belief that Indians will never get a fair equal treatment under British rulers, and he shifted his attention to swaraj and political independence for India. In 1921, Gandhi was the leader of the Indian National Congress. He reorganised the Congress. With Congress now behind him, and Muslim support triggered by his backing the Khilafat movement to restore the Caliph in Turkey, Gandhi had the political support and the attention of the British Raj.

 

Gandhi expanded his nonviolent non-co-operation platform to include the swadeshi policy – the boycott of foreign-made goods, especially British goods. Linked to this was his advocacy that khadi (homespun cloth) be worn by all Indians instead of British-made textiles. Gandhi exhorted Indian men and women, rich or poor, to spend time each day spinning khadi in support of the independence movement. In addition to boycotting British products, Gandhi urged the people to boycott British institutions and law courts, to resign from government employment, and to forsake British titles and honours. Gandhi thus began his journey aimed at crippling the British India government economically, politically and administratively.

 

The appeal of "Non-cooperation" grew, its social popularity drew participation from all strata of Indian society. Gandhi was arrested on 10 March 1922, tried for sedition, and sentenced to six years' imprisonment. He began his sentence on 18 March 1922. With Gandhi isolated in prison, the Indian National Congress split into two factions, one led by Chitta Ranjan Das and Motilal Nehru favouring party participation in the legislatures, and the other led by Chakravarti Rajagopalachari and Sardar Vallabhbhai Patel, opposing this move. Furthermore, co-operation among Hindus and Muslims ended as Khilafat movement collapsed with the rise of Atatürk in Turkey. Muslim leaders left the Congress and began forming Muslim organisations. The political base behind Gandhi had broken into factions. Gandhi was released in February 1924 for an appendicitis operation, having served only two years.

 

After his early release from prison for political crimes in 1924, over the second half of the 1920s Gandhi continued to pursue swaraj. He pushed through a resolution at the Calcutta Congress in December 1928 calling on the British government to grant India dominion status or face a new campaign of non-cooperation with complete independence for the country as its goal. After his support for World War I with Indian combat troops, and the failure of Khilafat movement in preserving the rule of Caliph in Turkey, followed by a collapse in Muslim support for his leadership, some such as Subhas Chandra Bose and Bhagat Singh questioned his values and non-violent approach. While many Hindu leaders championed a demand for immediate independence, Gandhi revised his own call to a one-year wait, instead of two.

 

The British did not respond favourably to Gandhi's proposal. British political leaders such as Lord Birkenhead and Winston Churchill announced opposition to "the appeasers of Gandhi" in their discussions with European diplomats who sympathised with Indian demands. On 31 December 1929, an Indian flag was unfurled in Lahore. Gandhi led Congress in a celebration on 26 January 1930 of India's Independence Day in Lahore. This day was commemorated by almost every other Indian organisation. Gandhi then launched a new Satyagraha against the British salt tax in March 1930. Gandhi sent an ultimatum in the form of a letter personally addressed to Lord Irwin, the viceroy of India, on 2 March. Gandhi condemned British rule in the letter, describing it as "a curse" that "has impoverished the dumb millions by a system of progressive exploitation and by a ruinously expensive military and civil administration...It has reduced us politically to serfdom." Gandhi also mentioned in the letter that the viceroy received a salary "over five thousand times India's average income." In the letter, Gandhi also stressed his continued adherence to non-violent forms of protest.

 

This was highlighted by the Salt March to Dandi from 12 March to 6 April, where, together with 78 volunteers, he marched 388 kilometres (241 mi) from Ahmedabad to Dandi, Gujarat to make salt himself, with the declared intention of breaking the salt laws. The march took 25 days to cover 240 miles with Gandhi speaking to often huge crowds along the way. Thousands of Indians joined him in Dandi. On 5 May he was interned under a regulation dating from 1827 in anticipation of a protest that he had planned. The protest at Dharasana salt works on 21 May went ahead without him see. A horrified American journalist, Webb Miller, described the British response thus:

 

In complete silence the Gandhi men drew up and halted a hundred yards from the stockade. A picked column advanced from the crowd, waded the ditches and approached the barbed wire stockade... at a word of command, scores of native policemen rushed upon the advancing marchers and rained blows on their heads with their steel-shot lathis [long bamboo sticks]. Not one of the marchers even raised an arm to fend off blows. They went down like ninepins. From where I stood I heard the sickening whack of the clubs on unprotected skulls... Those struck down fell sprawling, unconscious or writhing with fractured skulls or broken shoulders.

 

This went on for hours until some 300 or more protesters had been beaten, many seriously injured and two killed. At no time did they offer any resistance.

 

This campaign was one of his most successful at upsetting British hold on India; Britain responded by imprisoning over 60,000 people. Congress estimates, however, put the figure at 90,000. Among them was one of Gandhi's lieutenants, Jawaharlal Nehru.

 

According to Sarma, Gandhi recruited women to participate in the salt tax campaigns and the boycott of foreign products, which gave many women a new self-confidence and dignity in the mainstream of Indian public life. However, other scholars such as Marilyn French state that Gandhi barred women from joining his civil disobedience movement because he feared he would be accused of using women as a political shield. When women insisted on joining the movement and participating in public demonstrations, Gandhi asked the volunteers to get permissions of their guardians and only those women who can arrange child-care should join him. Regardless of Gandhi's apprehensions and views, Indian women joined the Salt March by the thousands to defy the British salt taxes and monopoly on salt mining. After Gandhi's arrest, the women marched and picketed shops on their own, accepting violence and verbal abuse from British authorities for the cause in the manner Gandhi inspired.

 

Indian Congress in the 1920s appealed to Andhra Pradesh peasants by creating Telugu language plays that combined Indian mythology and legends, linked them to Gandhi's ideas, and portrayed Gandhi as a messiah, a reincarnation of ancient and medieval Indian nationalist leaders and saints. The plays built support among peasants steeped in traditional Hindu culture, according to Murali, and this effort made Gandhi a folk hero in Telugu speaking villages, a sacred messiah-like figure.

 

According to Dennis Dalton, it was Gandhi's ideas that were responsible for his wide following. Gandhi criticised Western civilisation as one driven by "brute force and immorality", contrasting it with his categorisation of Indian civilisation as one driven by "soul force and morality". Gandhi captured the imagination of the people of his heritage with his ideas about winning "hate with love". These ideas are evidenced in his pamphlets from the 1890s, in South Africa, where too he was popular among the Indian indentured workers. After he returned to India, people flocked to him because he reflected their values.

 

Gandhi also campaigned hard going from one rural corner of the Indian subcontinent to another. He used terminology and phrases such as Rama-rajya from Ramayana, Prahlada as a paradigmatic icon, and such cultural symbols as another facet of swaraj and satyagraha. During his lifetime, these ideas sounded strange outside India, but they readily and deeply resonated with the culture and historic values of his people.

 

The government, represented by Lord Irwin, decided to negotiate with Gandhi. The Gandhi–Irwin Pact was signed in March 1931. The British Government agreed to free all political prisoners, in return for the suspension of the civil disobedience movement. According to the pact, Gandhi was invited to attend the Round Table Conference in London for discussions and as the sole representative of the Indian National Congress. The conference was a disappointment to Gandhi and the nationalists. Gandhi expected to discuss India's independence, while the British side focused on the Indian princes and Indian minorities rather than on a transfer of power. Lord Irwin's successor, Lord Willingdon, took a hard line against India as an independent nation, began a new campaign of controlling and subduing the nationalist movement. Gandhi was again arrested, and the government tried and failed to negate his influence by completely isolating him from his followers.

 

In Britain, Winston Churchill, a prominent Conservative politician who was then out of office but later became its prime minister, became a vigorous and articulate critic of Gandhi and opponent of his long-term plans. Churchill often ridiculed Gandhi, saying in a widely reported 1931 speech:

 

It is alarming and also nauseating to see Mr Gandhi, a seditious Middle Temple lawyer, now posing as a fakir of a type well known in the East, striding half-naked up the steps of the Vice-regal palace....to parley on equal terms with the representative of the King-Emperor.

 

Churchill's bitterness against Gandhi grew in the 1930s. He called Gandhi as the one who was "seditious in aim" whose evil genius and multiform menace was attacking the British empire. Churchill called him a dictator, a "Hindu Mussolini", fomenting a race war, trying to replace the Raj with Brahmin cronies, playing on the ignorance of Indian masses, all for selfish gain. Churchill attempted to isolate Gandhi, and his criticism of Gandhi was widely covered by European and American press. It gained Churchill sympathetic support, but it also increased support for Gandhi among Europeans. The developments heightened Churchill's anxiety that the "British themselves would give up out of pacifism and misplaced conscience".

 

During the discussions between Gandhi and the British government over 1931–32 at the Round Table Conferences, Gandhi, now aged about 62, sought constitutional reforms as a preparation to the end of colonial British rule, and begin the self-rule by Indians. The British side sought reforms that would keep the Indian subcontinent as a colony. The British negotiators proposed constitutional reforms on a British Dominion model that established separate electorates based on religious and social divisions. The British questioned the Congress party and Gandhi's authority to speak for all of India. They invited Indian religious leaders, such as Muslims and Sikhs, to press their demands along religious lines, as well as B. R. Ambedkar as the representative leader of the untouchables. Gandhi vehemently opposed a constitution that enshrined rights or representations based on communal divisions, because he feared that it would not bring people together but divide them, perpetuate their status, and divert the attention from India's struggle to end the colonial rule.

 

The Second Round Table conference was the only time he left India between 1914 and his death in 1948. He declined the government's offer of accommodation in an expensive West End hotel, preferring to stay in the East End, to live among working-class people, as he did in India. He based himself in a small cell-bedroom at Kingsley Hall for the three-month duration of his stay and was enthusiastically received by East Enders. During this time he renewed his links with the British vegetarian movement.

 

After Gandhi returned from the Second Round Table conference, he started a new satyagraha. He was arrested and imprisoned at the Yerwada Jail, Pune. While he was in prison, the British government enacted a new law that granted untouchables a separate electorate. It came to be known as the Communal Award. In protest, Gandhi started a fast-unto-death, while he was held in prison. The resulting public outcry forced the government, in consultations with Ambedkar, to replace the Communal Award with a compromise Poona Pact.

 

In 1934 Gandhi resigned from Congress party membership. He did not disagree with the party's position but felt that if he resigned, his popularity with Indians would cease to stifle the party's membership, which actually varied, including communists, socialists, trade unionists, students, religious conservatives, and those with pro-business convictions, and that these various voices would get a chance to make themselves heard. Gandhi also wanted to avoid being a target for Raj propaganda by leading a party that had temporarily accepted political accommodation with the Raj.

 

Gandhi returned to active politics again in 1936, with the Nehru presidency and the Lucknow session of the Congress. Although Gandhi wanted a total focus on the task of winning independence and not speculation about India's future, he did not restrain the Congress from adopting socialism as its goal. Gandhi had a clash with Subhas Chandra Bose, who had been elected president in 1938, and who had previously expressed a lack of faith in nonviolence as a means of protest. Despite Gandhi's opposition, Bose won a second term as Congress President, against Gandhi's nominee, Bhogaraju Pattabhi Sitaramayya. Gandhi declared that Sitaramayya's defeat was his defeat. Bose later left the Congress when the All-India leaders resigned en masse in protest of his abandonment of the principles introduced by Gandhi.

 

Gandhi opposed providing any help to the British war effort and he campaigned against any Indian participation in World War II. The British government responded with the arrests of Gandhi and many other Congress leaders and killed over 1,000 Indians who participated in this movement. A number of violent attacks were also carried out by the nationalists against the British government. While Gandhi's campaign did not enjoy the support of a number of Indian leaders, and over 2.5 million Indians volunteered and joined the British military to fight on various fronts of the Allied Forces, the movement played a role in weakening the control over the South Asian region by the British regime and it ultimately paved the way for Indian independence.

 

Gandhi's opposition to the Indian participation in World War II was motivated by his belief that India could not be party to a war ostensibly being fought for democratic freedom while that freedom was denied to India itself. He also condemned Nazism and Fascism, a view which won endorsement of other Indian leaders. As the war progressed, Gandhi intensified his demand for independence, calling for the British to Quit India in a 1942 speech in Mumbai. This was Gandhi's and the Congress Party's most definitive revolt aimed at securing the British exit from India. The British government responded quickly to the Quit India speech, and within hours after Gandhi's speech arrested Gandhi and all the members of the Congress Working Committee. His countrymen retaliated the arrests by damaging or burning down hundreds of government owned railway stations, police stations, and cutting down telegraph wires.

 

In 1942, Gandhi now nearing age 73, urged his people to completely stop co-operating with the imperial government. In this effort, he urged that they neither kill nor injure British people, but be willing to suffer and die if violence is initiated by the British officials. He clarified that the movement would not be stopped because of any individual acts of violence, saying that the "ordered anarchy" of "the present system of administration" was "worse than real anarchy." He urged Indians to karo ya maro ("do or die") in the cause of their rights and freedoms.

 

Gandhi's arrest lasted two years, as he was held in the Aga Khan Palace in Pune. During this period, his long time secretary Mahadev Desai died of a heart attack, his wife Kasturba died after 18 months' imprisonment on 22 February 1944; and Gandhi suffered a severe malaria attack. While in jail, he agreed to an interview with Stuart Gelder, a British journalist. Gelder then composed and released an interview summary, cabled it to the mainstream press, that announced sudden concessions Gandhi was willing to make, comments that shocked his countrymen, the Congress workers and even Gandhi. The latter two claimed that it distorted what Gandhi actually said on a range of topics and falsely repudiated the Quit India movement.

 

Gandhi was released before the end of the war on 6 May 1944 because of his failing health and necessary surgery; the Raj did not want him to die in prison and enrage the nation. He came out of detention to an altered political scene – the Muslim League for example, which a few years earlier had appeared marginal, "now occupied the centre of the political stage" and the topic of Jinnah's campaign for Pakistan was a major talking point. Gandhi and Jinnah had extensive correspondence and the two men met several times over a period of two weeks in September 1944 at Jinnah's house in Bombay, where Gandhi insisted on a united religiously plural and independent India which included Muslims and non-Muslims of the Indian subcontinent coexisting. Jinnah rejected this proposal and insisted instead for partitioning the subcontinent on religious lines to create a separate Muslim homeland (later Pakistan).These discussions continued through 1947.

 

While the leaders of Congress languished in jail, the other parties supported the war and gained organisational strength. Underground publications flailed at the ruthless suppression of Congress, but it had little control over events. At the end of the war, the British gave clear indications that power would be transferred to Indian hands. At this point Gandhi called off the struggle, and around 100,000 political prisoners were released, including the Congress's leadership.

 

Gandhi opposed the partition of the Indian subcontinent along religious lines. The Indian National Congress and Gandhi called for the British to Quit India. However, the All-India Muslim League demanded "Divide and Quit India". Gandhi suggested an agreement which required the Congress and the Muslim League to co-operate and attain independence under a provisional government, thereafter, the question of partition could be resolved by a plebiscite in the districts with a Muslim majority.

 

Jinnah rejected Gandhi's proposal and called for Direct Action Day, on 16 August 1946, to press Muslims to publicly gather in cities and support his proposal for the partition of the Indian subcontinent into a Muslim state and non-Muslim state. Huseyn Shaheed Suhrawardy, the Muslim League Chief Minister of Bengal – now Bangladesh and West Bengal, gave Calcutta's police special holiday to celebrate the Direct Action Day. The Direct Action Day triggered a mass murder of Calcutta Hindus and the torching of their property, and holidaying police were missing to contain or stop the conflict. The British government did not order its army to move in to contain the violence. The violence on Direct Action Day led to retaliatory violence against Muslims across India. Thousands of Hindus and Muslims were murdered, and tens of thousands were injured in the cycle of violence in the days that followed. Gandhi visited the most riot-prone areas to appeal a stop to the massacres.

 

Archibald Wavell, the Viceroy and Governor-General of British India for three years through February 1947, had worked with Gandhi and Jinnah to find a common ground, before and after accepting Indian independence in principle. Wavell condemned Gandhi's character and motives as well as his ideas. Wavell accused Gandhi of harbouring the single minded idea to "overthrow British rule and influence and to establish a Hindu raj", and called Gandhi a "malignant, malevolent, exceedingly shrewd" politician. Wavell feared a civil war on the Indian subcontinent, and doubted Gandhi would be able to stop it.

 

The British reluctantly agreed to grant independence to the people of the Indian subcontinent, but accepted Jinnah's proposal of partitioning the land into Pakistan and India. Gandhi was involved in the final negotiations, but Stanley Wolpert states the "plan to carve up British India was never approved of or accepted by Gandhi".

 

The partition was controversial and violently disputed. More than half a million were killed in religious riots as 10 million to 12 million non-Muslims (Hindus and Sikhs mostly) migrated from Pakistan into India, and Muslims migrated from India into Pakistan, across the newly created borders of India, West Pakistan and East Pakistan.

 

Gandhi spent the day of independence not celebrating the end of the British rule but appealing for peace among his countrymen by fasting and spinning in Calcutta on 15 August 1947. The partition had gripped the Indian subcontinent with religious violence and the streets were filled with corpses. Gandhi's fasting and protests are credited for stopping the religious riots and communal violence.

 

At 5:17 pm on 30 January 1948, Gandhi was with his grandnieces in the garden of Birla House (now Gandhi Smriti), on his way to address a prayer meeting, when Nathuram Godse, a Hindu nationalist, fired three bullets into his chest from a pistol at close range. According to some accounts, Gandhi died instantly. In other accounts, such as one prepared by an eyewitness journalist, Gandhi was carried into the Birla House, into a bedroom. There he died about 30 minutes later as one of Gandhi's family members read verses from Hindu scriptures.

 

Prime Minister Jawaharlal Nehru addressed his countrymen over the All-India Radio saying:

 

Friends and comrades, the light has gone out of our lives, and there is darkness everywhere, and I do not quite know what to tell you or how to say it. Our beloved leader, Bapu as we called him, the father of the nation, is no more. Perhaps I am wrong to say that; nevertheless, we will not see him again, as we have seen him for these many years, we will not run to him for advice or seek solace from him, and that is a terrible blow, not only for me, but for millions and millions in this country.

 

Godse, a Hindu nationalist, with links to the Hindu Mahasabha and the Rashtriya Swayamsevak Sangh, made no attempt to escape; several other conspirators were soon arrested as well. The accused were Nathuram Vinayak Godse, Narayan Apte, Vinayak Damodar Savarkar, Shankar Kistayya, Dattatraya Parchure, Vishnu Karkare, Madanlal Pahwa, and Gopal Godse.

 

The trial began on 27 May 1948 and ran for eight months before Justice Atma Charan passed his final order on 10 February 1949. The prosecution called 149 witnesses, the defense none. The court found all of the defendants except one guilty as charged. Eight men were convicted for the murder conspiracy, and others were convicted for violation of the Explosive Substances Act. Savarkar was acquitted and set free. Nathuram Godse and Narayan Apte were sentenced to death by hanging and the remaining six (including Godse's brother, Gopal) were sentenced to life imprisonment.

 

Gandhi's death was mourned nationwide. Over a million people joined the five-mile-long funeral procession that took over five hours to reach Raj Ghat from Birla house, where he was assassinated, and another million watched the procession pass by. Gandhi's body was transported on a weapons carrier, whose chassis was dismantled overnight to allow a high-floor to be installed so that people could catch a glimpse of his body. The engine of the vehicle was not used; instead four drag-ropes held by 50 people each pulled the vehicle. All Indian-owned establishments in London remained closed in mourning as thousands of people from all faiths and denominations and Indians from all over Britain converged at India House in London.

 

Gandhi was cremated in accordance with Hindu tradition. His ashes were poured into urns which were sent across India for memorial services. Most of the ashes were immersed at the Sangam at Allahabad on 12 February 1948, but some were secretly taken away. In 1997, Tushar Gandhi immersed the contents of one urn, found in a bank vault and reclaimed through the courts, at the Sangam at Allahabad. Some of Gandhi's ashes were scattered at the source of the Nile River near Jinja, Uganda, and a memorial plaque marks the event. On 30 January 2008, the contents of another urn were immersed at Girgaum Chowpatty. Another urn is at the palace of the Aga Khan in Pune (where Gandhi was held as a political prisoner from 1942 to 1944) and another in the Self-Realization Fellowship Lake Shrine in Los Angeles.

 

The Birla House site where Gandhi was assassinated is now a memorial called Gandhi Smriti. The place near Yamuna river where he was cremated is the Rāj Ghāt memorial in New Delhi. A black marble platform, it bears the epigraph "Hē Rāma" (Devanagari: हे ! राम or, Hey Raam). These are said to be Gandhi's last words after he was shot.

 

New York, often called New York City or simply NYC, is the most populous city in the United States, located at the southern tip of New York State on one of the world's largest natural harbors. The city comprises five boroughs, each of which is coextensive with a respective county. It is a global city and a cultural, financial, high-tech, entertainment, and media center with a significant influence on commerce, health care, scientific output, life sciences, research, technology, education, politics, tourism, dining, art, fashion, and sports. Home to the headquarters of the United Nations, New York is an important center for international diplomacy, and is sometimes described as the world's most important city and the capital of the world.

 

With an estimated population in 2022 of 8,335,897 distributed over 300.46 square miles (778.2 km2), the city is the most densely populated major city in the United States. New York has more than double the population of Los Angeles, the nation's second-most populous city. New York is the geographical and demographic center of both the Northeast megalopolis and the New York metropolitan area, the largest metropolitan area in the U.S. by both population and urban area. With more than 20.1 million people in its metropolitan statistical area and 23.5 million in its combined statistical area as of 2020, New York City is one of the world's most populous megacities. The city and its metropolitan area are the premier gateway for legal immigration to the United States. As many as 800 languages are spoken in New York, making it the most linguistically diverse city in the world. In 2021, the city was home to nearly 3.1 million residents born outside the U.S., the largest foreign-born population of any city in the world.

 

New York City traces its origins to Fort Amsterdam and a trading post founded on the southern tip of Manhattan Island by Dutch colonists in approximately 1624. The settlement was named New Amsterdam (Dutch: Nieuw Amsterdam) in 1626 and was chartered as a city in 1653. The city came under English control in 1664 and was renamed New York after King Charles II granted the lands to his brother, the Duke of York. The city was temporarily regained by the Dutch in July 1673 and was renamed New Orange; however, the city has been named New York since November 1674. New York City was the capital of the United States from 1785 until 1790. The modern city was formed by the 1898 consolidation of its five boroughs: Manhattan, Brooklyn, Queens, The Bronx, and Staten Island, and has been the largest U.S. city ever since.

 

Anchored by Wall Street in the Financial District of Lower Manhattan, New York City has been called both the world's premier financial and fintech center and the most economically powerful city in the world. As of 2022, the New York metropolitan area is the largest metropolitan economy in the world with a gross metropolitan product of over US$2.16 trillion. If the New York metropolitan area were its own country, it would have the tenth-largest economy in the world. The city is home to the world's two largest stock exchanges by market capitalization of their listed companies: the New York Stock Exchange and Nasdaq. New York City is an established safe haven for global investors. As of 2023, New York City is the most expensive city in the world for expatriates to live. New York City is home to the highest number of billionaires, individuals of ultra-high net worth (greater than US$30 million), and millionaires of any city in the world

 

The written history of New York City began with the first European explorer, the Italian Giovanni da Verrazzano in 1524. European settlement began with the Dutch in 1608 and New Amsterdam was founded in 1624.

 

The "Sons of Liberty" campaigned against British authority in New York City, and the Stamp Act Congress of representatives from throughout the Thirteen Colonies met in the city in 1765 to organize resistance to Crown policies. The city's strategic location and status as a major seaport made it the prime target for British seizure in 1776. General George Washington lost a series of battles from which he narrowly escaped (with the notable exception of the Battle of Harlem Heights, his first victory of the war), and the British Army occupied New York and made it their base on the continent until late 1783, attracting Loyalist refugees.

 

The city served as the national capital under the Articles of Confederation from 1785 to 1789, and briefly served as the new nation's capital in 1789–90 under the United States Constitution. Under the new government, the city hosted the inauguration of George Washington as the first President of the United States, the drafting of the United States Bill of Rights, and the first Supreme Court of the United States. The opening of the Erie Canal gave excellent steamboat connections with upstate New York and the Great Lakes, along with coastal traffic to lower New England, making the city the preeminent port on the Atlantic Ocean. The arrival of rail connections to the north and west in the 1840s and 1850s strengthened its central role.

 

Beginning in the mid-19th century, waves of new immigrants arrived from Europe dramatically changing the composition of the city and serving as workers in the expanding industries. Modern New York traces its development to the consolidation of the five boroughs in 1898 and an economic and building boom following the Great Depression and World War II. Throughout its history, New York has served as a main port of entry for many immigrants, and its cultural and economic influence has made it one of the most important urban areas in the United States and the world. The economy in the 1700s was based on farming, local production, fur trading, and Atlantic jobs like shipbuilding. In the 1700s, New York was sometimes referred to as a breadbasket colony, because one of its major crops was wheat. New York colony also exported other goods included iron ore as a raw material and as manufactured goods such as tools, plows, nails and kitchen items such as kettles, pans and pots.

 

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+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

The McDonnell Douglas (now Boeing) T-45 Goshawk was a highly modified version of the BAe Hawk land-based training jet aircraft. Manufactured by McDonnell Douglas (now Boeing) and British Aerospace (now BAe Systems), the T-45 was used by the United States Navy and the United States Marine Corps (USMC) as an aircraft carrier-capable trainer.

The Goshawk's origins began in the mid-1970s, when the US Navy began looking for a single aircraft replacement for both its T-2 and TA-4 jet trainers. The US Navy started the VTXTS advanced trainer program in 1978. Several companies made submissions, e. g. North American or Northrop/Vought. Due to the size of the potential contract, European companies made submissions, too, including a navalized Alpha Jet from Dassault/Dornier and a fully carrier-capable version of the BAe Hawk Mk.60, mutually proposed by British Aerospace (BAe) and McDonnell Douglas (MDC). The latter eventually won the competition and BAe and MDC were awarded the T-45 contract in 1981.

 

The Hawk had not been designed for carrier operations and numerous modifications were required to make it suitable for use on carriers. These included improvements to the low-speed handling characteristics and a reduction in the approach speed. It was found that the aircraft was apt to stall at the low approach speed required. Modifications were designed by BAe in England; most notably a simple slat system was devised, operated by an actuator and linkage mechanism to fit into the small space available. Strakes were also added on the fuselage to improve airflow. Other changes were a strengthened airframe, a more robust and wider landing gear with a two-wheel nose landing gear, a catapult tow bar attachment and an arresting hook. The modified aircraft was christened “Goshawk”, flew in 1988 for the first time and became operational in 1991.

 

Beyond being a naval trainer the T-45 was also adapted for first-line duty with strike capabilities, in the form of the OA-45 for the USMC. The role of this aircraft dated back to the Vietnam War when twenty-three A-4 two-seaters were converted into OA-4Ms for “FastFAC” (Fast Forward Air Controller) missions, in order to control interdiction sorties dedicated to shaping the battlefield for future operations. Basically, the OA-4M was a TA-4F equipped with A-4M electronics. The most visible and characteristic change was the fitting of the A-4M’s dorsal electronics hump, neatly faired into the rear of the two-seat canopy. The nose sensor group of the OA-4M was basically the same as that of the A-4M, but the Angle/Rate Bombing system was not installed as it would not be needed.

 

When the T-45 was introduced in the early Nineties, the USMCs OA-4Ms had reached the end of their service life and the USMC started looking for a replacement, wanting a comparable, light and fast fixed-wing aircraft. The USMC did not accept the LTV A-7 as an A-4 replacement (even though a two-seater version was available), because it was already dated, too, and not part of the USMC inventory. The USMC's A-4Ms were supposed to be replaced by the VTOL AV-8 by the mid-nineties, but the AV-8, even as a two-seater, was deemed unsuitable for FFAC duties. The new T-45 looked like a good and economical alternative with future potential, since the airframe was brand new and the type's infrastructure was fully established, so that a small number of specialized aircraft could easily be supported without much extra cost.

 

With fresh experience from the 1st Gulf War in 1990-91 the decision was made to buy 25 extra T-45A airframes and convert them to OA-45A standard. Most important change were modified wings, using structures and systems from the BAe Hawk 100 series. While the T-45 only had two underwing and a single ventral hardpoint, the OA-45A featured a total of seven: four underwing and one ventral hardpoints, plus wingtip stations for defensive air-to-air missiles. Upgraded avionics allowed the deployment of a wide range of external stores, including air-to-ground missiles and rocket launchers, a reconnaissance pod, retarded and free-fall bombs of up to 1,000 pounds (450 kg) caliber, runway cratering, anti-personnel and light armor bombs, cluster bombs, practice bombs as well as external fuel tanks and ECM pods. This was a vital asset, since Desert Storm had proved that FFAC aircraft had to have an offensive capability to handle targets of opportunity on their own, when no air assets to control were available. A total ordnance load of up to 6,800 lb (3,085 kg) was possible, even though the aircraft was not supposed to play an offensive role and rather act from a distance, relying on its small size and agility.

 

Communication modifications for the FastFAC role included a KY-28 secure voice system, an ARC-159 radio and an ARC-114 VHF radio. Similar to the Skyhawk, a hump behind the cockpit had to be added to make room for the additional electronic equipment and a heat exchanger. Other additions were a continuous-wave Doppler navigation radar under a shallow ventral radome underneath the cockpit, a ground control bombing system, an APN-194 altimeter, an ALR-45 radar warning suite, a retrofitted, fixed midair refueling probe and cockpit armor plating that included Kevlar linings on the floor and the lower side walls as well as externally mounted armor plates for the upper areas.

 

VMA-131 of Marine Aircraft Group 49 (the Diamondbacks) retired its last four OA-4Ms on 22 June 1994, and the new OA-45A arrived just in time to replace the venerable Skyhawk two-seaters in the FastFAC role. Trainer versions of the Skyhawk remained in Navy service, however, finding a new lease on life with the advent of "adversary training". OA-45A deliveries were finished in 1996 and the 25 aircraft were distributed among the newly established Marine Aviation Logistics Squadron (MALS, formerly Headquarters & Maintenance Squadron/H&MS) 12 & 13. The USMC crews soon nicknamed their new mounts "GosHog", to underlöine ist offensive capabilities and to set themselves apart from the USN's "tame" trainers. Even though thos name was never officially approved it caught on quickly.

 

After initial experience with the new aircraft and in the wake of technological advances, the USMC decided to upgrade the OA-45As in 2000 to improve its effectiveness and interaction capabilities with ground troops. This primarily resulted in the addition of a forward-looking infrared camera laser in the aircraft’s nose section, which enabled the aircraft to execute all-weather/night reconnaissance and to illuminate targets for laser-guided infantry shells or ordnance launched by the OA-45 itself or by other aircraft. Through this measure the OA-45 became capable of carrying and independently deploying light laser-guided smart weapons like the GBU-12 and -16 “Paveway II” glide bombs or the laser-guided AGM-65E “Maverick” variant. The update was gradually executed during regular overhauls in the course of 2001 and 2002 (no new airframes were built/converted), the modified machines received the new designation OA-45B.

 

After this update phase, the OA-45Bs were deployed in several global conflicts and saw frequent use in the following years. For instance, MALS 13 used its OA-45Bs operationally for the first time in October 2002 when the squadron was tasked with providing support to six AV-8B Harrier aircraft in combat operations in Afghanistan during Operation Enduring Freedom. This mission lasted until October 2003, four aircraft were allocated and one OA-45B was lost during a landing accident.

On 15 January 2003, MALS 13 embarked 205 Marines and equipment aboard the USS Bonhomme Richard in support of combat operations in Southwest Asia during Operation Southern Watch. Four OA-45Bs successfully supported these troops from land bases, marking targets and flying reconnaissance missions.

Furthermore, six MALS 13 OA-45Bs took actively part in Operation Iraqi Freedom from Al Jaber Air Base, Kuwait, and An Numiniyah Expeditionary Air Field, Iraq, where the aircraft worked closely together with the advancing ground troops of the USMC’s 15th Marine Expeditionary Unit. They successfully illuminated targets for US Navy fighter bombers, which were launched from USS Abraham Lincoln (CVN-72) in the Persian Gulf, and effectively guided these aircraft to their targets. Two OA-45Bs were lost during this conflict, one through enemy MANPADS, the other through friendly AA fire. In late May 2003 the surviving machines and their crews returned to MCAS Yuma.

 

On 16 March 2007, the 200th T-45 airframe was delivered to the US Navy. From this final batch, six airframes were set aside and modified into OA-45Bs in order to fill the losses over the past years.

Later T-45 production aircraft were built with enhanced avionics systems for a heads-up display (HUD) and glass cockpit standard, while all extant T-45A aircraft were eventually converted to a T-45C configuration under the T-45 Required Avionics Modernization Program (T-45 RAMP), bringing all aircraft to same HUD plus glass cockpit standard. These updates, esp. concerning the cockpit, were introduced to the OA-45Bs, too, and they were re-designated again, now becoming OA-45Cs, to reflect the commonality with the Navy’s Goshawk trainers. Again, these modifications were gradually introduced in the course of the OA-45s’ normal maintenance program.

 

In 2007, an engine update of the whole T-45 fleet, including the OA-45s, with the Adour F405-RR-402 was considered. This new engine was based on the British Adour Mk 951, designed for the latest versions of the BAe Hawk and powering the BAe Taranis and Dassault nEUROn UCAV technology demonstrators. The Adour Mk 951 offered 6,500 lbf (29 kN) thrust and up to twice the service life of the F405-RR-401. It featured an all-new fan and combustor, revised HP and LP turbines, and introduced Full Authority Digital Engine Control (FADEC). The Mk 951 was certified in 2005, the F405-RR-402 derived from it was certified in 2008, but it did not enter service due to funding issues, so that this upgrade was not carried out.

 

The final delivery of the 246th T-45 airframe took place in November 2009, and both T-45 and the OA-45 "GosHog" are supposed to remain in service until 2035.

  

General characteristics:

Crew: 2 (pilot, observer)

Length: 39 ft 4 in (11.99 m)

Wingspan: 30 ft 10 in (9.39 m)

Height: 13 ft 5 in (4.08 m)

Wing area: 190.1 ft² (17.7 m²)

Empty weight: 10,403 lb (4,460 kg)

Max. takeoff weight: 14,081 lb (6,387 kg)

 

Powerplant:

1× Rolls-Royce Turbomeca F405-RR-401 (Adour) non-afterburning turbofan with 5,527 lbf (26 kN)

 

Performance:

Maximum speed: Mach 2 (2,204 km/h (1,190 kn; 1,370 mph) at high altitude

Combat radius: 800 km (497 mi, 432 nmi)

Ferry range: 3,200 km (1,983 mi) with drop tanks

Service ceiling: 15,240 m (50,000 ft)

Wing loading: 283 kg/m² (58 lb/ft²)

Thrust/weight: 0.97

Maximum g-load: +9 g

 

Armament:

No internal gun; seven external hardpoints (three on each wing and one under fuselage)

for a wide range of ordnance of up to 6,800 lb (3,085 kg), including up to six AIM-9 Sidewinder for

self-defense, pods with unguided rockets for target marking or ECM pods, but also offensive weapons

of up to 1.000 lb (454 kg) weight, including iron/cluster bombs and guided AGM-65, GBU-12 and -16.

  

The kit and its assembly:

This fictional T-45 variant is actually the result of a long idea evolution, and simply rooted in the idea of a dedicated OA-4M replacement for the USMC; in real life, the FFAC role has been transferred to F-18 two-seaters, though, but the T-45 appeared like a sound alternative to me.

 

There's only one T-45 kit available, a dubious T-45A from Italeri with poor wings and stabilizers. Wolfpack also offers a T-45, but it’s just a re-boxing of the Italeri kit with some PE parts and a price tag twice as big – but it does not mend the original kit’s issues… After reading the A-4 Skyhawk book from the French "Planes & Pilots" series, I was reminded of the USMC's special OA-4M FAC two-seaters (and the fact that it is available in kit form from Italeri and Hasegawa), and, cross-checking the real-world timeline of the T-45, I found that it could have been a suitable successor. The ide of the USMC’s OA-45 was born! :D

 

Building-wise the Italeri T-45 remained close to OOB, even though I transplanted several parts from an Italeri BAe Hawk Mk. 100 to create a different look. I modified the nose with the Mk. 100’s laser fairing and added some radar warning sensor bumps. This transplantation was not as easy as it might seem because the T-45’s nose is, due to the different and more massive front landing gear quite different from the Hawk’s. Took some major PSR to integrate the laser nose.

An ALR-45 “hot dog” fairing from a late A-4M (Italeri kit) was added to the fin, together with a small styrene wedge extending the fin’s leading edge. This small detail markedly changes the aircraft’s look. I furthermore added a refueling probe, scratched from coated wire and some white glue, as well as a low “camel back” fairing behind the cockpit, created from a streamlined bomb half with air outlets for an integrated heat exchanger. Blade antennae were relocated and added. A shallow bump for the Doppler radar was added under the fuselage behind the landing gear well – left over from an Airfix A-4B (from an Argentinian A-4P, to be correct, actually a dorsal fairing).

 

On the wings, a tailored pair of pylons and wing tip launch rails from the Italeri BAe Hawk Mk. 100 kit were added, too, as well as the donor kit’s pair of Sidewinders. The rest of the ordnance consists of drop tanks and LAU-19 pods for target marking missiles. The tanks were taken from the Hawk Mk. 100 kit, too, the rocket launchers came from an Italeri NATO aircraft weapons set. The centerline position carries an ALQ-131 ECM pod from a Hasegawa US aircraft weapons set on a pylon from the scrap box.

  

Painting and markings:

The low-viz idea prevailed, since I had some leftover OA-4M decals from Italeri kits in store, as well as some other suitable low-viz decals from a Revell A-4F kit. However, an all-grey livery was IMHO not enough, and when I came across a picture of a USN low-viz A-7E with an improvised desert camouflage in sand and reddish brown applied over the grey (even partly extending over its markings) from Operation Iraqi Freedom, I had that extra twist that would set the OA-45 apart. MALS-13 was chosen as operator because I had matching codes, and, as another benefit, the unit had actually been deployed overseas during the 2003 Iraq War, so that the whif’’s time frame was easily settled, adding to its credibility.

 

The livery was built up just like on the real aircraft: on top of a basic scheme in FS 36320 and 36375 (Humbrol 128 and 127) with a slightly darker anti-glare panel in front of the cockpit (FS 35237, I used Revell 57 as a slightly paler alternative) I applied the low-viz marking decals, which were protected with a coat of acrylic varnish. Next, additional desert camouflage was added with dry-brushed sand and millitary brown (supposedly FS 33711 and 30400 in real life, I used, after consulting pictures of aircraft from both Gulf Wars, Humbrol 103 (Cream) and 234 (Dark Flesh). They were applied with a kind of a dry-brushing technique, for a streaky and worn look, leaving out the codes and other markings. The pattern itself was inspired by an USMC OV-10 Bronco in desert camouflage from the 1st Gulf War.

On top of that a black ink washing was applied. Once things had thoroughly dried over night, I wet-sanded the additional desert camouflage away, carefully from front to back, so that the edges became blurred and the underlying grey became visible again.

 

The cockpit interior was painted in standard Dark Gull Grey (Humbrol 140), while the air intakes and the landing gear became white, the latter with red trim on the covers’ edges – just standard. Finally, the model was sealed with a coat of matt acrylic varnish (Italeri).

  

The upgraded T-45 is an interesting result. The add-ons suit the aircraft, which already looks sturdier than its land-based ancestor, well. The improvised desert paint scheme with the additional two-tone camouflage over the pale grey base really makes the aircraft an unusual sight, adding to its credibility.

Hardware-wise I am really happy how the added dorsal hump blends into the overall lines – in a profile view it extends the canopy’s curve and blends into the fin, much like the A-4F/M’s arrangement. And the modified fin yields a very different look, even though not much was changed. The T-45 looks much beefier now, and from certain angles really reminds of the OA-4M and sometimes even of a diminutive Su-25?

The iPhone is now capable of shooting RAW using iOS 10 and Adobe Lightroom mobile.

 

The results are astounding. This is an edited RAW file from the iPhone and you can see the detail that can be brought out of the highlights.

 

Watch the tutorial on my YouTube channel - www.firstmanphotography.com/tutorials/shoot-raw-files-on-...

The opening of the Connaught Bridge Generating Station, on the Klang River in Selangor, in March 1953 was a real milestone int he history of what was then Malaya - now Malaysia. The power station, capable of being either coal or oil fired, was at 80,000kw by far the largest generating station at the time in the country and, as importantly, the project included elements of a new proposed Malayan 'National Grid' that linked existing stations such as the hydro-electric plant at Chenderoh with stations and locations along the East Coast centred on the Bungsar station in Kuala Lumpur that hitherto had supplied the bulk of the capital's power requirements. As the booklet notes it meant an end to the long post-war years of restriction of supply to both industrial and domestic consumers.

 

The station was originally planned in 1944 by the Malayan Planning Unit in London in anticipation of the return to Malaya after the end of the Japanses occupation. A provisional order for the equipment was placed in 1945, with additional equipment following in 1947. Meanwhile the site at Connaught Bridge alongside the Klang River was selected in 1946 with the contract to start construction given by the Federation's Government in 1949. The first phase of the station, plant and the double circuit 66kv interconnecting lines running the 23 miles to Kuala Lumpur, was ready for opening in March 1953. Full commissioning came in 1955. Initailly the output was linked to the Bangsar (KL) station and that of Ulu Langat hydro-electric station. Construction of the former had started in 1926 and was opened in 1927 by the Government electricity department and in 1933 they purchased the Ulu Langat station from the Sungei Besi Mines Ltd. KL's earlier supplies, from 1905, had been provided from a small hydro-electric plant on the Gombak River, 12 miles from the town, what had two 400kw Pelton wheel-alternators. This had been augmented in 1919 by a mixed steam and diesel engine plant at Gombak Lane in the centre of KL.

 

Elsewhere, Penang's Municipal Department was the first to supply electriicty within Malaya when it started in 1904 - the station on the mainland at Prai came into use in 1926. By this date electricity was available in Ipoh, Johore Bahru (and Singapore), Seremban and Malacca/Melaka. That at Johore Bahru under the Johore adminsitraion grew to include Muar, Batu Pahat, Kluang, Kota Tinggi and Segamat. In Perak supplies were largely in the hands of the Perak River Hydro-Electric Power Company who operated stations at Malim Nawar (1928) and Chenderoh (1929). In North Perak the Government supplied Taiping and in Province Wellesley Messrs. Huttenbach's bought bulk supply from Penang and supplied power to various towns, supplemented by diesel generating stations in Kedah, Perak and Negri Sembilan. Power came to Kota Bharu (Kelantan), Ruab, Bentong, Kuala Lipis and Kuantan between 1928 and 1931, and in 1938 and 1939 to Mentakab, Fraser's Hill and Kuala Kubu.

 

In 1946 the Malayan Union Government acquired most electricity undertakings except those of private companies and Penang Corporation whilst it also fully acquired the undertkaing operated by the Malacca Electric Light Company in 1948 that it has previously run on a rental basis. On the 1 September 1949 the new Central Electricity Board of the Federation fo Malaya came into existance and took over all functions of the old Electricity Department.

 

The booklet is marvellously detailed and illustrated describing the site, the power station, ancilliary equipment and other works, such as staff accomodaton and housing, with photographs and plans. The latter include a map of the proposed Malayan Grid and the plans show the works designed by both the staff of the Central Electricity Board and the consulting engineers, Preece, Cardew and Rider, and civil engineers Coode and Partners. The station took cooling water from the Klang River and could be powered by either fuel oil (via a pipeline from Port Swettenham) and coal via connections with the Malayan Railways and the colliery at Batu Arang.

 

Needless to say much of the equipment was supplied from the UK - Parsons generators and transformers and switchgear from various manufacturers including British Thomson Houston.

 

The photos are great as they show named members of the operating staff at work which is unusual but that now provided a real social history to the economic history of electricity supply in Malaysia.

Capable of long jumps and sufficient sand walking capabilities, this melee orientated hardsuit is a tough friend or foe in desert battlegrounds

Some background:

The VF-1 was developed by Stonewell/Bellcom/Shinnakasu for the U.N. Spacy by using alien Overtechnology obtained from the SDF-1 Macross alien spaceship. Its production was preceded by an aerodynamic proving version of its airframe, the VF-X. Unlike all later VF vehicles, the VF-X (sometimes referred to as VF-X1) was strictly a conventional/non-transformable jet aircraft, even though it incorporated many structural components and several key technologies that were vital for the transformable VF-1’s successful development that ran in parallel. Therefore, the VF-X was never intended as an air superiority fighter, but rather a flight-capable analogue test bed and proof of concept for the VF-1’s basic layout and major components. In this role, however, the VF-X made vital contributions to systems’ development that were later incorporated into the VF-1’s serial production and sped the program up considerably.

 

VF-X production started in early 2006, with four airframes built. The flight tests began in February 2007. The first prototype (“01”) was piloted and evaluated by ace pilot Roy Fokker, in order to explore the aircraft’s flight envelope, general handling and for external stores carriage tests. The three other VF-Xs successively joined the test program, each with a different focus. “02” was primarily tasked with the flight control and pilot interface program, “03” was allocated to the engine, vectoring thrust and steering systems development, and “04” was primarily involved in structural and fatigue tests.

 

In November 2007, the successful VF-X tests and the flights of the VF-X-1 (the first fully transformable VF-1 prototype, which had been under construction in parallel to the VF-X program) led to formal adoption of the “Valkyrie” variable fighter by the United Nations Government.

The space-capable VF-1's combat debut was on February 7, 2009, during the Battle of South Ataria Island - the first battle of Space War I - and remained the mainstay fighter of the U.N. Spacy for the entire conflict.

 

Introduced in 2008, the VF-1 proved to be an extremely capable craft, successfully combating a variety of Zentraedi mecha, even in most sorties which saw UN Spacy forces significantly outnumbered. The versatility of the Valkyrie design enabled the variable fighter to act as both large-scale infantry and as air/space superiority fighter. The signature skills of U.N. Spacy ace pilot Maximilian Jenius exemplified the effectiveness of the variable systems as he near-constantly transformed the Valkyrie in battle to seize advantages of each mode as combat conditions changed from moment to moment.

 

The basic VF-1 was deployed in four sub-variants (designated A, D, J, and S) and its success was increased by continued development of various enhancements. These included the GBP-1S "Armored Valkyrie” external armor and infantry weapons pack, so-called FAST Packs for "Super Valkyries” for orbital use, and the additional RÖ-X2 heavy cannon pack weapon system for the VF-1S “Strike Valkyrie” with additional firepower.

 

After the end of Space War I, the VF-1 continued to be manufactured both in the Sol system and throughout the UNG space colonies. Although the VF-1 would eventually be replaced as the primary Variable Fighter of the U.N. Spacy by the more capable, but also much bigger, VF-4 Lightning III in 2020, a long service record and continued production after the war proved the lasting worth of the design.

 

The VF-1 was without doubt the most recognizable variable fighter of Space War I and was seen as a vibrant symbol of the U.N. Spacy even into the first year of the New Era 0001 in 2013. At the end of 2015 the final rollout of the VF-1 was celebrated at a special ceremony, commemorating this most famous of variable fighters. The VF-1 Valkryie was built from 2006 to 2013 with a total production of 5,459 VF-1 variable fighters with several variants (VF-1A = 5,093, VF-1D = 85, VF-1J = 49, VF-1S = 30, VF-1G = 12, VE-1 = 122, VT-1 = 68), and several upgrade programs were introduced.

The fighter remained active in many second line units and continued to show its worthiness years later, e. g. through Milia Jenius who would use her old VF-1 fighter in defense of the colonization fleet - 35 years after the type's service introduction.

  

General characteristics:

Accommodation: One pilot in a Marty & Beck Mk-7 zero/zero ejection seat

Length 14.23 meters

Wingspan 14.78 meters (at 20° minimum sweep)

Height 3.84 meters

Empty weight: 13.25 metric tons

Standard T-O mass: 18.5 metric tons

 

Power Plant:

2x Shinnakasu Heavy Industry/P&W/Roice FF-2001 thermonuclear reaction turbine engines, output 650 MW each, rated at 11,500 kg in standard or in overboost (225.63 kN x 2)

4 x Shinnakasu Heavy Industry NBS-1 high-thrust vernier thrusters (1 x counter reverse vernier thruster nozzle mounted on the side of each leg nacelle/air intake, 1 x wing thruster roll control system on each wingtip);

 

Performance:

Top speed: Mach 2.71 at 10,000 m; Mach 3.87 at 30,000+ m

Thrust-to-weight ratio: empty 3.47; standard T-O 2.49; maximum T-O 1.24

 

Armament:

None installed, but the VF-X had 4x underwing hard points for a wide variety of ordnance, plus a ventral hardpoint for a Howard GU-11 55 mm three-barrel Gatling gun pod with 200 RPG, fired at 1,200 rds/min or other stores like test instruments

  

The model and its assembly:

Another submission to the “Prototypes” group build at whatifmodelers.com in July 2020. Being a VF-1 fan (and have built maybe twenty o these simple Arii kits), adding a VF-X was, more or less, a must – even more so because I had a suitable Valkyrie Fighter kit at hand for the conversion. As a side note, I have actually built something quite similar from a VF-1D many years ago: a fictional, non-transformable advanced trainer, without knowing about the VF-X at all.

 

Thanks to the “Macross - Perfect Memory” source book, the differences between the transformable VF-1 and its early testbed were easy to identify:

- Fixed legs with faired ducts from the intakes on (thighs)

- Ankle recesses disappeared

- Less and slightly different panel lines on the back and on the nose

- ventral head unit deleted and a respective fairing installed instead

- Levelled underside (shoulder fairings of the folded arms were cut down)

- Leg attachment points on the nose deleted

- No small, circular vernier thrusters all around the hull

- Some new/different venting grills (created mostly with 0.5mm black decal stripes)

 

Beyond the changes, the VF-1A was basically built OOB. Thankfully, the VF-X already features the later VF-1’s vectored thrust nozzles/feet, so that no changes had to be made in this respect. A pilot figure was added to the cockpit for the beauty pics, and after the flight scenes had been shot, the canopy remained open on a swing arm for static display. For the same reason, the model was built with the landing gear extended.

 

As a test aircraft, the underwing pylons and their AMM-1 ordnance were left away and the attachment points hidden with putty. I also omitted the ventral gun pod and left the aircraft clean. However, for the flight scene pictures, I implanted an adapter for a display holder made from wire.

 

In order to emphasize the test vehicle character of the VF-X, I gave the model a scratched spin recovery parachute installation between the fins, using a real world F-22 testbed as benchmark. It consists of styrene profiles, quite a delicate construction. For the same reason I gave the VF-X a long sensor boom on the nose, which changes the Valkyrie’s look, too. Finally, some small blade antennae were added to the nose and to the spine behind the cockpit.

  

Painting and markings:

To be honest, I have no idea if there was only a single VF-X prototype in the Macross universe, or more. Just one appears in the TV series in episode #33, and lack of suitable information and my personal lack of Japanese language proficiency prevents any deeper research. However, this would not keep me from inventing a personal interpretation of the canonical VF-X, especially because I do not really like the original livery from the TV series: an overall light grey with some simple black trim and “TEST” written on the (fixed) legs. Yamato did an 1:60 scale toy of the VF-X, but it was/is just a VF-1 with a ventral fairing; they added some shading to the basic grey – but this does not make the aircraft more attractive, IMHO.

 

When I looked at the original conceptual drawing of the VF-X in the “Macross - Perfect Memory” source book, however, I was immediately reminded of the F-15 prototypes from the Seventies (and this program used a total of twelve machines!). These featured originally a light grey (FS 36375?) overall base, to which bright dayglo orange markings on wings, fins and fuselage were soon added – in a very similar pattern to the VF-X. I think the VF-X livery was actually inspired by this, the time frame matches well with the production of the Macross TV series, too, and that’s what I adapted for my model.

In order to come close to the F-15 prototype livery, I gave “my” VF-X an overall basic coat of RAL 7047 “Telegrau 4”, one of German Telekom’s corporate colors and a very pale grey that can easily be mistaken for white when you do not have a contrast reference.

 

The cockpit received a medium grey finish, the ejection seat became black with brown cushions; the pilot figure is a 1:100 seated passenger from an architecture supplies, painted like an early VF-1 pilot in a white/blue suit. The jet nozzles/feet were painted with Revell 91 (Iron) and later treated with grinded graphite for a more metallic finish. The landing gear became classic white (I used Revell 301, which is a very pure tone, as contrast to the RAL 7047 on the hull), the air intake ducts and the internal sections of the VG wings were painted with dark grey (Revell 77).

 

For some diversity I took inspiration from the Yamato VF-X toy and added slightly darker (Humbrol 166, RAF Light Aircraft Grey) areas to the hull and the legs. Next, the panel lines were emphasized through a thinned black ink wash, but I did no panel post shading so that the VF-X would not look too dirty or worn.

 

Onto this basis I applied the orange dayglo markings. On the wings and fins, these were painted – they were applied with spray paint from a rattle can, involving lots of masking. The leading edges on wings and fins were created with grey decal sheet material, too. At this stage, some surface details and more fake panel lines were added with a soft pencil.

The orange cheatline under the cockpit is a personal addition; I found that some more orange had to be added to the nose for visual balance, and I eventually went for the simple, trimmed stripe (TL Modellbau material) instead of trying to apply decal sheet material around the jagged air intakes (F-15 prototype style). The black “TEST”, “VFX” and “U.N. Spacy” markings were designed at the computer and printed on clear inkjet decal paper. Even though the “real” VF-X does not feature the UNS “kite” insignia, I decided to add them to the model. These come from the OOB sheet, which also provided most (slightly yellowed) stencils.

Finally, the model was sealed with a coat of matt acrylic varnish (Italeri).

  

A rather different VF-1 project (and it is – to my astonishment – #28 in my 1:100 VF-1 Fighter mode collection!!!), with more changes to the basic model kit than one might expect at first sight. VF-X and VF-1 differ considerably from each other, despite identical outlines! However, I like the outcome, and I think that going a different route from the canonical grey/black livery paid out, the bright orange markings really make this VF-X stand out, and it looks IMHO more like a testbed than the “real” aircraft from the TV series.

Medical Staff practise casualty treatment during Exercise Capable Eagle at RAF Leeming.

 

Royal Air Force medics have been responding after a simulated air attack on a North Yorkshire airfield.

 

RAF Leeming was playing the part of a foreign airbase being used by UK and French forces, as part of Exercise Capable Eagle, a test of the two countries’ ability to mount a combined air operation.

 

The exercise saw personnel planning, preparing for and flying missions, while facing a series of challenges.

 

One of those was an ‘attack’ by aircraft from 100 Squadron – itself normally based at RAF Leeming. 100 Squadron’s main role is to support training for all three services, including acting as an enemy when required. The simulated attack left a number of simulated casualties, giving the RAF’s healthcare experts a chance to test their skills.

 

While their colleagues are operating in Afghanistan daily, there is still a need for military medics to prepare for other possible operations. And Exercise Capable Eagle has given them the opportunity to do that.

-------------------------------------------------------

© Crown Copyright 2013

Photographer: Cpl Andy Holmes

Image 45156306.jpg from www.defenceimages.mod.uk

  

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Man is capable of such amazing pieces of engineering. It boggles the mind that since 1937 with thousands of heavy machinery driving by it every day, earthquakes, strong winds and the fog, this beauty is still going strong. Ventured early morning with a friend (pictured) to find this spot.

Some background:

The VF-1 was developed by Stonewell/Bellcom/Shinnakasu for the U.N. Spacy by using alien Overtechnology obtained from the SDF-1 Macross alien spaceship. Its production was preceded by an aerodynamic proving version of its airframe, the VF-X. Unlike all later VF vehicles, the VF-X (sometimes referred to as VF-X1) was strictly a conventional/non-transformable jet aircraft, even though it incorporated many structural components and several key technologies that were vital for the transformable VF-1’s successful development that ran in parallel. Therefore, the VF-X was never intended as an air superiority fighter, but rather a flight-capable analogue test bed and proof of concept for the VF-1’s basic layout and major components. In this role, however, the VF-X made vital contributions to systems’ development that were later incorporated into the VF-1’s serial production and sped the program up considerably.

 

VF-X production started in early 2006, with four airframes built. The flight tests began in February 2007. The first prototype (“01”) was piloted and evaluated by ace pilot Roy Fokker, in order to explore the aircraft’s flight envelope, general handling and for external stores carriage tests. The three other VF-Xs successively joined the test program, each with a different focus. “02” was primarily tasked with the flight control and pilot interface program, “03” was allocated to the engine, vectoring thrust and steering systems development, and “04” was primarily involved in structural and fatigue tests.

 

In November 2007, the successful VF-X tests and the flights of the VF-X-1 (the first fully transformable VF-1 prototype, which had been under construction in parallel to the VF-X program) led to formal adoption of the “Valkyrie” variable fighter by the United Nations Government.

The space-capable VF-1's combat debut was on February 7, 2009, during the Battle of South Ataria Island - the first battle of Space War I - and remained the mainstay fighter of the U.N. Spacy for the entire conflict.

 

Introduced in 2008, the VF-1 proved to be an extremely capable craft, successfully combating a variety of Zentraedi mecha, even in most sorties which saw UN Spacy forces significantly outnumbered. The versatility of the Valkyrie design enabled the variable fighter to act as both large-scale infantry and as air/space superiority fighter. The signature skills of U.N. Spacy ace pilot Maximilian Jenius exemplified the effectiveness of the variable systems as he near-constantly transformed the Valkyrie in battle to seize advantages of each mode as combat conditions changed from moment to moment.

 

The basic VF-1 was deployed in four sub-variants (designated A, D, J, and S) and its success was increased by continued development of various enhancements. These included the GBP-1S "Armored Valkyrie” external armor and infantry weapons pack, so-called FAST Packs for "Super Valkyries” for orbital use, and the additional RÖ-X2 heavy cannon pack weapon system for the VF-1S “Strike Valkyrie” with additional firepower.

 

After the end of Space War I, the VF-1 continued to be manufactured both in the Sol system and throughout the UNG space colonies. Although the VF-1 would eventually be replaced as the primary Variable Fighter of the U.N. Spacy by the more capable, but also much bigger, VF-4 Lightning III in 2020, a long service record and continued production after the war proved the lasting worth of the design.

 

The VF-1 was without doubt the most recognizable variable fighter of Space War I and was seen as a vibrant symbol of the U.N. Spacy even into the first year of the New Era 0001 in 2013. At the end of 2015 the final rollout of the VF-1 was celebrated at a special ceremony, commemorating this most famous of variable fighters. The VF-1 Valkryie was built from 2006 to 2013 with a total production of 5,459 VF-1 variable fighters with several variants (VF-1A = 5,093, VF-1D = 85, VF-1J = 49, VF-1S = 30, VF-1G = 12, VE-1 = 122, VT-1 = 68), and several upgrade programs were introduced.

The fighter remained active in many second line units and continued to show its worthiness years later, e. g. through Milia Jenius who would use her old VF-1 fighter in defense of the colonization fleet - 35 years after the type's service introduction.

  

General characteristics:

Accommodation: One pilot in a Marty & Beck Mk-7 zero/zero ejection seat

Length 14.23 meters

Wingspan 14.78 meters (at 20° minimum sweep)

Height 3.84 meters

Empty weight: 13.25 metric tons

Standard T-O mass: 18.5 metric tons

 

Power Plant:

2x Shinnakasu Heavy Industry/P&W/Roice FF-2001 thermonuclear reaction turbine engines, output 650 MW each, rated at 11,500 kg in standard or in overboost (225.63 kN x 2)

4 x Shinnakasu Heavy Industry NBS-1 high-thrust vernier thrusters (1 x counter reverse vernier thruster nozzle mounted on the side of each leg nacelle/air intake, 1 x wing thruster roll control system on each wingtip);

 

Performance:

Top speed: Mach 2.71 at 10,000 m; Mach 3.87 at 30,000+ m

Thrust-to-weight ratio: empty 3.47; standard T-O 2.49; maximum T-O 1.24

 

Armament:

None installed, but the VF-X had 4x underwing hard points for a wide variety of ordnance, plus a ventral hardpoint for a Howard GU-11 55 mm three-barrel Gatling gun pod with 200 RPG, fired at 1,200 rds/min or other stores like test instruments

  

The model and its assembly:

Another submission to the “Prototypes” group build at whatifmodelers.com in July 2020. Being a VF-1 fan (and have built maybe twenty o these simple Arii kits), adding a VF-X was, more or less, a must – even more so because I had a suitable Valkyrie Fighter kit at hand for the conversion. As a side note, I have actually built something quite similar from a VF-1D many years ago: a fictional, non-transformable advanced trainer, without knowing about the VF-X at all.

 

Thanks to the “Macross - Perfect Memory” source book, the differences between the transformable VF-1 and its early testbed were easy to identify:

- Fixed legs with faired ducts from the intakes on (thighs)

- Ankle recesses disappeared

- Less and slightly different panel lines on the back and on the nose

- ventral head unit deleted and a respective fairing installed instead

- Levelled underside (shoulder fairings of the folded arms were cut down)

- Leg attachment points on the nose deleted

- No small, circular vernier thrusters all around the hull

- Some new/different venting grills (created mostly with 0.5mm black decal stripes)

 

Beyond the changes, the VF-1A was basically built OOB. Thankfully, the VF-X already features the later VF-1’s vectored thrust nozzles/feet, so that no changes had to be made in this respect. A pilot figure was added to the cockpit for the beauty pics, and after the flight scenes had been shot, the canopy remained open on a swing arm for static display. For the same reason, the model was built with the landing gear extended.

 

As a test aircraft, the underwing pylons and their AMM-1 ordnance were left away and the attachment points hidden with putty. I also omitted the ventral gun pod and left the aircraft clean. However, for the flight scene pictures, I implanted an adapter for a display holder made from wire.

 

In order to emphasize the test vehicle character of the VF-X, I gave the model a scratched spin recovery parachute installation between the fins, using a real world F-22 testbed as benchmark. It consists of styrene profiles, quite a delicate construction. For the same reason I gave the VF-X a long sensor boom on the nose, which changes the Valkyrie’s look, too. Finally, some small blade antennae were added to the nose and to the spine behind the cockpit.

  

Painting and markings:

To be honest, I have no idea if there was only a single VF-X prototype in the Macross universe, or more. Just one appears in the TV series in episode #33, and lack of suitable information and my personal lack of Japanese language proficiency prevents any deeper research. However, this would not keep me from inventing a personal interpretation of the canonical VF-X, especially because I do not really like the original livery from the TV series: an overall light grey with some simple black trim and “TEST” written on the (fixed) legs. Yamato did an 1:60 scale toy of the VF-X, but it was/is just a VF-1 with a ventral fairing; they added some shading to the basic grey – but this does not make the aircraft more attractive, IMHO.

 

When I looked at the original conceptual drawing of the VF-X in the “Macross - Perfect Memory” source book, however, I was immediately reminded of the F-15 prototypes from the Seventies (and this program used a total of twelve machines!). These featured originally a light grey (FS 36375?) overall base, to which bright dayglo orange markings on wings, fins and fuselage were soon added – in a very similar pattern to the VF-X. I think the VF-X livery was actually inspired by this, the time frame matches well with the production of the Macross TV series, too, and that’s what I adapted for my model.

In order to come close to the F-15 prototype livery, I gave “my” VF-X an overall basic coat of RAL 7047 “Telegrau 4”, one of German Telekom’s corporate colors and a very pale grey that can easily be mistaken for white when you do not have a contrast reference.

 

The cockpit received a medium grey finish, the ejection seat became black with brown cushions; the pilot figure is a 1:100 seated passenger from an architecture supplies, painted like an early VF-1 pilot in a white/blue suit. The jet nozzles/feet were painted with Revell 91 (Iron) and later treated with grinded graphite for a more metallic finish. The landing gear became classic white (I used Revell 301, which is a very pure tone, as contrast to the RAL 7047 on the hull), the air intake ducts and the internal sections of the VG wings were painted with dark grey (Revell 77).

 

For some diversity I took inspiration from the Yamato VF-X toy and added slightly darker (Humbrol 166, RAF Light Aircraft Grey) areas to the hull and the legs. Next, the panel lines were emphasized through a thinned black ink wash, but I did no panel post shading so that the VF-X would not look too dirty or worn.

 

Onto this basis I applied the orange dayglo markings. On the wings and fins, these were painted – they were applied with spray paint from a rattle can, involving lots of masking. The leading edges on wings and fins were created with grey decal sheet material, too. At this stage, some surface details and more fake panel lines were added with a soft pencil.

The orange cheatline under the cockpit is a personal addition; I found that some more orange had to be added to the nose for visual balance, and I eventually went for the simple, trimmed stripe (TL Modellbau material) instead of trying to apply decal sheet material around the jagged air intakes (F-15 prototype style). The black “TEST”, “VFX” and “U.N. Spacy” markings were designed at the computer and printed on clear inkjet decal paper. Even though the “real” VF-X does not feature the UNS “kite” insignia, I decided to add them to the model. These come from the OOB sheet, which also provided most (slightly yellowed) stencils.

Finally, the model was sealed with a coat of matt acrylic varnish (Italeri).

  

A rather different VF-1 project (and it is – to my astonishment – #28 in my 1:100 VF-1 Fighter mode collection!!!), with more changes to the basic model kit than one might expect at first sight. VF-X and VF-1 differ considerably from each other, despite identical outlines! However, I like the outcome, and I think that going a different route from the canonical grey/black livery paid out, the bright orange markings really make this VF-X stand out, and it looks IMHO more like a testbed than the “real” aircraft from the TV series.

The silvereye or wax-eye (Zosterops lateralis) is a very small omnivorous passerine bird of the south-west pacific. Although one of Australia's smallest birds, the Silvereye is capable of travelling great distances during migration, with Silvereyes from the most southerly regions of Tasmania travelling all the way up to Southern Queensland. Truly an astonishing feat for birds weighing only around 10 grams.

 

In New Zealand, the silvereye was first recorded in 1832. It arrived in greater numbers in 1856, and it is assumed that a migrating flock was swept eastwards by a storm. As an apparently self-introduced bird it is protected as a native New Zealand species. Its Māori name, tauhou, means "stranger" or more literally, "new arrival".

 

DESCRIPTION

The Silvereye, - which belongs to a group of birds known as white-eyes -, is a small bird (11 to 13 cm in length) with a conspicuous ring of white feathers around the eye. The Silvereye shows interesting plumage variations depending on the sub-species (17 in total). To complicate this, the ranges of the sub-species overlap or may replace each other in their different areas for parts of the year because the birds in the east have regular seasonal migrations within Australia.

 

Generally it has olive-green wings and either a grey or olive-green back, a lighter coloured throat - yellow or grey, flanks that range from chestnut to pale buff, and an undertail that may be white or yellow. The grey back and olive-green head and wings are found in birds through the east, while western birds have a uniformly olive-green back. Breeding birds of the east coast have yellow throats, pale buff flanks (side of the belly) and white on the undertail. Tasmanian birds have grey throats, chestnut flanks and yellow on the undertail. Birds in Western Australia have yellowish olive, rather than grey, backs.

 

DISTRIBUTION AND HABITAT

The silvereye is native to Australia, New Zealand and the south-west Pacific islands of Lord Howe, New Caledonia, Loyalty Islands, Vanuatu, and Fiji. Silvereyes are more common in the relatively fertile south-west and south-east of Australia (including Tasmania and the Bass Strait islands), but their range extends from Cape York Peninsula, Queensland, through the south and south-west to about Shark Bay, Western Australia. In the south of their range, Silvereyes move north each autumn, and move back south in late winter to breed. Silvereyes may occur in almost any wooded habitat, including commercial orchards and urban parks and gardens.

 

Birds are seen alone, in pairs or small flocks during the breeding season, but form large flocks in the winter months. In late summer silvereyes gather into flocks and many Australian birds migrate, making their way north along the coast and ranges, foraging busily during the day with much calling and quick movement through the shrubbery, then flying long distances through the night.

 

FEEDING

The omnivorous Silvereyes feed on insect prey and large amounts of fruit and nectar, making them occasional pests of commercial orchards. When food is scarce in winter they will take a wide variety of foods from bird tables, ranging from sugar water through bread and cooked meats, to solid lumps of fat.

 

They perform a valuable service in gardens and orchards, eating insects harmful to produce, including aphids, scale insects, and the diamondback moth. However some orchardists, grape growers and home gardeners regard them as a serious pest particularly as, being so small, they simply ignore bird nets, popping in and out through the netting at will. They are attracted to a wide range of fruit species, including apples, citrus, feijoas, figs, grapes, pears and persimmons.

 

BREEDING

Silvereyes breed in spring and early summer, mainly between September and December. Silvereye pairs actively defend a small territory. The nest is a tiny, neatly woven cup of grasses, hair, and other fine vegetation, bound with spider web. It is placed in a horizontal tree fork in the outer reaches of small trees or shrubs up to 5m above the ground. The nest is constructed by both sexes, who both also incubate the two to four pale bluish-green eggs. If conditions are suitable two to three clutches will be raised during each breeding season. The juveniles are independent at 3 weeks and able to breed at 9 months.

Source: Wikipedia, birdsinbackyards.net

The 2000MW capable West Burton Power Station sits idle this afternoon, taking a break during a lull in UK Demand.

 

The station is equipped with x4 English Electric 500MW Turbo Generators which are horizontally placed within the turbine hall to which steam is provided from x4 International Combustion Boilers.

 

Four 17.5MW Rolls Royce Avon Gas Turbine Units are also held in reserve, giving the station black start capability.

 

Some background:

The VF-1 was developed by Stonewell/Bellcom/Shinnakasu for the U.N. Spacy by using alien Overtechnology obtained from the SDF-1 Macross alien spaceship. Its production was preceded by an aerodynamic proving version of its airframe, the VF-X. Unlike all later VF vehicles, the VF-X was strictly a jet aircraft, built to demonstrate that a jet fighter with the features necessary to convert to Battroid mode was aerodynamically feasible. After the VF-X's testing was finished, an advanced concept atmospheric-only prototype, the VF-0 Phoenix, was flight-tested from 2005 to 2007 and briefly served as an active-duty fighter from 2007 to the VF-1's rollout in late 2008, while the bugs were being worked out of the full-up VF-1 prototype (VF-X-1).

 

The space-capable VF-1's combat debut was on February 7, 2009, during the Battle of South Ataria Island - the first battle of Space War I - and remained the mainstay fighter of the U.N. Spacy for the entire conflict. Introduced in 2008, the VF-1 would be out of frontline service just five years later, though.

 

The VF-1 proved to be an extremely capable craft, successfully combating a variety of Zentraedi mecha even in most sorties which saw UN Spacy forces significantly outnumbered. The versatility of the Valkyrie design enabled the variable fighter to act as both large-scale infantry and as air/space superiority fighter. The signature skills of U.N. Spacy ace pilot Maximilian Jenius exemplified the effectiveness of the variable systems as he near-constantly transformed the Valkyrie in battle to seize advantages of each mode as combat conditions changed from moment to moment.

 

The basic VF-1 was deployed in four minor variants (designated A, D, J, and S) and its success was increased by continued development of various enhancements including the GBP-1S "Armored" Valkyrie, FAST Pack "Super" Valkyrie and the additional RÖ-X2 heavy cannon pack weapon system for the VF-1S for additional firepower.

The FAST Pack system was designed to enhance the VF-1 Valkyrie variable fighter, and the initial V1.0 came in the form of conformal pallets that could be attached to the fighter’s leg flanks for additional fuel – primarily for Long Range Interdiction tasks in atmospheric environment. Later FAST Packs were designed for space operations.

 

After the end of Space War I, the VF-1 continued to be manufactured both in the Sol system and throughout the UNG space colonies. Although the VF-1 would be replaced in 2020 as the primary Variable Fighter of the U.N. Spacy by the more capable, but also much bigger, VF-4 Lightning III, a long service record and continued production after the war proved the lasting worth of the design.

The versatile aircraft also underwent constant upgrade programs. For instance, about a third of all VF-1 Valkyries were upgraded with Infrared Search and Track (IRST) systems from 2016 onwards, placed in a streamlined fairing on the upper side of the nose, just in front of the cockpit. This system allowed for long-range search and track modes, freeing the pilot from the need to give away his position with active radar emissions, and it could also be used for target illumination and guiding precision weapons.

Many Valkyries also received improved radar warning systems, with receivers, depending on the systems, mounted on the wing-tips, on the fins and/or on the LERXs. Improved ECR measures were also mounted on some machines, typically in conformal fairings on the flanks of the legs/engine pods.

 

The VF-1 was without doubt the most recognizable variable fighter of Space War I and was seen as a vibrant symbol of the U.N. Spacy even into the first year of the New Era 0001 in 2013. At the end of 2015 the final rollout of the VF-1 was celebrated at a special ceremony, commemorating this most famous of variable fighters. The VF-1 Valkryie was built from 2006 to 2013 with a total production of 5,459 VF-1 variable fighters with several variants (VF-1A = 5,093, VF-1D = 85, VF-1J = 49, VF-1S = 30, VF-1G = 12, VE-1 = 122, VT-1 = 68)

 

However, the fighter remained active in many second line units and continued to show its worthiness years later, e. g. through Milia Jenius who would use her old VF-1 fighter in defense of the colonization fleet - 35 years after the type's service introduction!

 

General characteristics:

All-environment variable fighter and tactical combat Battroid,

used by U.N. Spacy, U.N. Navy, U.N. Space Air Force

 

Accommodation:

Pilot only in Marty & Beck Mk-7 zero/zero ejection seat

 

Dimensions:

Fighter Mode:

Length 14.23 meters

Wingspan 14.78 meters (at 20° minimum sweep)

Height 3.84 meters

 

Battroid Mode:

Height 12.68 meters

Width 7.3 meters

Length 4.0 meters

 

Empty weight: 13.25 metric tons;

Standard T-O mass: 18.5 metric tons;

MTOW: 37.0 metric tons

 

Power Plant:

2x Shinnakasu Heavy Industry/P&W/Roice FF-2001 thermonuclear reaction turbine engines, output 650 MW each, rated at 11,500 kg in standard or in overboost (225.63 kN x 2)

4x Shinnakasu Heavy Industry NBS-1 high-thrust vernier thrusters (1 x counter reverse vernier thruster nozzle mounted on the side of each leg nacelle/air intake, 1 x wing thruster roll control system on each wingtip);

18x P&W LHP04 low-thrust vernier thrusters beneath multipurpose hook/handles

 

Performance:

Battroid Mode: maximum walking speed 160 km/h

Fighter Mode: at 10,000 m Mach 2.71; at 30,000+ m Mach 3.87

g limit: in space +7

Thrust-to-weight ratio: empty 3.47; standard T-O 2.49; maximum T-O 1.24

 

Design Features:

3-mode variable transformation; variable geometry wing; vertical take-off and landing; control-configurable vehicle; single-axis thrust vectoring; three "magic hand" manipulators for maintenance use; retractable canopy shield for Battroid mode and atmospheric reentry; option of GBP-1S system, atmospheric-escape booster, or FAST Pack system

 

Transformation:

Standard time from Fighter to Battroid (automated): under 5 sec.

Min. time from Fighter to Battroid (manual): 0.9 sec.

 

Armament:

2x internal Mauler RÖV-20 anti-aircraft laser cannon, firing 6,000 pulses per minute

1x Howard GU-11 55 mm three-barrel Gatling gun pod with 200 RPG, fired at 1,200 rds/min

4x underwing hard points for a wide variety of ordnance, including

12x AMM-1 hybrid guided multipurpose missiles (3/point), or

12x MK-82 LDGB conventional bombs (3/point), or

6x RMS-1 large anti-ship reaction missiles (2/outboard point, 1/inboard point), or

4x UUM-7 micro-missile pods (1/point) each carrying 15 x Bifors HMM-01 micro-missiles,

or a combination of above load-outs

  

The kit and its assembly:

Well, once in a while I dig one of these vintage ARII kits out of the mecha pile and let the spirits flow. This time it was a distraction from Corona cabin fever, and this Valkyrie is heavily based on a profile drawing published in the Macross source book “Variable Fighter Master File VF-1 Valkyrie”, p. 122; an online version of this profile can be found here:

 

mechajournal.com/wp-content/uploads/2016/03/2010-1-SVF-65...

 

It shows aircraft “100”, though, the machine of SVF-65’s squadron leader, a VF-1 in an all-light blue livery with blue and white trim and some exotic details like a blue canopy frame or a yellow buzz number. I always found this scheme quite attractive, so I decided to replicate it with a model.

However, I was not able to 100% copy the look of “NE 100”, so I rather decided to build a standard fighter from this unit, with a slightly less flashy livery but still as close to the benchmark as possible.

 

Concerning the model, it’s another vintage ARII VF-1, in this case a basic VF-1A. It was built OOB, with the landing gear retracted, a scratched wire display that sticks in the gun pod’s rear end and holds the Valkyrie in flight, and the simple model received a few standard personal updates like a pilot figure and some blade antennae. The ordnance is strictly OOB.

  

Painting and markings:

The basic colors are Humbrol 47 (Sea Blue) overall, with white (Revell 301, a very pure/cold tone) on nose and fins and dark blue (Humbrol 15, Midnight Blue) and medium blue (Humbrol 48, Mediterranean Blue) trim lines. As mentioned above, I tried to stay as close to the benchmark profile as possible, and this posed some challenges.

Painting was done, as usual, only with brushes. The trim on fins, legs and wings was created with paint and masking, while the cheatlines under the cockpit were “faked” with enamel paint on decal sheet, since masking would have been a messy affair in this section of the tiny model. The grey leading edges on wings and fins were done with decal material, too.

 

After a black ink wash, very light post-shading was added. The decals and stencils come mostly from the OOB sheet, which turned out to be tough customers because it took them ages to detach from the carrier paper. The tactical codes were gathered from the scrap box: the “114”s come from a 1:72 Canadair Tutor trainer (their BuNo), the “NE” code on the fin with 3D effect was created from yellow and black single letters of the same size placed one above the other. The “SVF-65”, “ARMD-5” and “AKAGI” tags were created at home with an ink jet printer and respective clear carrier film.

Finally, after some typical highlights with clear paint had been added, the small VF-1 was sealed with a semi-gloss acrylic varnish.

  

A small and quick interim project, realized in just a few days – most time passed while waiting for the gloss Humbrol enamels to cure properly. There are certainly better VF-1 kits, but I just love those simple vintage ARII models. Staying close to the benchmark profile was quite a challenge, but worked out fine, and the compromise of a “normal” fighter of the unit with slightly simplified markings turned out well. And it’s certainly not the last Valkyrie of this kind to come…

 

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

  

Some background:

The Ling-Temco-Vought A-7 Corsair II was a carrier-capable subsonic light attack aircraft introduced to replace the Douglas A-4 Skyhawk. The A-7 airframe design was based on the successful supersonic Vought F-8 Crusader, although it was somewhat smaller and rounded off. The Corsair II initially entered service with the United States Navy during the Vietnam War. It was later adopted by the United States Air Force, including the Air National Guard, to replace the Douglas A-1 Skyraider and North American F-100 Super Sabre. The aircraft was also exported to several foreign countries, including Greece, Portugal, Thailand and New Zealand.

 

For the latter operator, the Corsair II was part of a major modernization campaign in the early 1970s. For instance, in 1970 14 McDonnell Douglas A-4 Skyhawks were purchased to replace the Vampire FB5's, which had been the primary light attack aircraft for the RNZAF for years, but the type was hopelessly outdated.

Furthermore New Zealand was also looking for a replacement of its similarly ageing Canberra fleet. These 31 aircraft were also phased out of service in mid 1970, and the A-7 chosen as the RNZAFs new fighter bomber because of its proven all-weather strike capability and advances avionics.

 

The RNZAF bought and operated 22 LTV A-7 Corsair II aircraft primarily in the coastal defense/anti-ship and sea patrol roles, air interdiction and air defense roles being secondary duties. The RNZAF Corsair II was very similar to the US Navy’s A-7E, even though the machines would only be operated form land bases. Designated A-7N, the machines featured an AN/APN-190 navigational radar with a Doppler groundspeed and drift detector plus an AN/APQ-128 terrain following radar. For the deployment of smart weapons, the machines were outfitted with a Pave Penny laser target acquisition system under the air intake lip, similar to the USAF’s A-7D, and could carry a wide range of weaponry and sensors, including AN/AAR-45 FLIR pods for an improved all-weather performance. Against enemy ships and large ground targets, visually guided smart bombs (AGM-62 and the more modern GBU-8 HOBOS) were bought, as well as AGM-65 Maverick against smaller, high priority targets.

 

Active service lasted between 1975 and 1999, and the A-7Ns were originally allocated between RNZAF 2 and 75 Squadron at Ohakea, where they were operated together with A-4K and TA-4K. The latter were also emplyed for A-7N pilot conversion training, since the RNZAF did not operate any Corsair II two seaters.

Several times the Squadron deployed to Clark Air Base in the Philippines and to Hawaii with both of the Corsair IIs and Skyhawks to exercise with the United States Air Force. Furthermore, the annual deployments as part of the Five Power Defence Agreement (called Exercise Vanguard) had the Squadron visit Australia, Singapore, Malaysia and Thailand to practice with those countries. Two RNZAF A-7s of 75 Squadron even made visits to Great Britain.

 

In the early Nineties the Corsair IIs started to suffer from numerous maintenance and logistic problems due to the lack of spare parts and general financial problems. This also prevented a major avionics update and the procurement of AGM-84 Harpoon missiles for the A-7Ns and the RNZAF P-3 Orion maritime patrol aircraft. The maintenance situation became so dire that several aircraft were cannibalized for spare parts to service other fighters. In 1992 only sixteen A-7Ns remained operational. This resulted in the available fighters no longer being assigned and dedicated to one specific squadron, but shared and assigned to one of the RNZAF combat squadrons (2, 14 and 75 Squadron, respectively), as needed.

 

During its 24 years of duty in the RNZAF, the A-7 fleet suffered 8 severe accidents with aircraft losses (and two pilots being killed). Nevertheless, the introduction of the A-7 was seen as a success due to the evolution that it allowed the Air Force in aircraft maintenance, with focus in modern computer and electronic systems, and in the steady qualification of pilots and technicians.

 

In 1999, the National Government selected an order of 28 F-16A/B Fighting Falcon aircraft to replace the complete fleet of A-4 Skyhawks and A-7 Corsair IIs, but this procurement plan was cancelled in 2001 following election by the incoming Labour Government under Helen Clark. This was followed by the disbanding of several fixed wing aircraft squadrons, with the consequence of removing the RNZAF's air combat capability. The last A-7 flight in RNZAF service took place on 1st of October 2001. Subsequently, most of the RNZAF's fighter pilots left New Zealand to serve in the Royal Australian Air Force and the Royal Air Force.

 

General characteristics:

Crew: 1

Length: 46 ft 2 in (14.06 m)

Wingspan: 38 ft 9 in (11.8 m), 23 ft 9 in (7.24 m) wings folded

Height: 16 ft 1 in (4.9 m)

Wing area: 374.9 sq ft (34.83 m²)

Airfoil: NACA 65A007 root and tip

Empty weight: 19,127 lb (8,676 kg)

Max takeoff weight: 41,998 lb (19,050 kg) overload condition.

Fuel capacity: 1,338 US gal (5,060 l; 1,114 imp gal) (10,200 lb (4,600 kg)) internal

 

Powerplant:

1 × Allison TF41-A-2 non-afterburning turbofan engine, 15,000 lbf (66.7 kN) thrust

 

Performance:

Maximum speed: 600 kn (690 mph; 1,111 km/h) at Sea level

Range: 1,070 nmi; 1,231 mi (1,981 km) maximum internal fuel

Ferry range: 1,342 nmi; 1,544 mi (2,485 km) with maximum internal and external fuel

Service ceiling: 42,000 ft (13,000 m)

Wing loading: 77.4 lb/sq ft (378 kg/m²)

Thrust/weight: 0.50

Take-off run: 1,705 ft (519.7 m) at 42,000 lb (19,000 kg)

 

Armament:

1× M61A1 Vulcan 20 mm (0.787 in) rotary cannon with 1,030 rounds

6× under-wing and 2× fuselage pylon stations (for mounting AIM-9 Sidewinder AAMs only)

with a total ordnance capacity of 15,000 lb (6,803.9 kg)

  

The kit and its assembly:

An idea that had been lingering on my project list for some years, and a recent build of an RNZAF A-7 by fellow modeler KiwiZac at whatifmodelers.com eventually triggered this build, a rather simple alternative livery whif. I had this idea on the agenda for some time, though, already written up a background story (which was accidently deleted early last year and sent the project into hiatus - until now) and had the kit as well as decals collected and stashed away.

 

The basis is the Hobby Boss A-7, which is available in a wide range of variant in 1:72 scale. Not cheap, but IMHO the best Corsair II kit at the moment, because it is full of ample surface details, goes together nicely and features a complete air intake, a good cockpit tub and even some maintenance covers that can be displayed in open position, in case you want to integrate the kit in a diorama. In my case it’s the A-7E kit, because I wanted a late variant and the US Navy’s refueling probe instead of the A-7D’s dorsal adapter for the USAF refueling boom system.

 

For the fictional RNZAF A-7N no fundamental changes were made. I just deliberately used OOB parts like the A-7D’s Pave Penny laser targeting pod under the air intake. As a personal addition I lowered the flaps slightly for a more lively look. Around the hull, some blade antennae were changed or added, and I installed the pair of pitots in front of the windscreen (made from thin wire).

 

The FLIR pod came with the kit, as well as the drop tank under the inner starboards wing pylon and the AIM-9Bs. Only the GBU-8s were externally sourced, from one of the Hasegawa USAF ordnance sets.

 

For the finalized kit on display I mounted the maintenance covers in open position, but for the beauty pics they were provisionally placed in closed position onto the kit’s flanks. The covers had to be modified for this stunt, but since their fit is very good and tight they easily stayed in place, even for the flight scenes!

 

Painting and markings:

This was the more interesting part – I wanted „something special“ for the fictional RNZAF Corsair II. Upon delivery, the USAF SEA scheme would certainly have been the most appropriate camouflage – the A-4K’s were painted this way and the aforementioned inspiring build by KiwiZac was finished this way.

 

Anyway, my plan had been from the start a machine in late service with low-viz markings similar to the A-4Ks, which received an attractive three-tone wrap-around scheme (in FS 34102, 34079 and 36081) or a simple all-around coat of FS 34079.

 

Both of these schemes could have been a sensible choice for this project, but… no! Too obvious, too simple for my taste. I rather wanted something that makes you wonder and yet make the aircraft look authentic and RNZAF-esque.

 

While digging for options and alternatives I stumbled upon the RNZAF’s C-130 Hercules transporters, which, like Canadian machines, carry a wrap-around scheme in two tones of grey (a light blue grey and a darker tone with a reddish hue) and a deep olive green tone that comes close to Dark Slate Grey, together with low-viz markings. A pretty unique scheme! Not as murky as the late A-4Ks and IMHO also well suited for the naval/coastal environment that the machine would patrol.

 

I was not able to positively identify the original tones on the CAF and RNZAF Hercs, so I interpreted various aircraft pictures. I settled upon Humbrol 163 (RAF Dark Green) 125 (FS 36118, Gunship Grey) and Revell 57 (RAL 7000, similar to FS 35237, but lighter and “colder”). For the wraparound scheme I used the C-130s as benchmark.

 

The cockpit became Dark Gull Grey (Humbrol 140) while the landing gear and the air intake duct became – behind 5mm of grey around the intake lip - white. The maintenance hatches’ interior was painted with a mix of Humbrol 81 and 38, for a striking zinc chromate primer look.

 

After a light black ink wash the kit received some panel post-shading for more contrast esp. between the dark colors and a slightly worn and sun-bleached look, since the aircraft would be depicted towards the end of its active service life.

 

Decals were the most challenging task, though: finding suitable RNZAF roundels is not easy, and I was happy when Xtradecal released an appropriate sheet that offers kiwi roundels for all positions (since motifs for port and starboard have to be mirrored). The Kiwi squadron emblem actually belongs to an RNZAF A-4K (from an Old Models sheet). The serial codes were puzzled together from single letter (TL Modellbau), most stencils come from the Hobby Boss OOB sheet.

  

A simple build, yet a very interesting topic and in the end also an IMHO very cool-looking aircraft in its fictional livery. Building the Hobby Boss A-7 was easy, despite some inherent flaws of the kit (e .g. totally blank dashboard and side consoles, and even no decals included!). The paint scheme lent from the RNZAF Hercs suits the SLUF well, though.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

  

The KAI T-50 Golden Eagle (골든이글) is a family of South Korean supersonic advanced trainers and light combat aircraft, developed by Korea Aerospace Industries (KAI) with Lockheed Martin. The T-50 is South Korea's first indigenous supersonic aircraft and one of the world's few supersonic trainers.

 

The T-50 program started in the late Nineties and was originally intended to develop an indigenous trainer aircraft capable of supersonic flight, to train and prepare pilots for the KF-16 and F-15K, replacing trainers such as T-38 and A-37 that were then in service with the ROKAF. Prior South Korean aircraft programs include the turboprop KT-1 basic trainer produced by Daewoo Aerospace (now part of KAI), and license-manufactured KF-16.

 

The mother program, code-named KTX-2, began in 1992, but the Ministry of Finance and Economy suspended the original project in 1995 due to financial constraints. The basic design of the aircraft was set by 1999, and eventually the development of the aircraft was funded 70% by the South Korean government, 17% by KAI, and 13% by Lockheed Martin.

 

In general, the T-50 series of aircraft closely resembles the KF-16 in configuration, but it actually is a completely new design: the T-50 is 11% smaller and 23% lighter than an F-16, and in order to create enough space for the two-seat cockpit, the air intake was bifurcated and placed under the wing gloves, resembling the F/A-18's layout.

 

The aircraft was formally designated as the T-50 'Golden Eagle' in February 2000, the T-50A designation had been reserved by the U.S. military to prevent it from being inadvertently assigned to another aircraft model. Final assembly of the first T-50 took place between 15 January and 14 September 2001. The first flight of the T-50 took place in August 2002, and initial operational assessment from 28 July to 14 August 2003.

 

The trainer has a cockpit for two pilots in a tandem arrangement, both crew members sitting in "normal" election seats, not in the F-16's reclined position. The high-mounted canopy is applied with stretched acrylic, providing the pilots with good visibility, and has been tested to offer the canopy with ballistic protection against 4-lb objects impacting at 400 knots.

 

The ROKAF, as original development driver, placed an initial production contract for 25 T-50s in December 2003, with aircraft scheduled to be delivered between 2005 and 2009. Original T-50 aircraft were equipped with the AN/APG-67(v)4 radar from Lockheed Martin. The T-50 trainer is powered by a GE F404 engine built under license by Samsung Techwin. Under the terms of the T-50/F404-102 co-production agreement, GE provides engine kits directly to Samsung Techwin who produces designated parts as well as performing final engine assembly and testing.

 

The T-50 program quickly expanded beyond a pure trainer concept to include the TA-50 armed trainer aircraft, as well as the FA-50 light attack aircraft, which has already similar capabilities as the multirole KF-16. Reconnaissance and electronic warfare variants were also being developed, designated as RA-50 and EA-50.

 

The TA-50 variant is a more heavily armed version of the T-50 trainer, intended for lead-in fighter training and light attack roles. It is equipped with an Elta EL/M-2032 fire control radar and designed to operate as a full-fledged combat platform. This variant mounts a lightweight three-barrel cannon version of the M61 Vulcan internally behind the cockpit, which fires linkless 20 mm ammunition. Wingtip rails can accommodate the AIM-9 Sidewinder missile, a variety of additional weapons can be mounted to underwing hardpoints, including precision-guided weapons, air-to-air missiles, and air-to-ground missiles. The TA-50 can also mount additional utility pods for reconnaissance, targeting assistance, and electronic warfare. Compatible air-to-surface weapons include the AGM-65 Maverick missile, Hydra 70 and LOGIR rocket launchers, CBU-58 and Mk-20 cluster bombs, and Mk-82, -83, and -84 general purpose bombs.

 

Among the operators of the TA-50 are the Philippines, Thailand and the ROKAF, and the type has attracted a global interest, also in Europe. The young Republic of Scotland Air Corps (locally known as Poblachd na h-Alba Adhair an Airm) chose, soon after the country's independence from the United Kingdom, after its departure from the European Union in 2017, the TA-50 as a complement to its initial procurements and add more flexibility to its small and young air arm.

 

According to a White Paper published by the Scottish National Party (SNP) in 2013, an independent Scotland would have an air force equipped with up to 16 air defense aircraft, six tactical transports, utility rotorcraft and maritime patrol aircraft, and be capable of “contributing excellent conventional capabilities” to NATO. Outlining its ambition to establish an air force with an eventual 2,000 uniformed personnel and 300 reservists, the SNP stated the organization would initially be equipped with “a minimum of 12 interceptors in the Eurofighter/Typhoon class, based at Lossiemouth, a tactical air transport squadron, including around six [Lockheed Martin] C-130J Hercules, and a helicopter squadron”.

 

According to the document, “Key elements of air forces in place at independence, equipped initially from a negotiated share of current UK assets, will secure core tasks, principally the ability to police Scotland’s airspace, within NATO.” An in-country air command and control capability would be established within five years of a decision in favor of independence, it continues, with staff also to be “embedded within NATO structures”.

This plan was immediately set into action after the country's independence in late 2017 with the purchase of twelve refurbished Saab JAS 39A Gripen interceptors for Quick Reaction Alert duties and upgraded, former Swedish Air Force Sk 90 trainers for the RoScAC. But these second hand machines were just the initial step in the mid-term procurement plan.

 

The twelve KAI TA-50 aircraft procured as a second step were to fulfill the complex requirement for a light and cost-effective multi-purpose aircraft that could be used in a wide variety of tasks: primarily as an advanced trainer for supersonic flight and as a trainer for the fighter role (since all Scottish Gripens were single seaters and dedicated to the interceptor/air defense role), but also as a light attack and point defense aircraft.

 

Scotland was offered refurbished F-16C and Ds, but this was declined as the type was deemed to be too costly and complex. Beyond the KAI T-50, the Alenia Aermacchi M-346 Master and the BAe Hawk were considered, too, but, eventually, a modified TA-50 that was tailored to the RoScAC’s procurement plans was chosen by the Scottish government.

 

In order to fulfill the complex duty profile, the Scottish TA-50s were upgraded with elements from the FA-50 attack aircraft. They possess more internal fuel capacity, enhanced avionics, a longer radome and a tactical datalink. Its EL/M-2032 pulse-Doppler radar has been modified so that it offers now a range two-thirds greater than the TA-50's standard radar. It enables the aircraft to operate in any weather, detect surface targets and deploy AIM-120 AAMs for BVR interceptions. The machines can also be externally fitted with Rafael's Sky Shield or LIG Nex1's ALQ-200K ECM pods, Sniper or LITENING targeting pods, and Condor 2 reconnaissance pods to further improve the machine’s electronic warfare, reconnaissance, and targeting capabilities.

 

Another unique feature of the Scottish Golden Eagle is its powerplant: even though the machines are originally powered by a single General Electric F404 afterburning turbofan and designed around this engine, the RoScAC TF-50s are powered by a Volvo RM12 low-bypass afterburning turbofan. These are procured and serviced through Saab in Sweden, as a part of the long-term collaboration contract for the RoScAC’s Saab Gripen fleet. This decision was taken in order to decrease overall fleet costs through a unified engine.

 

The RM12 is a derivative of the General Electric F404-400. Changes from the standard F404 includes greater reliability for single-engine operations (including more stringent birdstrike protection) and slightly increased thrust. Several subsystems and components were also re-designed to reduce maintenance demands, and the F404's analogue Engine Control Unit was replaced with the Digital Engine Control – jointly developed by Volvo and GE – which communicates with the cockpit through the digital data buses and, as redundancy, mechanical calculators controlled by a single wire will regulate the fuel-flow into the engine.

 

Another modification of the RoScAC’s TA-50 is the exchange of the original General Dynamics A-50 3-barrel rotary cannon for a single barrel Mauser BK-27 27mm revolver cannon. Being slightly heavier and having a lower cadence, the BK-27 featured a much higher kinetic energy, accuracy and range. Furthermore, the BK-27 is the standard weapon of the other, Sweden-built aircraft in RoScAC service, so that further synergies and cost reductions were expected.

 

The Scottish Department of National Defense announced the selection of the TA-50 in August 2018, after having procured refurbished Saab Sk 90 and JAS 39 Gripen from Sweden as initial outfit of the country's small air arm with No. 1 Squadron based at Lossiemouth AB.

 

Funding for the twelve aircraft was approved by Congress on September 2018 and worth € 420 mio., making the Golden Eagle the young country’s first brand new military aircraft. Deliveries of the Golden Hawk TF.1, how the type was officially designated in Scottish service, began in November 2019, lasting until December 2020.

The first four Scottish Golden Hawk TF.1 aircraft were allocated to the newly established RoScAC No. 2 Squadron, based at Leuchars, where the RoScAC took control from the British Army. The latter had just taken over the former air base from the RAF in 2015, losing its “RAF air base” status and was consequentially re-designated “Leuchars Station”, primarily catering to the Royal Scots Dragoon Guards who have, in the meantime, become part of Scotland’s Army Corps. The brand new machines were publically displayed on the shared army and air corps facility in the RoScAC’s new paint scheme on 1st of December 2019 for the first time, and immediately took up service.

 

General characteristics:

Crew: 2

Length: 13.14 m (43.1 ft)

Wingspan (with wingtip missiles): 9.45 m (31 ft)

Height: 4.94 m (16.2 ft)

Wing area: 23.69 m² (255 ft²)

Empty weight: 6,470 kg (14,285 lb)

Max. takeoff weight: 12,300 kg (27,300 lb)

 

Powerplant:

1× Volvo RM12 afterburning turbofan, rated at 54 kN (12,100 lbf) dry thrust

and 80.5 kN (18,100 lbf) with afterburner

 

Performance:

Maximum speed: Mach 1.5 (1,640 km/h, 1,020 mph at 9,144 m or 30,000 ft)

Range: 1,851 km (1,150 mi)

Service ceiling: 14,630 m (48,000 ft)

Rate of climb: 198 m/s (39,000 ft/min)

Thrust/weight: 0.96

Max g limit: -3 g / +8 g

 

Armament:

1× 27mm Mauser BK-27 revolver cannon with 120 rounds

A total of 7 hardpoints (4 underwing, 2 wingtip and one under fuselage)

for up to 3,740 kg (8,250 lb) of payload

  

The kit and its assembly:

A rare thing concerning my builds: an alternative reality whif. A fictional air force of an independent Scotland crept into my mind after the hysterical “Brexit” events in 2016 and the former (failed) public vote concerning the independence of Scotland from the UK. What would happen to the military, if the independence would take place, nevertheless, and British forces left the country?

 

The aforementioned Scottish National Party (SNP) paper from 2013 is real, and I took it as a benchmark. Primary focus would certainly be set on air space defense, and the Gripen appears as a good and not too expensive choice. The Sk 90 is a personal invention, but would fulfill a good complementary role.

Nevertheless, another multi-role aircraft would make sense as an addition, and both M-346 and T-50 caught my eye (Russian options were ruled out due to the tense political relations), and I gave the TA-50 the “Go” because of its engine and its proximity to the Gripen.

 

The T-50 really looks like the juvenile offspring from a date between an F-16 and an F-18. There’s even a kit available, from Academy – but it’s a Snap-Fit offering without a landing gear but, as an alternative, a clear display that can be attached to the engine nozzle. It also comes with stickers instead of waterslide decals. This sounds crappy and toy-like, but, after taking a close look at kit reviews, I gave it a try.

 

And I am positively surprised. While the kit consists of only few parts, moulded in the colors of a ROCAF trainer as expected, the surfaces have minute, engraved detail. Fit is very good, too, and there’s even a decent cockpit that’s actually better than the offering of some “normal” model kits. The interior comes with multi-part seats, side consoles and dashboards that feature correctly shaped instrument details (no decals). The air intakes are great, too: seamless, with relatively thin walls, nice!

 

So far, so good. But not enough. I could have built the kit OOB with the landing gear tucked up, but I went for the more complicated route and trans-/implanted the complete landing gear from an Intech F-16, which is available for less than EUR 5,- (and not much worth, to be honest). AFAIK, there’s white metal landing gear for the T-50 available from Scale Aircraft Conversions, but it’s 1:48 and for this set’s price I could have bought three Intech F-16s…

 

But back to the conversion. This landing gear transplantation stunt sounds more complicated as it actually turned out to be. For the front wheel well I simply cut a long opening into the fuselage and added inside a styrene sheet as a well roof, attached under the cockpit floor.

For the main landing gear I just opened the flush covers on the T-50 fuselage, cut out the interior from the Intech F-16, tailored it a little and glued it into its new place.

 

This was made easy by the fact that the T-50 is a bit smaller than the F-16, so that the transplants are by tendency a little too large and offer enough “flesh” for adaptations. Once in place, the F-16 struts were mounted (also slightly tailored to fit well) and covers added. The front wheel cover was created with 0.5 mm styrene sheet, for the main covers I used the parts from the Intech F-16 kit because they were thinner than the leftover T-50 fuselage parts and feature some surface detail on the inside. They had to be adapted in size, though. But the operation worked like a charm, highly recommended!

 

Around the hull, some small details like missing air scoops, some pitots and antennae were added. In a bout of boredom (while waiting for ordered parts…) I also added static dischargers on the aerodynamic surfaces’ trailing edges – the kit comes with obvious attachment points, and they are a small detail that improves the modern look of the T-50 even more.

 

Since the Academy kit comes clean with only a ventral drop tank as ordnance, underwing pylons from a SEPECAT Jaguar (resin aftermarket parts from Pavla) and a pair of AGM-65 from the Italeri NATO Weapons set plus launch rails were added, plus a pair of Sidewinders (from a Hasegawa AAM set, painted as blue training rounds) on the wing tip launch rails.

Since the T-50 trainer comes unarmed, a gun nozzle had to be added – its position is very similar to the gun on board of the F-16, on the upper side of the port side LERX. Another addition are conformal chaff/flare dispensers at the fin’s base, adding some beef to the sleek aircraft.

  

Painting and markings:

I did not want a grey-in-grey livery, yet something “different” and rather typical or familiar for the British isles. My approach is actually a compromise, with classic RAF colors and design features inspired by camouflage experiments of the German Luftwaffe on F-4F Phantoms and Alpha Jets in the early Eighties.

 

For the upper sides I went for a classic British scheme, in Dark Green and Dark Sea Grey (Humbrol 163 and 164), colors I deem very appropriate for the Scottish landscape and for potential naval operations. These were combined with elements from late RAF interceptors: Barley Grey (Humbrol 167) for the flanks including the pylons, plus Light Aircraft Grey (Humbrol 166) for the undersides, with a relatively high waterline and a grey fin, so that a side or lower view would rather blend with the sky than the ground below.

 

Another creative field were the national markings: how could fictional Scottish roundels look like, and how to create them so that they are easy to make and replicate (for a full set for this kit, as well as for potential future builds…)? Designing and printing marking decals myself was an option, but I eventually settled for a composite solution which somewhat influenced the roundels’ design, too.

My Scottish roundel interpretationconsists of a blue disk with a white cross – it’s simple, different from any other contemporary national marking, esp. the UK roundel, and easy to create from single decal parts. In fact, the blue roundels were die-punched from blue decal sheet, and the cross consists of two thin white decal strips, cut into the correct length with the same stencil, using generic sheet material from TL Modellbau.

 

Another issue was the potential tactical code, and a small fleet only needs a simple system. Going back to a WWII system with letter codes for squadrons and individual aircraft was one option, but, IMHO, too complicated. I adopted the British single letter aircraft code, though, since this system is very traditional, but since the RoScAC would certainly not operate too many squadrons, I rather adapted a system similar to the Swedish or Spanish format with a single number representing the squadron. The result is a simple 2-digit code, and I adapted the German system of placing the tactical code on the fuselage, separated by the roundel. Keeping British traditions up I repeated the individual aircraft code letter on the fin, where a Scottish flag, a small, self-printed Fife coat-or-arms and a serial number were added, too.

 

The kit saw only light weathering and shading, and the kit was finally sealed with matt acrylic varnish (Italeri).

  

Creating this whif, based on an alternative historic timeline with a near future perspective, was fun – and it might spawn more models that circle around the story. A Scottish Sk 90 and a Gripen are certain options (and for both I have kits in the stash…), but there might also be an entry level trainer, some helicopters for the army and SAR duties, as well as a transport aircraft. The foundation has been laid out, now it’s time to fill Scotland’s history to come with detail and proof. ;-)

 

Besides, despite being a snap-fit kit, Academy’s T-50 is a nice basis, reminding me of some Hobby Boss kits but with less flaws (e .g. most of the interiors), except for the complete lack of a landing gear. But with the F-16 and Jaguar transplants the simple kit developed into something more convincing.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

In 1948, a swept wing version of the F-84 was created with the hope of bringing performance to the level of the F-86. The last production F-84E was fitted with a swept tail, a new wing with 38.5 degrees of leading-edge sweep and 3.5 degrees of anhedral, and a J35-A-25 engine producing 5,300 pound-force (23.58 kN) of thrust. The aircraft was designated XF-96A and flew on 3 June 1950. Although the airplane was capable of 602 knots (693 mph, 1,115 km/h), the performance gain over the F-84E was considered minor. Nonetheless, it was ordered into production in July 1950 as the F-84F Thunderstreak. The F-84 designation was eventually retained because the fighter was expected to be a low-cost improvement of the straight-wing Thunderjet with over 55 percent commonality in tooling.

 

In the meantime, the USAF, hoping for improved high-altitude performance from a more powerful engine, arranged for the British Armstrong Siddeley Sapphire turbojet engine to be built in the United States as the Wright J65. To accommodate the larger engine, YF-84Fs with a British-built Sapphire as well as production F-84Fs with the J65 had a vertically stretched fuselage, with the air intake attaining an oval cross-section. Production quickly ran into problems, though. Although tooling commonality with the Thunderjet was supposed to be 55 %, but just 15 % of the tools could actually be re-used. To make matters worse, the F-84F utilized press-forged wing spars and ribs. At the time, only three presses in the United States could manufacture these, and priority was given to the Boeing B-47 Stratojet bomber over the F-84. The YJ65-W-1 engine was considered obsolete, too, and the improved J65-W-3 did not become available until 1954. When the first production F-84F flew on 22 November 1952, it was considered not ready for operational deployment due to control and stability problems. The first 275 aircraft, equipped with conventional stabilizer-elevator tailplanes, suffered from accelerated stall pitch-up and poor turning ability at combat speeds. Beginning with Block 25, the problem was improved upon by the introduction of a hydraulically powered one-piece stabilator. A number of aircraft were also retrofitted with spoilers for improved high-speed control. As a result, the F-84F was not declared operational until 12 May 1954.

 

The second YF-84F prototype was completed with wing-root air intakes. These were not adopted for the fighter due to loss of thrust, but this arrangement kept the nose section free and permitted placement of cameras, and the different design was adopted for the RF-84F Thunderflash reconnaissance version. Being largely identical to the F-84F, the Thunderflash suffered from the same production delays and engine problems, though, delaying operational service until March 1954.

 

During the F-84F’s development the Air Defense Command was looking for a replacement for the outdated F-94 ‘Starfire’ interceptor, a hasty development from the T-33 trainer airframe with an afterburner engine and an on-board radar. However, the F-94 was only armed with machine guns in its early versions or unguided missiles in its later incarnations, which were inadequate. An aircraft with better performance, ideally with supersonic speed, a better radar, and the ability to carry guided missiles (in the form if the AIR-1 and 2 ‘Falcon’ AAMs) as well as the AIR-2 ‘Genie’ missile was now requested.

 

The Douglas AIR-2 Genie followed a unique but effective concept that represented the technological state-of-the-art: it was an unguided air-to-air rocket with a 1.5 kt W25 nuclear warhead. The interception of Soviet strategic bombers was a major military preoccupation of the late 1940s and 1950s. The World War II-age fighter armament of machine guns and cannon were inadequate to stop attacks by massed bomber formations, which were expected to come in at high altitude and at high subsonic speed. Firing large volleys of unguided rockets into bomber formations was not much better, and true air-to-air missiles were in their infancy. In 1954 Douglas Aircraft began a program to investigate the possibility of a nuclear-armed air-to-air weapon. To ensure simplicity and reliability, the weapon would be unguided, since the large blast radius made precise accuracy unnecessary. Full-scale development began in 1955, with test firing of inert warhead rockets commencing in early 1956. The final design carried a 1.5-kiloton W25 nuclear warhead and was powered by a Thiokol SR49-TC-1 solid-fuel rocket engine of 162 kN (36,000 lbf) thrust, sufficient to accelerate the rocket to Mach 3.3 during its two-second burn. Total flight time was about 12 seconds, during which time the rocket covered 10 km (6.2 mi). Targeting, arming, and firing of the weapon were coordinated by the launch aircraft's fire-control system. Detonation was by time-delay fuze, although the fuzing mechanism would not arm the warhead until engine burn-out, to give the launch aircraft sufficient time to turn and escape. However, there was no mechanism for disarming the warhead after launch. Lethal radius of the blast was estimated to be about 300 meters (980 ft). Once fired, the Genie's short flight-time and large blast radius made it virtually impossible for a bomber to avoid destruction. The rocket entered service with the designation MB-1 Genie in 1957.

 

During the development phase the first carrier aircraft earmarked to carry the AIR-2 was the Northrop F-89 Scorpion, which had already been introduced in the early Fifties. While being an all-weather interceptor with on-board radar, it was a slow and large aircraft, and outdated like the F-94. Trying to keep the F-84 production lines busy, however, Republic saw the chance to design an all-weather interceptor aircraft that would surpass the F-89’s mediocre performance and meet the AIR-2 carrier requirements on the basis of the swept-wing (R)F-84F. To emphasize its dedicated interceptor role and set it apart from its fighter-bomber ancestors, the heavily modified aircraft was designated F-96B (even though it had little to do with the XF-96A that became the F-84F) and called ‘Thunderguard’.

 

The F-96B was largely based on the RF-84F’s airframe with its wing-root air intakes, what offered ample space in the aircraft’s nose for a radar system and other equipment. The radar was coupled with a state-of-the-art Hughes MC-10 fire control system. To relieve the pilot from operating the radar system one of the fuel cells behind the cockpit was deleted and a second crew member was placed behind him under an extended, strutless hood that opened to starboard. To compensate for the loss of fuel and maintain the F-84F’s range, a new tank was mounted under the cockpit floor in the aircraft’s center of gravity.

To improve performance and cope with the raised take-off weight, the F-96B was powered by an uprated Wright J65-W-18 turbojet, which generated 0.4 kN more dry thrust than the F-84F’s original J65-W-3 (7,700 lbf/34 kN). This was not too much, though, so that the J65 was additionally outfitted with an afterburner. With this upgrade the powerplant provided a maximum thrust of 10,500 lbf (47 kN), what resulted in a markedly improved rate of climb and the ability to break the sound barrier in level flight. The additional reheat section necessitated a wider and longer rear fuselage, which had to be redesigned. As an unintended side benefit, this new tail section reduced overall drag due to a slightly area-ruled coke-bottle shape behind the wings’ trailing edge, which was even emphasized through the ventral brake parachute fairing.

Armament consisted only of missiles, which were all carried externally on wing stations, all guns of the former F-84 versions were deleted to save weight. The F-96B’s weapons range included GAR-1/2/3/4 (Later re-designated as AIM-4) radar- and IR-guided Falcon air-to-air missiles and a pair of MB-1 Genie missiles. Up to four pods with nineteen unguided 2.75 in (70 mm) "Mighty Mouse" Mk 4/Mk 40 Folding-Fin Aerial Rockets each were an alternative, too, and a pair of drop tanks were typically carried under the inner wings to provide the aircraft with sufficient range, since the new afterburner significantly increased fuel consumption.

 

Even though it was only a derivative design, the F-96B introduced a lot of innovations. One of these was the use of a diverertless supersonic inlet (DSI), a novel type of jet engine air intake to control air flow into their engines. Initial research into the DSI was done by Antonio Ferri in the 1950s. It consisted of a "bump" and a forward-swept inlet cowl, which worked together to divert boundary layer airflow away from the aircraft's engine. In the case of the F-96B this was realized as an inward-turning inlet with a variable contraction ratio. However, even though they had not been deemed necessary to guarantee a clean airflow, the F-96B’s air intakes were further modified with splitter plates to adapt them to the expected higher flight speeds and direct the air flow. The initial flight tests had also revealed a directional instability at high speed, due to the longer nose, so that the tail surfaces (both fin and stabilizers) were enlarged for the serial aircraft to compensate.

 

Another novel feature was an IRST sensor in front of the windscreen which augmented the on-board radar. This sensor, developed by Hughes International and designated ‘X-1’, was still very experimental, though, highly unreliable, and difficult to handle, because it relied on pressurized coolant to keep the sensor cold enough to operate properly, and dosing it at a consistent level proved to be difficult (if not impossible). On the other side the IRST allowed to track targets even in a massively radar-jammed environment. The 7” diameter silicone sensor was, together with the on-board radar, slaved to the fire control system so that its input could be used to lock guided missiles onto targets, primarily the GAR-1 and GAR-2 AAMs. The X-1 had a field of view of 70×140°, with an angular resolution of 1°, and operated in 2.5 micron wavelength range. When it worked properly the sensor was able to detect a B-47-sized aircraft’s tails aspect from 25 nm (29 ml/46 km) and a target of similar size from directly ahead from 10 nm (12 ml/19 km). Later, better developed versions of Hughes IRST, like the X-3 that was retrofitted to the F-101B in the early Sixties, had a better range and were more reliable.

 

During the Thunderguard’s development another competitor entered the stage, the F-101B Voodoo. In the late 1940s, the Air Force had already started a research project into the future interceptor aircraft that eventually settled on an advanced specification known as the 1954 interceptor. Contracts for this specification eventually resulted in the selection of the F-102 Delta Dagger, but by 1952 it was becoming clear that none of the parts of the specification other than the airframe would be ready by 1954; the engines, weapons, and fire control systems were all going to take too long to get into service. An effort was then started to quickly produce an interim supersonic design to replace the various subsonic interceptors then in service, and the F-101 airframe was selected as a starting point. Although McDonnell proposed the designation F-109 for the new aircraft (which was to be a substantial departure from the basic Voodoo fighter bomber), the USAF assigned the designation F-101B. Its development was protracted, so that the F-96B – even though it offered less performance – was ordered into production to fill the USAF’s urgent interceptor gap.

 

F-96B production started after a brief test phase in late 1957, and the first aircraft were delivered to the 60th Fighter-Interceptor Squadron in 1958. However, when it became clear that the F-101B would finally enter service in 1959, F-96B production was quickly cut down and the initial order of 300 aircraft reduced to only 150, which were produced until early 1960 in three batches. Only sixty were directly delivered to ADC units, because these were preferably equipped with the supersonic F-102A and the new F-101B, which could also carry the nuclear Genie missile. The rest was directly handed over to Air National Guard units – and even there they were quickly joined and replaced by the early ADC aircraft.

 

Operationally, almost all F-96Bs functioned under the US–Canadian North American Air Defense Command (NORAD), which protected North American airspace from Soviet intruders, particularly the threat posed by nuclear-armed bombers. In service, the F-96Bs were soon upgraded with a data link to the Semi-Automatic Ground Environment (SAGE) system, allowing ground controllers to steer the aircraft towards its targets by making adjustments through the plane's autopilot. Furthermore, the F-96B was upgraded to allow the carrying of two GAR-11/AIM-26 Nuclear Falcon missiles instead of the Genies when they became available in 1961.

A handful F-96Bs were camouflaged during the late Sixties with the USAF’s new SEA scheme, but most aircraft retained their original bare metal finish with more or less colorful unit markings. Due to its limited capabilities and the introduction of the Mach 2 McDonnell F-4 Phantom, the last F-96B was retired from ANG service in 1971.

  

General characteristics:

Crew: 2

Length: 54t 11 1/2 in (16,77 m) incl. pitot

Wingspan: 33 ft 7.25 in (10,25 m)

Height: 16 ft 9 in (5,11 m)

Wing area: 350 sq ft (37,55 m²)

Empty weight: 13,810 lb (6.264 kg)

Gross weight: 21,035 lb (9.541 kg)

Max takeoff weight: 28,000 lb (12.701 kg)

 

Powerplant:

1× Wright J65-W-18 turbojet with 8,600 lbf (34 kN) dry thrust and 10,500 lbf (47 kN) with afterburner

 

Performance:

Maximum speed: 695 mph (1,119 km/h, 604 kn, Mach 1.1) at 35,000 ft (10,668 m)

Cruise speed: 577 mph (928 km/h, 501 kn)

Range: 810 mi (1,304 km, 704 nmi) combat radius with two droptanks

Service ceiling: 49,000 ft (15,000 m)

Rate of climb: 16,300 ft/min (83 m/s)

Wing loading: 86 lb/sq ft (423 kg/m²)

 

Armament:

No internal guns;

6× underwing hardpoints for a total ordnance load of up to 6,000lb (2,727 kg), including

a pair of 191.5 US gal (727 l) or 375 US gal (1.429 l) drop tanks on the inner stations

and a mix of AIM-4 Falcon (up to six), MB-1 Genie (up to two) and/or pods with

nineteen 2.75”/70 mm FFAR unguided missiles each (up to four) on the outer stations

  

The kit and its assembly:

This fictional missing link between the RF-84F and the F-105 was conceived for the Fifties Group Build at whatifmodellers.com, an era when the USAF used a wide variety of interceptor aircraft types and technical advancements were quick and significant – in just a decade the interceptor evolved from a subsonic machine gun-toting aircraft to a guided weapons carrier platform, capable of Mach 2.

 

The F-96B (I re-used Republic’s dropped designation for the swept-wing F-84F) was to display one of the many “in between” designs, and the (R)F-84F was just a suitable basis for a conversion similar to the T-33-derived F-94, just more capable and big enough to carry the nuclear Genie missile.

The basis became Italeri’s vintage RF-84F kit, a rather simple affair with raised panel lines and a mediocre fit, plus some sinkholes. This was, however, heavily modified!

 

Work started with the implantation of a new tandem cockpit, taken wholesale from a Heller T-33. Fitting the cockpit tub into the wider Thunderflash hull was a bit tricky, putty blobs held the implant in place. The canopy was taken from the T-33, too, just the RF-84F’s original rear side windows were cut away to offer sufficient length for the longer clear part and the cockpit side walls had to be raised to an even level with the smaller windscreen with the help of styrene strips. With these adapters the T-33 canopy fitted surprisingly well over the opening and blended well into the spine.

 

The camera nose section lost its tip, which was replaced with the tail cone from a Matchbox H.S. Buccaneer (actually its air brake), and the camera windows as well as the slant surfaces that held them were PSRed away for a conical shape that extended the new pointed radome. Lots of weight in the nose and under the cockpit floor ensured a safe stance on the OOB landing gear.

The rear section behind the air brakes became all-new; for an afterburner I extended and widened the tail section and implanted the rear part from a B-66 (Italeri kit, too) engine nacelle, which received a wider nozzle (left over from a Nakotne MiG-29, a featureless thing) and an interior.

To balance the longer nose I also decided to enlarge the tail surfaces and replaced the OOB fin and stabilizers with leftover parts from a Trumpeter Il-28 bomber – the fin was shortened and the stabilizers reduced in span to match the rest of the aircraft. Despite the exotic source the parts blend well into the F-84’s overall design!

 

To add supersonic credibility and to connect the design further with the later F-105 I modified the air intakes and cut them into a raked shape – quite easy to realize. Once the wings were in place, I also added small splitter plates, left over from an Airfix BAC Strikemaster.

 

As an interceptor the armament had to be adapted accordingly, and I procured the quartet of IR-guided Falcons as well as the Genie duo from an Academy F-89. The large drop tanks were taken OOB from the Italeri kit. The Genies were mounted onto their massive Scorpion pylons under the outer wings of the F-96B, while the Falcons, due to relatively little space left under the wings, required a scratched solution. I eventually settled for dual launchers on small pylons, mounted in front of the landing gear wells. The pylons originally belong to an ESCI Ka-34 “Hokum” helicopter kit (they were just short enough!), the launch rails are a halved pair of F-4 Sidewinder rails from a Hasegawa air-to-air weapons set. With everything on place the F-96B looks quite crowded.

  

Painting and markings:

The machine would represent a late Fifties USAF type, so that the paint options were rather limited if I wanted to be authentic. ADC Grey was introduced in the early Sixties, SEA camouflage even later, so that bare metal became a natural choice – but this can be quite attractive! The model received an overall coat with acrylic “White Aluminum” from the rattle can, plus some darked panels all over the hull (Humbrol 56 for good contrast) and an afterburner section in Revell 91 (Iron Metallic) and Humbrol’s Steel Metallizer. The radome became deep black, the anti-glare panel in front of the windscreen olive drab (Revell 46). Light grey (Revell 75) was used for some small di-electric fairings.

Interior surfaces (cockpit and landing gear wells) were painted with Zinc Chromate primer (I used Humbrol 80), while the landing gear struts became silver-grey (Humbrol 56) and the inside of the covers as well as the air brakes were painted in bright red (Humbrol 19).

Once basic painting was done the model received a black ink washing and was rubbed with grinded graphite to emphasize the raised panel lines, and the material adds a nice dark metallic shine to the silver base coat.

 

Another challenge was to find suitable unit markings for the Fifties era in the decal vault, which would also fit onto the model. After a long search I eventually settled for rather simple markings from a 325th FIS F-102 from an Xtradecal sheet, which only features a rather timid fin decoration.

Finding other suitable standard markings remained demanding, though. Stars-And-Bars as well as the USAF taglines were taken from the Academy F-89 that also provided the ordnance, most stencils were taken from the OOB Italeri sheet and complemented by small markings from the scrap box. The biggest problem was the creation of a matching serial number. The “FF” code was originally used for P/F-51D Mustangs during the Korea War, but after the type had been phased out it might have been re-used? The letters as well as the serial number digits were created from various markings for USAF F-100s, also from an Xtradecal sheet.

 

Once the decals had been applied the model was sealed with semi-gloss acrylic varnish, except for the radome, the anti-glare panel as well as the walking areas on the wings as well as parts of the afterburner section, which were coated with matt varnish.

  

A rather straightforward conversion, even though finishing the project took longer than expected. But the result looks surprisingly natural and plausible. Lots of PSR was needed to modify the fuselage, though, especially the tail section was not easy to integrate into the Thunderflash’s hull. Sticking to the simple NMF livery paid IMHO out, too: the livery looks very natural and believable on the fictional aircraft, and it suits the F-84’s bulbous shape well.

Already recognised as the most dynamically capable, performance-focused Jaguar, the F-TYPE sports car continues to evolve, with a fresh look, state-of-the-art infotainment system and world-first ReRun app that combines vehicle data with GoPro video to enhance the driving experience.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

 

Some background

The Focke Wulf Ta 338 originated as a response of request by the RLM in mid 1943 for an aircraft capable of vertical takeoff and landing (VTOL), optimized for the interceptor and point defense role and without a hazardous liquid rocket engine as means of propulsion. In the course of the year, several German manufacturers responded with a multitude of highly innovative if not unusual design, including Heinkel with the ducted fan project "Lerche", Rheinmetall-Borsig with a jet-powered tailsitter, and Focke Wulf. This company’s engineering teams submitted two designs: the revolutionary "Triebflügel" concept and the more conservative, yet still futuristic "P.03.10338" tail sitter proposal, conceived by Focke Wulf’s leading engineer Kurt Tank and Walter Kappus from BMW, responsible for the engine development.

 

The P.03.10338 was based on the proven Fw 190 fighter, but the similarities were only superficial. Only the wings and a part of the fuselage structure around the cockpit would be used, but Tank assumed that using existing parts and tools would appreciably reduce development and production time.

A great part of the fuselage structure had to be re-designed to accommodate a powerful BMW 803 engine and its integral gearbox for an eight-bladed contraprop.

 

The BMW 803 was BMW's attempt to build a high-output aircraft engine, primarily for heavy bombers, by basically "coupling" two BMW 801 engines back-to-back into a single and very compact power unit. The result was a 28-cylinder, four-row radial engine, each comprising a multiple-bank in-line engine with two cylinders in each bank, which, due to cooling concerns, were liquid cooled.

 

This arrangement was from the start intended to drive independent contra-rotating propellers, in order to avoid stiffness problems with the whole engine driving just a single crankshaft and also to simply convert the raw power of this unit into propulsion. The front half of the engine drove the front propeller directly, while the rear engine drove a number of smaller shafts that passed between the cylinders of the front engine before being geared back together to drive the rear prop. This complex layout resulted in a rather large and heavy gearbox on the front of the engine, and the front engine needing an extended shaft to "clear" that gearbox. The four-row 803 engine weighed 2,950 kg (6,490 lb) dry and 4,130 kg (9,086 lb) fully loaded, and initial versions delivered 3,900 PS (3,847 hp; 2,868 kW).

 

While the engine was heavy and there were alternatives with a better weight/output ratio (e. g. the Jumo 222), the BMW 803 was favored for this project because it was the most powerful engine available, and it was relatively compact so that it could be fitted into a fighter's airframe. On the P.03.10338 it drove an all-metal, eight-blade contraprop with a diameter of 4,25 m (13 ft 11 in).

 

In order to accept this massive engine, the P.03.10338’s structure had to be stiffened and the load-bearing structures re-arranged. The aircraft kept the Fw 190's wing structure and surface, but the attachment points at the fuselage had to be moved for the new engine mount, so that they ended up in mid position. The original space for the Fw 190's landing gear was used for a pair of radiator baths in the wings' inner leading edge, the port radiator catering to the front engine half while the radiator on starboard was connected with the rear half. An additional annular oil and sodium cooler for the gearbox and the valve train, respectively, was mounted in the fuselage nose.

 

The tail section was completely re-designed. Instead of the Fw 190's standard tail with fin and stabilizers the P.03.10338’s tail surfaces were a reflected cruciform v-tail (forming an x) that extended above and below the fuselage. On the four fin tips, aerodynamic bodies carried landing pads while the fuselage end contained an extendable landing damper. The pilot sat in a standard Fw 190 cockpit, and the aircraft was supposed to start and land vertically from a mobile launch pad. In the case of an emergency landing, the lower stabilizers could be jettisoned. Nor internal armament was carried, instead any weaponry was to be mounted under the outer wings or the fuselage, in the form of various “Rüstsätze” packages.

 

Among the many exotic proposals to the VTOL fighter request, Kurt Tank's design appeared as one of the most simple options, and the type received the official RLM designation Ta 338. In a rush of urgency (and maybe blinded by clever Wunderwaffen marketing from Focke Wulf’s side), a series of pre-production aircraft was ordered instead of a dedicated prototype, which was to equip an Erprobungskommando (test unit, abbreviated “EK”) that would evaluate the type and develop tactics and procedures for the new fighter.

 

Fueled by a growing number of bomber raids over Germany, the “EK338” was formed as a part of JG300 in August 1944 in Schönwalde near Berlin, but it took until November 1944 that the first Ta 338 A-0 machines were delivered and made operational. These initial eight machines immediately revealed several flaws and operational problems, even though the VTOL concept basically worked and the aircraft flew well – once it was in the air and cruising at speeds exceeding 300 km/h (186 mph).

 

Beyond the many difficulties concerning the aircraft’s handling (esp. the landing was hazardous), the lack of a landing gear hampered ground mobility and servicing. Output of the BMW 803 was sufficient, even though the aircraft had clear limits concerning the take-off weight, so that ordnance was limited to only 500 kg (1.100 lb). Furthermore, the noise and the dust kicked up by starting or landing aircraft was immense, and servicing the engine or the weapons was more complicated than expected through the high position of many vital and frequently tended parts.

 

After three Ta 338 A-0 were lost in accidents until December 1944, a modified version was ordered for a second group of the EK 338. This led to the Ta 338 A-1, which now had shorter but more sharply swept tail fins that carried single wheels and an improved suspension under enlarged aerodynamic bodies.

This machine was now driven by an improved BMW 803 A-2 that delivered more power and was, with an MW-50 injection system, able to produce a temporary emergency output of 4.500 hp (3.308 kW).

 

Vertical start was further assisted by optional RATO units, mounted in racks at the rear fuselage flanks: either four Schmidding SG 34 solid fuel booster rockets, 4.9 kN (1,100 lbf) thrust each, or two larger 9.8 kN (2,203 lbf) solid fuel booster rockets, could be used. These improvements now allowed a wider range of weapons and equipment to be mounted, including underwing pods with unguided rockets against bomber pulks and also a conformal pod with two cameras for tactical reconnaissance.

 

The hazardous handling and the complicated maintenance remained the Ta 338’s Achilles heel, and the tactical benefit of VTOL operations could not outbalance these flaws. Furthermore, the Ta 338’s range remained very limited, as well as the potential firepower. Four 20mm or two 30mm cannons were deemed unsatisfactory for an interceptor of this class and power. And while bundles of unguided missiles proved to be very effective against large groups of bombers, it was more efficient to bring these weapons with simple and cheap vehicles like the Bachem Ba 349 Natter VTOL rocket fighter into target range, since these were effectively “one-shot” weapons. Once the Ta 338 fired its weapons it had to retreat unarmed.

 

In mid 1945, in the advent of defeat, further tests of the Ta 338 were stopped. I./EK338 was disbanded in March 1945 and all machines retreated from the Eastern front, while II./EK338 kept defending the Ruhrgebiet industrial complex until the Allied invasion in April 1945. Being circled by Allied forces, it was not possible to evacuate or destroy all remaining Ta 338s, so that at least two more or less intact airframes were captured by the U.S. Army and later brought to the United States for further studies.

  

General characteristics:

Crew: 1

Length/height on the ground: 10.40 m (34 ft 2 in)

Wingspan: 10.50 m (34 ft 5 in)

Fin span: 4:07 m (13 ft 4 in)

Wing area: 18.30 m² (196.99 ft²)

Empty weight: 11,599 lb (5,261 kg)

Loaded weight: 16,221 lb (7,358 kg)

Max. takeoff weight: 16,221 lb (7,358 kg)

 

Powerplant:

1× BMW 803 A-2 28-cylinder, liquid-cooled four-row radial engine,

rated at 4.100 hp (2.950 kW) and at 4.500 hp (3.308 kW) with emergency boost.

4x Schmidding SG 34 solid fuel booster rockets, 4.9 kN (1,100 lbf) thrust each, or

2x 9.8 kN (2,203 lbf) solid fuel booster rockets

 

Performance:

Maximum speed: 860 km/h (534 mph)

Cruise speed: 650 km/h (403 mph)

Range: 750 km (465 ml)

Service ceiling: 43,300 ft (13,100 m)

Rate of climb: 10,820 ft/min (3,300 m/min)

Wing loading: 65.9 lb/ft² (322 kg/m²)

 

Armament:

No internal armament, any weapons were to be mounted on three hardpoints (one under the fuselage for up to 1.000 kg (2.200 lb) and two under the outer wings, 500 kg (1.100 lb) each. Total ordnance was limited to 1.000 kg (2.200 lb).

 

Various armament and equipment sets (Rüstsätze) were tested:

R1 with 4× 20 mm (.79 in) MG 151/20 cannons

R2 with 2x 30 mm (1.18 in) MK 213C cannons

R3 with 48x 73 mm (2.874 in) Henschel Hs 297 Föhn rocket shells

R4 with 66x 55 mm (2.165 in) R4M rocket shells

R5 with a single 1.000 kg (2.200 lb) bomb under the fuselage

R6 with an underfuselage pod with one Rb 20/20 and one Rb 75/30 topographic camera

  

The kit and its assembly:

This purely fictional kitbashing is a hardware tribute to a highly inspiring line drawing of a Fw 190 VTOL tailsitter – actually an idea for an operational RC model! I found the idea, that reminded a lot of the Lockheed XFV-1 ‘Salmon’ prototype, just with Fw 190 components and some adaptations, very sexy, and so I decided on short notice to follow the urge and build a 1:72 version of the so far unnamed concept.

 

What looks simple (“Heh, it’s just a Fw 190 with a different tail, isn’t it?”) turned out to become a major kitbashing. The basis was a simple Hobby Boss Fw 190 D-9, chose because of the longer tail section, and the engine would be changed, anyway. Lots of work followed, though.

 

The wings were sliced off and moved upwards on the flanks. The original tail was cut off, and the cruciform fins are two pairs of MiG-21F stabilizers (from an Academy and Hasegawa kit), outfitted with reversed Mk. 84 bombs as aerodynamic fairings that carry four small wheels (from an 1:144 T-22M bomber) on scratched struts (made from wire).

 

The cockpit was taken OOB, only a pilot figure was cramped into the seat in order to conceal the poor interior detail. The engine is a bash from a Ju 188’s BMW 801 cowling and the original Fw 190 D-9’s annular radiator as well as a part of its Jumo 213 cowling. BMW 801 exhaust stubs were inserted, too, and the propeller comes from a 1:100 VEB Plasticart Tu-20/95 bomber.

 

Since the BMW 803 had liquid cooling, radiators had to go somewhere. The annular radiator would certainly not have been enough, so I used the space in the wings that became available through the deleted Fw 190 landing gear (the wells were closed) for additional radiators in the wings’ leading edges. Again, these were scratched with styrene profiles, putty and some very fine styrene mesh.

 

As ordnance I settled for a pair of gun pods – in this case these are slipper tanks from a Hobby Boss MiG-15, blended into the wings and outfitted with hollow steel needles as barrels.

  

Painting and markings:

Several design options were possible: all NMF with some colorful markings or an overall RLM76 finish with added camouflage. But I definitively went for a semi-finished look, inspired by late WWII Fw 190 fighters.

 

For instance, the wings’ undersides were partly left in bare metal, but the rudders painted in RLM76 while the leading edges became RLM75. This color was also taken on the wings’ upper sides, with RLM82 thinly painted over. The fuselage is standard RLM76, with RLM82 and 83 on the upper side and speckles on the flanks. The engine cowling became NMF, but with a flashy ‘Hartmann Tulpe’ decoration.

 

Further highlights are the red fuselage band (from JG300 in early 1945) and the propeller spinner, which received a red tip and segments in black and white on both moving propeller parts. Large red “X”s were used as individual aircraft code – an unusual Luftwaffe practice but taken over from some Me 262s.

 

After a light black ink wash some panel shading and light weathering (e.g. exhaust soot, leaked oil, leading edges) was done, and the kit sealed under matt acrylic varnish.

  

Building this “thing” on the basis of a line drawing was real fun, even though challenging and more work than expected. I tried to stay close to the drawing, the biggest difference is the tail – the MiG-21 stabilizers were the best option (and what I had at hand as donation parts), maybe four fins from a Hawker Harrier or an LTV A-7 had been “better”, but now the aircraft looks even faster. ;)

Besides, the Ta 338 is so utterly Luft ’46 – I am curious how many people might take this for real or as a Hydra prop from a contemporary Captain America movie…

Full frontal gear porn. :) This is an amateur radio transceiver; it sends and receives various kinds of radio transmissions in the portions of the radio spectrum that we (amateur radio operators) are allowed to use. In addition, it is a very capable receiver for a good portion of the lower RF spectrum; from below AM radio, where airport beacons and submarine transmissions reside, through AM, shortwave, and on up to 50 MHz.

 

Most non-voice radio transmissions use some form of tone encoding; this includes fax, radio-teletype (RTTY), slow scan television, and many more. A simple audio cable from the radio to the audio input of my macbook pro (just off to the right, but not visible), plus the right software, lets me easily decode and display these transmissions. The Internet has taken on the role of sending a great deal of this information, and so interesting transmissions are becoming more difficult to find, but they're still out there, particularly being sent out of the developing countries.

 

The monitor above the radio is plugged into the rectangular unit in between the speaker and the radio; this is the DMU, or "Data Management Unit", a tool that lets you see the RF spectrum directly, as shown here, as well as keep logs, aim your antenna, examine the spectrum of received and transmitted audio, keep various world clocks and other hand radio-related activities. The DMU is a Linux based computer that monitors a special interface card in the radio. The memory card visible in the front of the DMU actually contains the boot software and also my personal settings, such as memory channels, my location, and so forth.

  

Shot info: Canon EOS 50D [modified IR response in Hα range], Canon EF-S 18-55mm ƒ/3.5-5.6 IS zoom [ø58mm] @ 23mm, ƒ/7.1, ISO 100, 1 sec. exposure, mf, manual mode. This is one of those images where none of the camera's semi-auto modes would expose reasonably. Manual mode to the rescue!

Capable of coming to rest on land or water but does neither gracefully...

Port side view.

 

Name: S.S. Bessemer

 

Registration Number: KCC-1894 (Kolter Construction Contract Number 1,894)

  

Affiliation: Kolter Mining, Refining, and Fuel.

 

Class Name: Bessemer class

  

Type: Deep Space Mining Operations Flagship

 

Commissioned: Circa late 2500’s, post recent major conflict

 

Specifications:

  

Length: 1,844 meters (184.4 studs, 58.1 inches, 4.83 feet, 147.5 cm model)

  

Width: 503 meters (50.3 studs, 15.8 inches, 40.2 cm model)

  

Height: 484 meters, 398 meters without dorsal comms array, (48.4 studs, 15.2 inches, 38.7 cm model)

  

Crew: 2,950 standard complement + capacity for crew families, as well as smaller guest quarters for up to 2,000 additional personnel to be moved to/from mining operations.

 

Armament: 1 super-heavy coaxial particle beam cannon, (primarily for asteroid mining, but also more than capable of defensive action,) 4 dual-mounted heavy particle cannon turrets, 8 dual-mounted medium particle cannon turrets, 2 coaxial fore medium particle cannons, 80 quad-mounted 80mm anti-fighter flak railgun turrets.

 

Defensive systems:

Hull: Super-heavy steel alloy hull with carbon nanotube/buckypaper composite layers as spall lining.

Armor plating: steel, titanium alloy, tungsten, ceramic, and carbon nanotube composite armor layers against asteroids/other space debris, kinetic weapons, kinetic spalling, particle, laser, and plasma fire. Thick composite armor provides excellent survivability, but with very high mass. Some battleships are less armored than this ship.

Bulkheads: Extensive titanium bulkhead support network.

Structural integrity field: High power system designed for significant cargo mass placing stress on the frame, or to withstand asteroid impacts to the hull.

Shielding: Internally housed high power adaptive particle field repulsing shielding system capable of surviving significant punishment. Some older battleships have less robust shielding.

 

Powerplant: 1 primary matter-antimatter reactor with extensive fuel reserves, 2 secondary fusion reactors with extensive fuel reserves. Multiple massive power capacitors. Extensive heatinks.

 

Propulsion: 1 massive primary fusion engine for sub-lightspeed travel, 1 internal FTL core capable of moderate FTL speed, long range travel, and 32 large reaction control thrusters for slow but dependable below light speed maneuvering.

 

Computer systems: Single supercomputer core with onboard Virtual Intelligence system.

  

Comms and Sensors: Local and FTL comms arrays. Radar, LIDAR, infrared, multi-spectral, and additional other local area sensors systems, along with extensive FTL sensors.

 

Additional Systems: High power artificial singularity for both artificial gravity generation and inertial dampening, allowing for 1G gravity even when hauling an entire cargo hold full of heavy-metal. 6 massive blast furnaces for refining metal ore, an enormous central cargo hold system, 4 fuel refining tanks, 4 massive fuel storage tanks, and an internal rail system for moving ore and personnel.

 

Embarked Craft: 2 Thunderbird class super-heavy cargo/personnel shuttles, 2 Hurricane class heavy cargo/personnel shuttles, 20 heavy mining drones, 24 medium mining drones, 2 gunships of variable class, 2 heavy fighter/bombers of variable class, potential for multiple additional light shuttles and fighters.

 

Background: After seeing both the devastation to outlying areas of space caused by the recent Great War, and the corruption within the Federal Defense Navy (working title) Admiralty, Captain David Courtland retired honorably from military service and went to helm his family’s generations old mining company, Kolter Mining, Refining, and Fuel; one of the largest mining companies in United Earth Federation space. (Working title.)

 

He wanted to take the company, already a reputable and successful business, in a new direction. That direction was the disputed, war-torn, no-man’s-waste-land of space known as The Divide, (working title) situated between the major powers of the galaxy. Life in The Divide was desperate, with little hope for the many people stranded in the ruins, poverty, and crime infested land. None of the major powers could intervene without starting another territorial war, and as such, pirates, gangs, and unscrupulous mega-corporations ruled supreme.

 

Courtland wanted to make a difference to this sorrowful place, and with trillions of credits and a Fortunes 1,000 company at his control, he had the means to at least begin; although even he lacked the ability to single-handedly remedy the myriad of woes The Divide faced.

 

David’s plan was simple, to move significant mining operations to The Divide, thus:

1: Creating new, safe, well-paying, good jobs for both an area and an industry that seldom offered such things.

2: Allowing for the placement of company security forces to deter pirate activity around major settlements.

3: Providing tax-free revenue to fund new schools, hospitals, food, water, shetler, and other charitable activities in The Divide.

  

But to do it, he required a new kind of mining vessel, as well as additional security forces. Thus he contacted Nelson Heavy Industries, who in turn partnered with AxonTech Interstellar Systems for some components, to place an order for a line of custom massive deep space mining operation flagships with enhanced combat capabilities and capable of operating in the remotest reaches of space for months or even years at a time. And so the Bessemer class was born.

 

The Bessemer class is unlike any mining vessel ever produced before it. Certainly significantly larger mining ships existed, but these were typically little more than unarmed, slow moving things with small engines; closer to a semi-mobile starbase than a combination frontier battleship/mining vessel. But Courtland required something unique. Something that could move faster, survive more punishment, and something that had teeth; not a fragile, barely moving thing that would only sit in safe areas of space. Courtland needed a mighty sheepdog in a world of sheep and wolves.

 

Bessemer class vessels are 1,844 meters long, and possess more armor, firepower, and shielding than many pre Great War battleship designs. Almost any pirate or local gang would be terrified of the sight of over a mile of steel and particle cannons; clad in Kolter white, green, and yellow.

 

But the Bessemer, and others of her class, are not merely warships masquerading as civilian craft. They are heavy mining machines that live up to their name; a steel producing process that revolutionized the industry of Earth some seven hundred years earlier. The Bessemer and her sister ships are capable of blasting metal-rich asteroids to bits with their coaxial mining particle beam cannon, and then having swarms of automated mining drones devour any valuable deposits within before unloading the materials into the Bessemer’s ore hold for the internal rail system to run any raw ore through her six corvette sized forges, and then having the refined metal shunted to her cavernous lower hold, while any waste material from the refining process is vented directly into space.

 

Ships of this class are outfitted with a sizable hangar, advanced sensor suite, extensive internal cargo bays, and large cargo pod clamps that allow it to act in the capacity of miner, defensive ship, operations command center, and even freighter and personnel carrier should usual shipping to outlying mining sites be disrupted.

 

But capable as they are, these are not the spartan mining vessels with unlivable working conditions that some shady companies have been known to operate. These space-faring cities of steel feature robust safety systems, spacious and comfortable crew quarters, multiple restaurants, multiple mess-halls, multiple shops for clothing, food, electronics, and other items, an arcade, multiple gyms with weights, various weight and cardio machines, martial arts areas, gymnastics equipment, along with a walking track, a small bowling alley, an olympic sized swimming pool, a multi-sport stadium, a greenhouse, hydroponics bays, a small stage/concert area, several computer labs, a library, a small movie theater, crew lounges and break areas, a salon/spa, a bar/club, chapels, classroom/daycare areas, office areas, as well as repair stations, enough dry and frozen storage to keep everyone fed for extended missions, advanced workshops, astrotography, laboratories, guest bunk-rooms, and a starbase grade medical center.

 

Not everyone is happy about Kolter Mining’s efforts, however. While Courtland founded the Kolter Foundation to aid those in need, he also lobbied for what came to be known as the Kolter Bill to be passed. Mining employees out in the colonies loved the added protections this afforded them. But the executives of Kolter’s rival mining companies operating out of Earth’s colony worlds quickly found themselves facing laws that favored the profits of Kolter and their already developed safety systems and excellent treatment of employees. What’s more, the Federal Defense Navy Admiralty have been continually frustrated that rather than helping to line their pockets as part of the military industrial complex, Courtland has been working tirelessly to reveal their corruption and hidden support of crime in outlying areas of space.

 

What’s more, there are even rumors that Courtland is now working with, and possibly even helping to fund, a mercenary vigilante unit out in The Divide known as the Phoenix Command Group, founded by Jonathan Scarlett, another former Federal Defense Navy Captain who ran afoul of the Admiralty.

 

The wealthy and corrupt among the Admiralty, military industrial complex, crime syndicates, and corrupt businesses running shady operations out in The Divide are deeply troubled by these rumors. But those who are now citizens of no nation, and who have known nothing but hopelessness and need for years, have a slight spark of hope rising like a Phoenix.

   

IRL info: This digital SHIP was made in Bricklink’s Studio software from September 11th to September 30th, 2021. I did not originally plan to participate in SHIPtember, but I couldn’t resist. It is 184 studs (58.1 inches) long, 50 studs wide, and 48 studs high. It is comprised of 23,470 pieces, which I believe makes it my highest piece-count SHIP to date, and means that the model itself has a mass of 973.502 ounces, or 60.843 pounds, or 27.597 kilograms, which most likely makes it my heaviest SHIP as well as my most piece intensive. (I really need to learn to build a little more hollow.) Note that it uses all real pieces/colors that are available for sale on Bricklink. (Albeit at a price that makes attempting to build it in physical bricks highly impractical.) It is 100% connected, and should be at least somewhat stable in real life. I would want to reinforce the fore-end with more Technic, and switch out the longest Lego Technic axle holding the engine for an aftermarket stainless steel version. I cannot guarantee that various sections built out from the main SNOT and Technic frame would be totally stable without slight redesign of a few bits. It would also require a hefty display stand of some kind.

 

The current pictures are WIP to show the completed status of the build itself. Better renders done by importing the Studio build into Mecabricks, replacing any pieces that fail to load or change position, and then exporting to Blender for higher quality rendering, and finally hopefully doing some cool backgrounds with GIMP, will hopefully follow before whatever October picture deadline is decided on. Please do not use these early pictures in the poster if time remains, as I hope to provide better ones. Thank you for reading this lengthy description. Have a cookie.

 

If this ship had a theme song, this magnificent piece by Clamavi De Profundis would be it: youtu.be/Xm96Cqu4Ils

As sharp looking and capable as this truck is, it doesn't float.

 

SMPD Harbor Officers are highly trained:

 

USLA

(United States Lifeguard Association) Members

SCUBA - Rescue Diver Certified

EMT (Emergency Medical Technician)

Rescue Boat Operator

Marine Firefighter (POST*)

PC 832 (POST* Arrest and Firearms Course)

 

*POST- California Commission on Peace Officer Standards and Training

 

1:64 Greenlight Collectibles

Hot Pursuit Series 22

2015 Chevrolet Silverado LT Hybrid

Santa Monica

Police Department

Harbor Unit

Santa Monica, California

 

Olympus OM-D E-M5 Mark II

Olympus M.14-42mm F3.5-5.6 II R

 

For more info about the dioramas, check out the FAQ: 1stPix FAQ

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

In 1948, a swept wing version of the F-84 was created with the hope of bringing performance to the level of the F-86. The last production F-84E was fitted with a swept tail, a new wing with 38.5 degrees of leading-edge sweep and 3.5 degrees of anhedral, and a J35-A-25 engine producing 5,300 pound-force (23.58 kN) of thrust. The aircraft was designated XF-96A and flew on 3 June 1950. Although the airplane was capable of 602 knots (693 mph, 1,115 km/h), the performance gain over the F-84E was considered minor. Nonetheless, it was ordered into production in July 1950 as the F-84F Thunderstreak. The F-84 designation was eventually retained because the fighter was expected to be a low-cost improvement of the straight-wing Thunderjet with over 55 percent commonality in tooling.

 

In the meantime, the USAF, hoping for improved high-altitude performance from a more powerful engine, arranged for the British Armstrong Siddeley Sapphire turbojet engine to be built in the United States as the Wright J65. To accommodate the larger engine, YF-84Fs with a British-built Sapphire as well as production F-84Fs with the J65 had a vertically stretched fuselage, with the air intake attaining an oval cross-section. Production quickly ran into problems, though. Although tooling commonality with the Thunderjet was supposed to be 55 %, but just 15 % of the tools could actually be re-used. To make matters worse, the F-84F utilized press-forged wing spars and ribs. At the time, only three presses in the United States could manufacture these, and priority was given to the Boeing B-47 Stratojet bomber over the F-84. The YJ65-W-1 engine was considered obsolete, too, and the improved J65-W-3 did not become available until 1954. When the first production F-84F flew on 22 November 1952, it was considered not ready for operational deployment due to control and stability problems. The first 275 aircraft, equipped with conventional stabilizer-elevator tailplanes, suffered from accelerated stall pitch-up and poor turning ability at combat speeds. Beginning with Block 25, the problem was improved upon by the introduction of a hydraulically powered one-piece stabilator. A number of aircraft were also retrofitted with spoilers for improved high-speed control. As a result, the F-84F was not declared operational until 12 May 1954.

 

The second YF-84F prototype was completed with wing-root air intakes. These were not adopted for the fighter due to loss of thrust, but this arrangement kept the nose section free and permitted placement of cameras, and the different design was adopted for the RF-84F Thunderflash reconnaissance version. Being largely identical to the F-84F, the Thunderflash suffered from the same production delays and engine problems, though, delaying operational service until March 1954.

 

During the F-84F’s development the Air Defense Command was looking for a replacement for the outdated F-94 ‘Starfire’ interceptor, a hasty development from the T-33 trainer airframe with an afterburner engine and an on-board radar. However, the F-94 was only armed with machine guns in its early versions or unguided missiles in its later incarnations, which were inadequate. An aircraft with better performance, ideally with supersonic speed, a better radar, and the ability to carry guided missiles (in the form if the AIR-1 and 2 ‘Falcon’ AAMs) as well as the AIR-2 ‘Genie’ missile was now requested.

 

The Douglas AIR-2 Genie followed a unique but effective concept that represented the technological state-of-the-art: it was an unguided air-to-air rocket with a 1.5 kt W25 nuclear warhead. The interception of Soviet strategic bombers was a major military preoccupation of the late 1940s and 1950s. The World War II-age fighter armament of machine guns and cannon were inadequate to stop attacks by massed bomber formations, which were expected to come in at high altitude and at high subsonic speed. Firing large volleys of unguided rockets into bomber formations was not much better, and true air-to-air missiles were in their infancy. In 1954 Douglas Aircraft began a program to investigate the possibility of a nuclear-armed air-to-air weapon. To ensure simplicity and reliability, the weapon would be unguided, since the large blast radius made precise accuracy unnecessary. Full-scale development began in 1955, with test firing of inert warhead rockets commencing in early 1956. The final design carried a 1.5-kiloton W25 nuclear warhead and was powered by a Thiokol SR49-TC-1 solid-fuel rocket engine of 162 kN (36,000 lbf) thrust, sufficient to accelerate the rocket to Mach 3.3 during its two-second burn. Total flight time was about 12 seconds, during which time the rocket covered 10 km (6.2 mi). Targeting, arming, and firing of the weapon were coordinated by the launch aircraft's fire-control system. Detonation was by time-delay fuze, although the fuzing mechanism would not arm the warhead until engine burn-out, to give the launch aircraft sufficient time to turn and escape. However, there was no mechanism for disarming the warhead after launch. Lethal radius of the blast was estimated to be about 300 meters (980 ft). Once fired, the Genie's short flight-time and large blast radius made it virtually impossible for a bomber to avoid destruction. The rocket entered service with the designation MB-1 Genie in 1957.

 

During the development phase the first carrier aircraft earmarked to carry the AIR-2 was the Northrop F-89 Scorpion, which had already been introduced in the early Fifties. While being an all-weather interceptor with on-board radar, it was a slow and large aircraft, and outdated like the F-94. Trying to keep the F-84 production lines busy, however, Republic saw the chance to design an all-weather interceptor aircraft that would surpass the F-89’s mediocre performance and meet the AIR-2 carrier requirements on the basis of the swept-wing (R)F-84F. To emphasize its dedicated interceptor role and set it apart from its fighter-bomber ancestors, the heavily modified aircraft was designated F-96B (even though it had little to do with the XF-96A that became the F-84F) and called ‘Thunderguard’.

 

The F-96B was largely based on the RF-84F’s airframe with its wing-root air intakes, what offered ample space in the aircraft’s nose for a radar system and other equipment. The radar was coupled with a state-of-the-art Hughes MC-10 fire control system. To relieve the pilot from operating the radar system one of the fuel cells behind the cockpit was deleted and a second crew member was placed behind him under an extended, strutless hood that opened to starboard. To compensate for the loss of fuel and maintain the F-84F’s range, a new tank was mounted under the cockpit floor in the aircraft’s center of gravity.

To improve performance and cope with the raised take-off weight, the F-96B was powered by an uprated Wright J65-W-18 turbojet, which generated 0.4 kN more dry thrust than the F-84F’s original J65-W-3 (7,700 lbf/34 kN). This was not too much, though, so that the J65 was additionally outfitted with an afterburner. With this upgrade the powerplant provided a maximum thrust of 10,500 lbf (47 kN), what resulted in a markedly improved rate of climb and the ability to break the sound barrier in level flight. The additional reheat section necessitated a wider and longer rear fuselage, which had to be redesigned. As an unintended side benefit, this new tail section reduced overall drag due to a slightly area-ruled coke-bottle shape behind the wings’ trailing edge, which was even emphasized through the ventral brake parachute fairing.

Armament consisted only of missiles, which were all carried externally on wing stations, all guns of the former F-84 versions were deleted to save weight. The F-96B’s weapons range included GAR-1/2/3/4 (Later re-designated as AIM-4) radar- and IR-guided Falcon air-to-air missiles and a pair of MB-1 Genie missiles. Up to four pods with nineteen unguided 2.75 in (70 mm) "Mighty Mouse" Mk 4/Mk 40 Folding-Fin Aerial Rockets each were an alternative, too, and a pair of drop tanks were typically carried under the inner wings to provide the aircraft with sufficient range, since the new afterburner significantly increased fuel consumption.

 

Even though it was only a derivative design, the F-96B introduced a lot of innovations. One of these was the use of a diverertless supersonic inlet (DSI), a novel type of jet engine air intake to control air flow into their engines. Initial research into the DSI was done by Antonio Ferri in the 1950s. It consisted of a "bump" and a forward-swept inlet cowl, which worked together to divert boundary layer airflow away from the aircraft's engine. In the case of the F-96B this was realized as an inward-turning inlet with a variable contraction ratio. However, even though they had not been deemed necessary to guarantee a clean airflow, the F-96B’s air intakes were further modified with splitter plates to adapt them to the expected higher flight speeds and direct the air flow. The initial flight tests had also revealed a directional instability at high speed, due to the longer nose, so that the tail surfaces (both fin and stabilizers) were enlarged for the serial aircraft to compensate.

 

Another novel feature was an IRST sensor in front of the windscreen which augmented the on-board radar. This sensor, developed by Hughes International and designated ‘X-1’, was still very experimental, though, highly unreliable, and difficult to handle, because it relied on pressurized coolant to keep the sensor cold enough to operate properly, and dosing it at a consistent level proved to be difficult (if not impossible). On the other side the IRST allowed to track targets even in a massively radar-jammed environment. The 7” diameter silicone sensor was, together with the on-board radar, slaved to the fire control system so that its input could be used to lock guided missiles onto targets, primarily the GAR-1 and GAR-2 AAMs. The X-1 had a field of view of 70×140°, with an angular resolution of 1°, and operated in 2.5 micron wavelength range. When it worked properly the sensor was able to detect a B-47-sized aircraft’s tails aspect from 25 nm (29 ml/46 km) and a target of similar size from directly ahead from 10 nm (12 ml/19 km). Later, better developed versions of Hughes IRST, like the X-3 that was retrofitted to the F-101B in the early Sixties, had a better range and were more reliable.

 

During the Thunderguard’s development another competitor entered the stage, the F-101B Voodoo. In the late 1940s, the Air Force had already started a research project into the future interceptor aircraft that eventually settled on an advanced specification known as the 1954 interceptor. Contracts for this specification eventually resulted in the selection of the F-102 Delta Dagger, but by 1952 it was becoming clear that none of the parts of the specification other than the airframe would be ready by 1954; the engines, weapons, and fire control systems were all going to take too long to get into service. An effort was then started to quickly produce an interim supersonic design to replace the various subsonic interceptors then in service, and the F-101 airframe was selected as a starting point. Although McDonnell proposed the designation F-109 for the new aircraft (which was to be a substantial departure from the basic Voodoo fighter bomber), the USAF assigned the designation F-101B. Its development was protracted, so that the F-96B – even though it offered less performance – was ordered into production to fill the USAF’s urgent interceptor gap.

 

F-96B production started after a brief test phase in late 1957, and the first aircraft were delivered to the 60th Fighter-Interceptor Squadron in 1958. However, when it became clear that the F-101B would finally enter service in 1959, F-96B production was quickly cut down and the initial order of 300 aircraft reduced to only 150, which were produced until early 1960 in three batches. Only sixty were directly delivered to ADC units, because these were preferably equipped with the supersonic F-102A and the new F-101B, which could also carry the nuclear Genie missile. The rest was directly handed over to Air National Guard units – and even there they were quickly joined and replaced by the early ADC aircraft.

 

Operationally, almost all F-96Bs functioned under the US–Canadian North American Air Defense Command (NORAD), which protected North American airspace from Soviet intruders, particularly the threat posed by nuclear-armed bombers. In service, the F-96Bs were soon upgraded with a data link to the Semi-Automatic Ground Environment (SAGE) system, allowing ground controllers to steer the aircraft towards its targets by making adjustments through the plane's autopilot. Furthermore, the F-96B was upgraded to allow the carrying of two GAR-11/AIM-26 Nuclear Falcon missiles instead of the Genies when they became available in 1961.

A handful F-96Bs were camouflaged during the late Sixties with the USAF’s new SEA scheme, but most aircraft retained their original bare metal finish with more or less colorful unit markings. Due to its limited capabilities and the introduction of the Mach 2 McDonnell F-4 Phantom, the last F-96B was retired from ANG service in 1971.

  

General characteristics:

Crew: 2

Length: 54t 11 1/2 in (16,77 m) incl. pitot

Wingspan: 33 ft 7.25 in (10,25 m)

Height: 16 ft 9 in (5,11 m)

Wing area: 350 sq ft (37,55 m²)

Empty weight: 13,810 lb (6.264 kg)

Gross weight: 21,035 lb (9.541 kg)

Max takeoff weight: 28,000 lb (12.701 kg)

 

Powerplant:

1× Wright J65-W-18 turbojet with 8,600 lbf (34 kN) dry thrust and 10,500 lbf (47 kN) with afterburner

 

Performance:

Maximum speed: 695 mph (1,119 km/h, 604 kn, Mach 1.1) at 35,000 ft (10,668 m)

Cruise speed: 577 mph (928 km/h, 501 kn)

Range: 810 mi (1,304 km, 704 nmi) combat radius with two droptanks

Service ceiling: 49,000 ft (15,000 m)

Rate of climb: 16,300 ft/min (83 m/s)

Wing loading: 86 lb/sq ft (423 kg/m²)

 

Armament:

No internal guns;

6× underwing hardpoints for a total ordnance load of up to 6,000lb (2,727 kg), including

a pair of 191.5 US gal (727 l) or 375 US gal (1.429 l) drop tanks on the inner stations

and a mix of AIM-4 Falcon (up to six), MB-1 Genie (up to two) and/or pods with

nineteen 2.75”/70 mm FFAR unguided missiles each (up to four) on the outer stations

  

The kit and its assembly:

This fictional missing link between the RF-84F and the F-105 was conceived for the Fifties Group Build at whatifmodellers.com, an era when the USAF used a wide variety of interceptor aircraft types and technical advancements were quick and significant – in just a decade the interceptor evolved from a subsonic machine gun-toting aircraft to a guided weapons carrier platform, capable of Mach 2.

 

The F-96B (I re-used Republic’s dropped designation for the swept-wing F-84F) was to display one of the many “in between” designs, and the (R)F-84F was just a suitable basis for a conversion similar to the T-33-derived F-94, just more capable and big enough to carry the nuclear Genie missile.

The basis became Italeri’s vintage RF-84F kit, a rather simple affair with raised panel lines and a mediocre fit, plus some sinkholes. This was, however, heavily modified!

 

Work started with the implantation of a new tandem cockpit, taken wholesale from a Heller T-33. Fitting the cockpit tub into the wider Thunderflash hull was a bit tricky, putty blobs held the implant in place. The canopy was taken from the T-33, too, just the RF-84F’s original rear side windows were cut away to offer sufficient length for the longer clear part and the cockpit side walls had to be raised to an even level with the smaller windscreen with the help of styrene strips. With these adapters the T-33 canopy fitted surprisingly well over the opening and blended well into the spine.

 

The camera nose section lost its tip, which was replaced with the tail cone from a Matchbox H.S. Buccaneer (actually its air brake), and the camera windows as well as the slant surfaces that held them were PSRed away for a conical shape that extended the new pointed radome. Lots of weight in the nose and under the cockpit floor ensured a safe stance on the OOB landing gear.

The rear section behind the air brakes became all-new; for an afterburner I extended and widened the tail section and implanted the rear part from a B-66 (Italeri kit, too) engine nacelle, which received a wider nozzle (left over from a Nakotne MiG-29, a featureless thing) and an interior.

To balance the longer nose I also decided to enlarge the tail surfaces and replaced the OOB fin and stabilizers with leftover parts from a Trumpeter Il-28 bomber – the fin was shortened and the stabilizers reduced in span to match the rest of the aircraft. Despite the exotic source the parts blend well into the F-84’s overall design!

 

To add supersonic credibility and to connect the design further with the later F-105 I modified the air intakes and cut them into a raked shape – quite easy to realize. Once the wings were in place, I also added small splitter plates, left over from an Airfix BAC Strikemaster.

 

As an interceptor the armament had to be adapted accordingly, and I procured the quartet of IR-guided Falcons as well as the Genie duo from an Academy F-89. The large drop tanks were taken OOB from the Italeri kit. The Genies were mounted onto their massive Scorpion pylons under the outer wings of the F-96B, while the Falcons, due to relatively little space left under the wings, required a scratched solution. I eventually settled for dual launchers on small pylons, mounted in front of the landing gear wells. The pylons originally belong to an ESCI Ka-34 “Hokum” helicopter kit (they were just short enough!), the launch rails are a halved pair of F-4 Sidewinder rails from a Hasegawa air-to-air weapons set. With everything on place the F-96B looks quite crowded.

  

Painting and markings:

The machine would represent a late Fifties USAF type, so that the paint options were rather limited if I wanted to be authentic. ADC Grey was introduced in the early Sixties, SEA camouflage even later, so that bare metal became a natural choice – but this can be quite attractive! The model received an overall coat with acrylic “White Aluminum” from the rattle can, plus some darked panels all over the hull (Humbrol 56 for good contrast) and an afterburner section in Revell 91 (Iron Metallic) and Humbrol’s Steel Metallizer. The radome became deep black, the anti-glare panel in front of the windscreen olive drab (Revell 46). Light grey (Revell 75) was used for some small di-electric fairings.

Interior surfaces (cockpit and landing gear wells) were painted with Zinc Chromate primer (I used Humbrol 80), while the landing gear struts became silver-grey (Humbrol 56) and the inside of the covers as well as the air brakes were painted in bright red (Humbrol 19).

Once basic painting was done the model received a black ink washing and was rubbed with grinded graphite to emphasize the raised panel lines, and the material adds a nice dark metallic shine to the silver base coat.

 

Another challenge was to find suitable unit markings for the Fifties era in the decal vault, which would also fit onto the model. After a long search I eventually settled for rather simple markings from a 325th FIS F-102 from an Xtradecal sheet, which only features a rather timid fin decoration.

Finding other suitable standard markings remained demanding, though. Stars-And-Bars as well as the USAF taglines were taken from the Academy F-89 that also provided the ordnance, most stencils were taken from the OOB Italeri sheet and complemented by small markings from the scrap box. The biggest problem was the creation of a matching serial number. The “FF” code was originally used for P/F-51D Mustangs during the Korea War, but after the type had been phased out it might have been re-used? The letters as well as the serial number digits were created from various markings for USAF F-100s, also from an Xtradecal sheet.

 

Once the decals had been applied the model was sealed with semi-gloss acrylic varnish, except for the radome, the anti-glare panel as well as the walking areas on the wings as well as parts of the afterburner section, which were coated with matt varnish.

  

A rather straightforward conversion, even though finishing the project took longer than expected. But the result looks surprisingly natural and plausible. Lots of PSR was needed to modify the fuselage, though, especially the tail section was not easy to integrate into the Thunderflash’s hull. Sticking to the simple NMF livery paid IMHO out, too: the livery looks very natural and believable on the fictional aircraft, and it suits the F-84’s bulbous shape well.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

The Saab JAS 39 Gripen (griffin) is a light single-engine multirole fighter aircraft manufactured by the Swedish aerospace company Saab. In 1979, the Swedish government began development studies for an aircraft capable of fighter, attack and reconnaissance missions to replace the Saab 35 Draken and 37 Viggen. The preferred aircraft was a single-engine, lightweight single-seater, embracing fly-by-wire technology, canards, and an aerodynamically unstable design. The powerplant selected was the Volvo-Flygmotor RM12, a license-built derivative of the General Electric F404−400; engine development priorities were weight reduction and lowering component count. A new design from Saab was selected and developed as the JAS 39, first flying in 1988.

 

The Gripen is a multirole fighter aircraft, intended as a lightweight and agile aerial platform with advanced, highly adaptable avionics. It has canard control surfaces that contribute a positive lift force at all speeds, while the generous lift from the delta wing compensates for the rear stabilizer producing negative lift at high speeds, increasing induced drag. It is capable of flying at a 70–80 degrees angle of attack.

Being intentionally unstable and employing digital fly-by-wire flight controls to maintain stability removes many flight restrictions, improves manoeuvrability and reduces drag. The Gripen also has good short takeoff performance, being able to maintain a high sink rate and strengthened to withstand the stresses of short landings. A pair of air brakes are located on the sides of the rear fuselage; the canards also angle downward to act as air brakes and decrease landing distance

 

To enable the Gripen to have a long service life, roughly 50 years, Saab designed it to have low maintenance requirements. Major systems such as the RM12 engine and PS-05/A radar are modular to reduce operating cost and increase reliability. The Gripen’s systems were designed to be flexible, so that newly developed sensors, computers and armaments could be easily integrated as technology advances. The aircraft was estimated to be roughly 67% sourced from Swedish or European suppliers and 33% from the US.

To market the aircraft internationally, Saab formed partnerships and collaborative efforts with overseas aerospace companies. One example of such efforts was Gripen International, a joint partnership between Saab and BAE Systems formed in 2001. Gripen International was responsible for marketing the aircraft, and was heavily involved in the successful export of the type to South Africa; the organisation was later dissolved amidst allegations of bribery being employed to secure foreign interest and sales. On the export market, the Gripen has achieved moderate success in sales to nations in Central Europe, South Africa and Southeast Asia.

 

The Swedish Air Force placed a total order for 204 Gripens in three batches. The first delivery of the JAS 39A/B (single seat and two seat variants) occurred on 8 June 1993, when aircraft “39102” was handed over to the Flygvapnet during a ceremony at Linköping. The final Batch three 1st generation aircraft was delivered to FMV on 26 November 2008, but in the meantime an upgraded Gripen variant, the JAS 39C/D already rolled off of the production lines and made the initial versions obsolete. The JAS C/D gradually replaced the A/B versions in the frontline units until 2012, which were then offered for export, mothballed or used for spares for the updated Swedish Gripen fleet.

 

A late European export customer became the nascent Republic of Scotland. According to a White Paper published by the Scottish National Party (SNP) in 2013, an independent Scotland would have an air force equipped with up to 16 air defense aircraft, six tactical transports, utility rotorcraft and maritime patrol aircraft, and be capable of “contributing excellent conventional capabilities” to NATO. Outlining its ambition to establish an air force with an eventual 2,000 uniformed personnel and 300 reservists, the SNP stated that the organization would initially be equipped with “a minimum of 12 interceptors in the Eurofighter/Typhoon class, based at Lossiemouth, a tactical air transport squadron, including around six Lockheed Martin C-130J Hercules, and a helicopter squadron for transport and SAR duties”.

 

According to the document, “Key elements of air forces in place at independence, equipped initially from a negotiated share of current UK assets, will secure core tasks, principally the ability to police Scotland’s airspace, within NATO.” An in-country air command and control capability would be established within five years of a decision in favor of independence, it continued, with staff also to be “embedded within NATO structures”.

This plan was immediately set into action with the foundation of the Poblachd na h-Alba Adhair an Airm (Republic of Scotland Air Corps/RoScAC) after the country's independence from Great Britain in late 2017. For the fighter role, Scotland was offered refurbished F-16C and Ds from the USA, but this was declined, as the type was considered too costly and complex. An offer from Austria to buy the country’s small Eurofighter fleet (even at a symbolic price) was rejected for the same reason.

Eventually, and in order to build a certain aura of neutrality, Scotland’s young and small air arm initially received twelve refurbished, NATO-compatible Saab JAS 39 Gripen (ten single-seater and two two-seaters) as well as Sk 90 trainers from Swedish overstock. These second hand machines were just the initial step in the mid-term procurement plan, though.

 

Even though all Scottish Gripens (locally called “Grìbhean”, designated F.1 for the JAS 39A single seaters and F.2 for the fully combat-capable JAS 39B two-seaters, respectively) were multi-role aircraft and capable of strike missions, its primary roles were interception/air defense and, to a lesser degree, reconnaissance. Due to severe budget restrictions and time pressure, these aircraft were almost identical to the Flygvapnet’s JAS 39A/B aircraft. They used the PS-05/A pulse-Doppler X band multi-mode radar, developed by Ericsson and GEC-Marconi, which was based on the latter's advanced Blue Vixen radar for the Sea Harrier that also served as the basis for the Eurofighter's CAPTOR radar. This all-weather radar is capable of locating and identifying targets 120 km (74 mi) away and automatically tracking multiple targets in the upper and lower spheres, on the ground and sea or in the air. It can guide several beyond visual range air-to-air missiles to multiple targets simultaneously. Therefore, RoScAC also procured AIM-9 Sidewinder and AIM-120 AMRAAM as primary armament for its Grìbhean fleet, plus AGM-65 Maverick air-to-ground missiles.

 

The twelve Grìbhean F.1 and F.2s formed the RoScAC’s 1st fighter (Sabaid) squadron, based at former RAF base Lossiemouth. Upon delivery and during their first months of service, the machines retained the former Swedish grey paint scheme, just with new tactical markings. In 2018, the RoScAC fighter fleet was supplemented with brand new KAI/Lockheed Martin TA-50 ‘Golden Eagle’ armed trainers from South Korea, which could also take over interceptor and air patrol duties. This expansion of resources allowed the RoScAC to initiate an update program for the JAS 39 fleet. It started in 2019 and included in-flight refueling through a fixed but detachable probe, a EuroFIRST PIRATE IRST, enhanced avionics with elements from the Swedish JAS 39C/D, and a tactical datalink.

With these updates, the machines could now also be externally fitted with Rafael's Sky Shield or LIG Nex1's ALQ-200K ECM pods, Sniper or LITENING targeting pods, and Condor 2 reconnaissance pods to further improve the machine’s electronic warfare, reconnaissance, and targeting capabilities.

The aircraft’s designations did not change, though, the only visible external change were the additional IRST fairing under the nose, and the machines received a new tactical camouflage with dark green and dark grey upper surfaces, originally introduced with the RoScAC’s TA-50s. However, all Grìbhean F.1 single seaters received individual fin designs instead of the grey camouflage, comprising simple red and yellow fins, the Scottish flag (instead of the standard fin flash) and even a large pink thistle on a white background and a white unicorn on a black background.

 

Despite being 2nd hand aircraft, the Scottish JAS 39A and Bs are expected to remain in service until at least 2035.

  

General characteristics:

Crew: one

Length: 14.1 m (46 ft 3 in)

Wingspan: 8.4 m (27 ft 7 in)

Height: 4.5 m (14 ft 9 in)

Wing area: 30 m2 (320 sq ft)

Empty weight: 6,800 kg (14,991 lb)

Max takeoff weight: 14,000 kg (30,865 lb)

 

Powerplant:

1× Volvo RM12 afterburning turbofan engine,

54 kN (12,000 lbf) dry thrust, 80.5 kN (18,100 lbf) with afterburner

 

Performance:

Maximum speed: 2,460 km/h (1,530 mph, 1,330 kn)/Mach 2

Combat range: 800 km (500 mi, 430 nmi)

Ferry range: 3,200 km (2,000 mi, 1,700 nmi)

Service ceiling: 15,240 m (50,000 ft)

g limits: +9/-3

Wing loading: 283 kg/m2 (58 lb/sq ft)

Thrust/weight: 0.97

Takeoff distance: 500 m (1,640 ft)

Landing distance: 600 m (1,969 ft)

 

Armament:

1× 27 mm Mauser BK-27 revolver cannon with 120 rounds

8 hardpoints (Two under the fuselage, one of them dedicated to FLIR / ECM / LD / Recon pods plus

two under and one on the tip of each wing) with a capacity of 5 300 kg (11 700 lb)

  

The kit and its assembly:

Nothing spectacular – actually, this build is almost OOB and rather a livery what-if model. However, I had the plan to build a (fictional) Scottish Gripen on my agenda for some years now, since I started to build RoScAC models, and the “Back into service” group build at whatifmodlers.com in late 2019 was a good motivation to tackle this project.

 

The starting point was the Italeri JAS 39A kit, a rather simple affair that goes together well but needs some PSR on almost every seam. Not much was changed, since the model would depict a slightly updated Gripen A – the only changes I made were the additional IRST fairing under the nose, the ejection handle on the seat and a modified ordnance which consists of a pair of AIM-9L and AIM-120 (the latter including appropriate launch rails) from a Hasegawa air-to-air weapons set. The ventral drop tank is OOB.

  

Painting and markings:

The motivation a behind was actually the desire to build a Gripen in a different livery than the usual and rather dull grey-in-grey scheme. Therefore I invented a tactical paint scheme for “my” RoScAC, which is a modified RAF scheme from the Seventies with uppers surfaces in Dark Green (Humbrol 163) and Dark Sea Grey (164), medium grey flanks, pylons, drop tank and a (theoretically) grey fin (167 Barley Grey, today better known as Camouflage Grey) plus undersides in Light Aircraft Grey (166), with a relatively high and wavy waterline, so that a side or lower view would rather blend with the sky than the ground below. The scheme was designed as a compromise between air superiority and landscape camouflage and somewhat inspired by the many experimental schemes tested by the German Luftwaffe in the early Eighties. The Scottish TA-50 I built some years ago was the overall benchmark, but due to the Gripen’s highly blended fuselage/wing intersections, I just painted the flanks under the cockpit and the air intakes as well as a short portion of the tail section in Barley Grey. That’s overall darker than intended (esp. in combination with the fin decoration, see below), but anything grey above the wings would have looked awkward.

 

As a reminiscence of the late British F-4 Phantoms, which carried a grey low-viz scheme with bright fins as quick ID markings, I added such a detail to the Gripen, too – in this case in the form of a stylized Scottish flag on the fin, with some mild 3D effect. The shadow and light effects were created through wet-in-wet painting of lighter and darker shades into the basic blue (using Humbrol 25, 104 and ModelMaster French Blue). Later, the white cross was added with simple decal stripes, onto which similar light effects were added with white and light grey, too.

  

Even though this one looks similar to my Scottish TA-50, which was the first model to carry this paint scheme, I like the very different look of this Gripen through its non-all-grey paint scheme. It’s also my final build of my initial RoScAC ideas, even though I am now considering a helicopter model (an SAR SA 365 Dauphin, maybe?) in fictional Scottish markings, too.

Some background:

The Rolls-Royce Griffon engine was designed in answer to Royal Navy specifications for an engine capable of generating good power at low altitudes. Concepts for adapting the Spitfire to take the new engine had begun as far back as October 1939; Joseph Smith felt that "The good big 'un will eventually beat the good little 'un." and Ernest Hives of Rolls-Royce thought that the Griffon would be "a second power string for the Spitfire". The first of the Griffon-engined Spitfires flew on 27 November 1941. Although the Griffon-powered Spitfires were never produced in the large numbers of the Merlin-engined variants they were an important part of the Spitfire family, and in their later versions kept the Spitfire at the forefront of piston-engined fighter development. The first Griffon-powered Spitfires suffered from poor high- altitude performance due to having only a single stage supercharged engine. By 1943, Rolls-Royce engineers had developed a new Griffon engine, the 61 series, with a two-stage supercharger. In the end it was a slightly modified engine, the 65 series, which was used in the Mk. XIV, the first Spitfire mark with a Griffon engine to enter service. The resulting aircraft provided a substantial performance increase over the Mk IX. Although initially based on the Mk VIII airframe, common improvements made in aircraft produced later included the cut-back fuselage and tear-drop canopies, and the E-Type wing with improved armament.

 

The Mk. XIV differed from its direct predecessor, the Mk XII, in that the longer, two-stage supercharged Griffon 65, producing 2,050 hp (1,528 kW), was mounted 10 inches (25.4 cm) further forward. The top section of the engine bulkhead was angled forward, creating a distinctive change of angle to the upper cowling's rear edge. A new five-bladed Rotol propeller of 10 ft 5 in (3.18 m) in diameter was used. The "fishtail" design of ejector exhaust stub gave way to ones of circular section. The increased cooling requirements of the Griffon engine meant that all radiators were much bigger, and the underwing housings were deeper than previous versions. The cowling fasteners were new, flush fitting "Amal" type and there were more of them. The oil tank (which had been moved from the lower cowling location of the Merlin engine variants to forward of the fuselage fuel tanks) was increased in capacity from 6 to 10 gal.

To help balance the new engine, the radio equipment was moved further back in the rear fuselage and the access hatch was moved from the left fuselage side to the right. Better VHF radio equipment allowed for the aerial mast to be removed and replaced by a "whip" aerial further aft on the fuselage spine. Because the longer nose and the increased slipstream of the big five-bladed propeller a new tail unit with a taller, broader fin and a rudder of increased area was adopted.

 

When the new fighter entered service with 610 Squadron in December 1943 it was a leap forward in the evolution of the Spitfire. The Mk. XIV could climb to 20,000 ft (6,100 m) in just over five minutes and its top speed, which was achieved at 25,400 ft (7,700 m), was 446 mph (718 km/h). In operational service many pilots initially found that the new fighter could be difficult to handle, particularly if they were used to earlier Spitfire marks. But in spite of the difficulties, pilots appreciated the performance increases.

 

F Mk. XIVs had a total of 109.5 gal of fuel consisting of 84 gal in two main tanks and a 12.5 imp gal fuel tank in each leading-edge wing tank; other 30, 45, 50 or 90 gal drop tanks could be carried. The fighter's maximum range was just a little over 460 miles (740 km) on internal fuel, since the new Griffon engine consumed much more fuel per hour than the original Merlin engine of earlier variants. By late 1944, Spitfire XIVs were fitted with an extra 33 gal in a rear fuselage fuel tank, extending the fighter's range to about 850 miles (1,370 km) on internal fuel and a 90 gal drop tank. Mk. XIVs with "tear-drop" canopies had 64 gal. As a result, F and FR Mk. XIVs had a range that was increased to over 610 miles (980 km), or 960 miles (1,540 km) with a 90 gal drop tank. The armament initially consisted of two 20 mm Hispano cannon and four light 0.303” machine guns (in a standard “C” wing configuration), but later builds had the latter replaced with a pair of heavier 0.5” machine guns that had better range and weight of fire (“E” wing configuration).

 

The first test of the aircraft was in intercepting V1 flying bombs and the Mk. XIV was the most successful of all Spitfire marks in this role. When 150 octane fuel was introduced in mid-1944 the "boost" of the Griffon engine was able to be increased to +25 lbs (80.7"), allowing the top speed to be increased by about 30 mph (26 kn; 48 km/h) to 400 mph (350 kn; 640 km/h) at 2,000 ft (610 m).

The Mk. XIV was used by the 2nd Tactical Air Force as their main high-altitude air superiority fighter in northern Europe with six squadrons operational by December 1944.

 

One problem which did arise in service was localized skin wrinkling on the wings and fuselage at load attachment points; although Supermarine advised that the Mk. XIVs had not been seriously weakened, nor were they on the point of failure, the RAF issued instructions in early 1945 that all F and FR Mk. XIVs were to be refitted with clipped wings. Spitfire XIVs began to arrive in the South-East Asian Theatre in June 1945, too late to operate against the Japanese. In total, 957 Mk. XIVs were built, over 430 of which were FR Mk. XIVs.

 

After the war, secondhand Mk. XIVs still in good shape were exported to a number of foreign air forces; 132 went to the Royal Belgian Air Force, 70 went to the Royal Indian Air Force and 30 of the reconnaissance version went to the Royal Thai Air Force. The Royal Iraqi Air Force (RIrAF) was another operator, even though only a small one.

In late 1946, five years after the Anglo-Iraqi War had left the RIrAF shattered, the Iraqis reached an agreement with the British under which they would return their surviving Avro Ansons in exchange for the authorization to order more modern and potent fighter aircraft from the UK, namely Supermarine Spitfires and Hawker Furies. The next year, three de Havilland Doves and three Bristol Freighters were ordered, too, and they arrived in early 1947 with a batch of ten refurbished ex-RAF Spitfire F Mk. XIVcs, some of them WWII survivors. All these machines received the original wing tips to better cope with the expected higher ambient temperatures in the Middle Eastern theatre of operations, reinforced aluminum skinning along the wing roots, and they were retrofitted with hardpoints under the wings and the fuselage to carry unguided missiles, bombs and drop tanks, what gave them an additional ground attack capability. The radio equipment was modernized, too, including a DF loop antenna as navigational aid. Despite these standardizations, though, the Spitfires were delivered with a mix of the different canopies.

 

The RIrAF was still recovering and re-structuring its assets when it joined in the war against the newly created state of Israel in the 1948 Arab-Israeli War. The RIrAF only played a small role in the first war against Israel, though. A few Spitfire F Mk. XIVs as well as Avro Anson training bombers operated from Transjordan airfields from where they flew several attacks against the Israelis. After a series of indiscriminate attacks on Arab capitals, flown by three Boeing B-17s that had been pressed into service by the Israeli Air Force, the governments of Transjordan and Syria demanded that the Iraqis take more offensive action and replace their Ansons with Hawker Furies. However, only six Furies were sent to Damascus to join the Spitfires in the region, and they never encountered any Israeli aircraft during their deployment.

Despite some effective attacks on ground targets by the Spitfires, limited amount of cannon ammunition, RPGs and suitable bombs heavily limited the Iraqi operations. The fighters were mostly used for armed reconnaissance, and three Spitfires were upgraded to FR Mk. XIV standard for this purpose. In 1949 a second batch of eight more Spitfire F Mk. XIVs was delivered from Britain, and in 1951 the RIrAF purchased 20 more Fury F.Mk.1s, for a total of 50 F.Mk.1s single-seaters and 2 two-seaters. They soon replaced the Spitfires in frontline units, even though the machines were still kept in service.

 

In the early Fifties, thanks to increased income from oil and agricultural exports, the RIrAF was thoroughly re-equipped. In 1951, 15 each of de Havilland Canada DHC-1 Chipmunks, Percival Provosts and North American T-6s were bought to replace obsolete de Havilland Tiger Moth trainers. With these new aircraft the RIrAF Flying School was expanded into the Air Force College. The training curriculum was improved, and the number of students graduating each year was increased. This allowed to form a solid basis for the RIrAF's long-term growth. Also in 1951, the RIrAF bought its first helicopters: three Westland Dragonflies. The RIrAF's first jet fighter was the de Havilland Vampire: 12 FB.Mk.52 fighters and 10 T.Mk.55 trainers were delivered from 1953 to 1955, and they fully replaced the Spitfires. The Vampires were quickly supplemented by 20 de Havilland Venoms, delivered between 1954 and 1956.

Following the formation of the Baghdad Pact, the United States donated at least six Stinson L-5 Sentinels and seven Cessna O-1 Bird Dogs to the RIrAF. The RAF also vacated Shaibah Air Base, and the RIrAF took over it as Wahda Air Base. In 1957, six Hawker Hunter F.Mk.6s were delivered. The next year, the United States agreed to provide 36 F-86F Sabres free of charge.

 

However, following the 14 July Revolution of 1958, which resulted in the end of monarchy in Iraq, the influence of the Iraqi Communist Party grew significantly. The first commander of the Iraqi Air Force (the "Royal" prefix was dropped after the revolution), Jalal Jaffar al-Awqati, was an outspoken communist, and encouraged prime minister Abd al-Karim Qasim to improve relations between Iraq and the USSR. The Soviets reacted quickly, and in the autumn of 1958 a series of arms contracts was passed between Iraq and the Soviet Union and Czechoslovakia. These stipulated the delivery of MiG-15UTI trainers, MiG-17F fighters, Ilyushin Il-28 bombers, and Antonov An-2 and An-12 transports. The first aircraft arrived in Iraq in January 1959; during the late Sixties and the early Seventies additional MiG-17s may have been purchased and then forwarded to either Syria or Egypt.

 

General characteristics

Crew: 1

Length: 32 ft 8 in (9.96 m)

Wingspan: 36 ft 10 in (11.23 m) with full span elliptical tips

Height: 10 ft 0 in (3.05 m)

Wing area: 242.1 sq ft (22.49 m²)

Airfoil: NACA 2213 (root), NACA 2209.4 (tip)

Empty weight: 6,578 lb (2,984 kg)

Gross weight: 7,923 lb (3,594 kg)

Max. takeoff weight: 8,400[53] lb (3,810 kg)

 

Powerplant:

1× Rolls-Royce Griffon 65 supercharged V12, 2,050 hp (1,530 kW) at 8,000 ft (2,438 m),

driving a 5-bladed Jablo-Rotol propeller

 

Performance:

Maximum speed: 441 mph (710 km/h, 383 kn) in FS supercharger gear at 29,500 ft.

391 mph in MS supercharger gear at 5,500 ft.

Combat range: 460 mi (740 km, 400 nmi)

Ferry range: 1,090 mi (1,760 km, 950 nmi)

Service ceiling: 43,500 ft (13,300 m)

Rate of climb: 5,040 ft/min (25.6 m/s) in MS supercharger gear at 2,100 ft.

3,550 ft/min in FS supercharger gear at 22,100 ft.

Time to altitude: 7 mins to 22,000 ft (at max weight)

Wing loading: 32.72 lb/sq ft (159.8 kg/m²)

Power/mass: 0.24

 

Armament:

2× 20 mm (0.787-in) Hispano Mk II cannon, 120 rpg

4× 0.303 in (7.7 mm) Browning machine guns, 350 rpg,

Underwing hard points for 8× 60 lb (27 kg) rockets, 2 x 250 lb (113 kg) bombs or slipper tanks,

1× ventral hardpoint for a 500 lb (227 kg) bomb or a drop tank

  

The kit and its assembly:

This was a rather spontaneous interim build. The Academy Spitfire was left over from a D-Day combo that contained a Hawker Typhoon, too, and I lacked an idea for the Spitfire for a long time) since I am not a big fan of the aircraft, at least what-if-inspiration-wise). However, when pondering about a potential operator from the very early pos-war period I remembered the Royal Iraqi Air Force and its later Hawker Hunters which retained their NATO-style camouflage (RAF green/grey) despite being primarily operated in a desert environment. This, on a Spitfire…?

 

From this idea the Academy Spitfire was built almost OOB. Because the kit offers them as an option and for the cool look, I gave the Spitfire four RPGs under each outer wing. The ventral drop tank was taken from a Special Hobby late Spitfire kit. The only other additions are the antenna mast and the non-standard DF loop antenna behind the cockpit, created from thin wire and mounted on a small, streamlined socket.

  

Painting and markings:

The upper surfaces were painted in standard RAF WWII colors, Dark Green and Ocean Grey, using a mix of Humbrol 163 and 30 for a slightly more bluish WWII-style green and a mix of 106 and 145 for a lightened grey tone, respectively. As an individual contrast and paint scheme variation the undersides and the spinner were painted in RAF Azure Blue (Humbrol 157, lightened up with 47), more appropriate than the standard WWII Medium Sea Grey from the European theatre of operations. The cockpit interior became RAF cockpit green (Humbro,78) while the inside surfaces of the landing gear were painted in Medium Sea Grey (Humbrol 165), reflecting the original undersides’ tone in former RAF service.

 

Other markings were minimal. The Iraqi triangles were taken from a Balkan Models Su-25 sheet, because their green was rather pale, for more contrast to the surrounding camouflage. RIrAF fin flash was taken from a PM Model Hawker Fury two-seater (a.k.a. “Bagdad Fury”). The tactical code came from an Airfix Hawker Hunter (from an optional Kuwaiti machine). This looked O.K. but somewhat bleak, so I added more markings. I could not find any evidence for special ID markings on Iraqi aircraft during the Arab-Israel war, but to add an eye-catcher I gave the aircraft white ID bands on the wings and on the fuselage – inspired by markings carried by Egyptian aircraft (e. g. Spitfires) during the conflict, but somewhat simplified, without black trim. They were created from generic white decal sheet material.

 

After some soot stains around the gun ports and the exhausts, the model was sealed with matt acrylic varnish.

  

A relatively simple project and just a fictional livery - but the Iraqi Spitfire looks pretty cool, especially the ID stripes add a special touch. The European RAF scheme looks a bit off on an aircraft that would be delivered to the Middel East, but the Iraqi Air Force operated British types like the Hunter in this guise, and later Su-22 fighter bombers carried a similarly murky camouflage in very dark green and earth brown.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some Background:

During the 1950s, Hindustan Aircraft Limited (HAL) had developed and produced several types of trainer aircraft, such as the HAL HT-2. However, elements within the firm were eager to expand into the then-new realm of supersonic fighter aircraft. Around the same time, the Indian government was in the process of formulating a new Air Staff Requirement for a Mach 2-capable combat aircraft to equip the Indian Air Force (IAF). However, as HAL lacked the necessary experience in both developing and manufacturing frontline combat fighters, it was clear that external guidance would be invaluable; this assistance was embodied by Kurt Tank.

 

In 1956, HAL formally began design work on the supersonic fighter project. The Indian government, led by Jawaharlal Nehru, authorized the development of the aircraft, stating that it would aid in the development of a modern aircraft industry in India. The first phase of the project sought to develop an airframe suitable for travelling at supersonic speeds, and able to effectively perform combat missions as a fighter aircraft, while the second phase sought to domestically design and produce an engine capable of propelling the aircraft. Early on, there was an explicit adherence to satisfying the IAF's requirements for a capable fighter bomber; attributes such as a twin-engine configuration and a speed of Mach 1.4 to 1.5 were quickly emphasized, and this led to the HF-24 Marut.

 

On 24 June 1961, the first prototype Marut conducted its maiden flight. It was powered by the same Bristol Siddeley Orpheus 703 turbojets that had powered the Folland Gnat, also being manufactured by HAL at that time. On 1 April 1967, the first production Marut was delivered to the IAF. While originally intended only as an interim measure during testing, HAL decided to power production Maruts with a pair of unreheated Orpheus 703s, meaning the aircraft could not attain supersonic speed. Although originally conceived to operate around Mach 2 the Marut in fact was barely capable of reaching Mach 1 due to the lack of suitably powerful engines.

 

The IAF were reluctant to procure a fighter aircraft only marginally superior to its existing fleet of British-built Hawker Hunters. However, in 1961, the Indian Government decided to procure the Marut, nevertheless, but only 147 aircraft, including 18 two-seat trainers, were completed out of a planned 214. Just after the decision to build the lukewarm Marut, the development of a more advanced aircraft with the desired supersonic performance was initiated.

 

This enterprise started star-crossed, though: after the Indian Government conducted its first nuclear tests at Pokhran, international pressure prevented the import of better engines of Western origin, or at times, even spares for the Orpheus engines, so that the Marut never realized its full potential due to insufficient power, and it was relatively obsolescent by the time it reached production.

Due to these restrictions India looked for other sources for supersonic aircraft and eventually settled upon the MiG-21 F-13 from the Soviet Union, which entered service in 1964. While fast and agile, the Fishbed was only a short-range daylight interceptor. It lacked proper range for escort missions and air space patrols, and it had no radar that enabled it to conduct all-weather interceptions. To fill this operational gap, the new indigenous HF-26 project was launched around the same time.

 

For the nascent Indian aircraft industry, HF-26 had a demanding requirements specification: the aircraft was to achieve Mach 2 top speed at high altitude and carry a radar with a guided missile armament that allowed interceptions in any weather, day and night. The powerplant question was left open, but it was clear from the start that a Soviet engine would be needed, since an indigenous development of a suitable powerplant would take much too long and block vital resources, and western alternatives were out of reach. The mission profile and the performance requirements quickly defined the planned aircraft’s layout: To fit a radar, the air intakes with movable ramps to feed the engines were placed on the fuselage flanks. To make sure the aircraft would fulfill its high-performance demands, it was right from the outset powered by two engines, and it was decided to give it delta wings, a popular design among high-speed aircraft of the time – exemplified by the highly successful Dassault Mirage III (which was to be delivered to Pakistan in 1967). With two engines, the HF-26 would be a heavier aircraft than the Mirage III, though, and it was planned to operate the aircraft from semi-prepared airfields, so that it would receive a robust landing gear with low-pressure tires and a brake parachute.

 

In 1962 India was able to negotiate the delivery of Tumansky RD-9 turbojet engines from the Soviet Union, even though no afterburner was part of the deal – this had to be indigenously developed by Hindustan Aeronautics Limited (HAL). However, this meant that the afterburner could be tailored to the HF-26, and this task would provide HAL with valuable engineering experience, too.

Now knowing the powerplant, HAL created a single-seater airframe around it, a rather robust design that superficially reminded of the French Mirage III, but there were fundamental differences. The HF-26 had boxy air intakes with movable ramps to control the airflow to the two engines and a relatively wide fuselage to hold them and most of the fuel in tanks between the air ducts behind the cockpit. The aircraft had a single swept fin and a rather small mid-positioned delta-wing with a 60° sweep. The pilot sat under a tight canopy that offered - similar to the Mirage III - only limited all-round vision.

The HF-26's conical nose radome covered an antenna for a ‘Garud’ interception radar – which was in fact a downgraded Soviet ‘Oryol' (Eagle; NATO reporting name 'Skip Spin') system that guided the HF-26’s main armament, a pair of semi-active radar homing (SARH) ‚Saanp’ missiles.

 

The Saanp missile was developed specifically for the HF-26 in India but used many components of Soviet origin, too, so that they were compatible with the radar. In performance, the Saanp was comparable with the French Matra R.530 air-to-air missile, even though the aerodynamic layout was reversed, with steering fins at the front end, right behind the SARH seaker head - overall the missile reminded of an enlarged AIM-4 Falcon. The missile weighed 180 kg and had a length of 3.5 m. Power came from a two-stage solid rocket that offered a maximum thrust of 80 kN for 2.7 s during the launch phase plus 6.5 s cruise. Maximum speed was Mach 2.7 and operational range was 1.5 to 20 km (0.9 to 12.5 miles). Two of these missiles could be carried on the main wing hardpoints in front of the landing gear wells. Alternatively, infrared-guided R-3 (AA-2 ‘Atoll’) short-range AAMs could be carried by the HF-26, too, and typically two of these were carried on the outer underwing hardpoints, which were plumbed to accept drop tanks (typically supersonic PTB-490s that were carried by the IAF's MiG-21s, too) . Initially, no internal gun was envisioned, as the HF-26 was supposed to be a pure high-speed/high-altitude interceptor that would not engage in dogfights. Two more hardpoints under the fuselage were plumbed, too, for a total of six external stations.

 

Due to its wing planform, the HF-26 was soon aptly called “Teer” (= Arrow), and with Soviet help the first prototype was rolled out in early 1964 and presented to the public. The first flight, however, would take place almost a year later in January 1965, due to many technical problems, and these were soon complemented by aerodynamic problems. The original delta-winged HF-26 had poor take-off and landing characteristics, and directional stability was weak, too. While a second prototype was under construction in April 1965 the first aircraft was lost after it had entered a spin from which the pilot could not escape – the aircraft crashed and its pilot was killed during the attempt to eject.

 

After this loss HAL investigated an enlarged fin and a modified wing design with deeper wingtips with lower sweep, which increased wing area and improved low speed handling, too. Furthermore, the fuselage shape had to be modified, too, to reduce supersonic drag, and a more pronounced area ruling was introduced. The indigenous afterburner for the RD-9 engines was unstable and troublesome, too.

It took until 1968 and three more flying prototypes (plus two static airframes) to refine the Teer for serial production service introduction. In this highly modified form, the aircraft was re-designated HF-26M and the first machines were delivered to IAF No. 3 Squadron in late 1969. However, it would take several months until a fully operational status could be achieved. By that time, it was already clear that the Teer, much like the HF-24 Marut before, could not live up to its expectations and was at the brink of becoming obsolete as it entered service. The RD-9 was not a modern engine anymore, and despite its indigenous afterburner – which turned out not only to be chronically unreliable but also to be very thirsty when engaged – the Teer had a disappointing performance: The fighter only achieved a top speed of Mach 1.6 at full power, and with full external load it hardly broke the wall of sound in level flight. Its main armament, the Saanp AAM, also turned out to be unreliable even under ideal conditions.

 

However, the HF-26M came just in time to take part in the Indo-Pakistani War of 1971 and was, despite its weaknesses, extensively used – even though not necessarily in its intended role. High-flying slow bombers were not fielded during the conflict, and the Teer remained, despite its on-board radar, heavily dependent on ground control interception (GCI) to vector its pilot onto targets coming in at medium and even low altitude. The HF-26M had no capability against low-flying aircraft either, so that pilots had to engage incoming, low-flying enemy aircraft after visual identification – a task the IAF’s nimble MiG-21s were much better suited for. Escorts and air cover missions for fighter-bombers were flown, too, but the HF-26M’s limited range only made it a suitable companion for the equally short-legged Su-7s. The IAF Canberras were frequently deployed on longer range missions, but the HF-26Ms simply could not follow them all the time; for a sufficient range the Teer had to carry four drop tanks, what increased drag and only left the outer pair of underwing hardpoints (which were not plumbed) free for a pair of AA-2 missiles. With the imminent danger of aerial close range combat, though, During the conflict with Pakistan, most HF-26M's were retrofitted with rear-view mirrors in their canopies to improve the pilot's field of view, and a passive IR sensor was added in a small fairing under the nose to improve the aircraft's all-weather capabilities and avoid active radar emissions that would warn potential prey too early.

 

The lack of an internal gun turned out to be another great weakness of the Teer, and this was only lightly mended through the use of external gun pods. Two of these cigar-shaped pods that resembled the Soviet UPK-23 pod could be carried on the two ventral pylons, and each contained a 23 mm Gryazev-Shipunov GSh-23L autocannon of Soviet origin with 200 rounds. Technically these pods were very similar to the conformal GP-9 pods carried by the IAF MiG-21FLs. While the gun pods considerably improved the HF-26M’s firepower and versatility, the pods were draggy, blocked valuable hardpoints (from extra fuel) and their recoil tended to damage the pylons as well as the underlying aircraft structure, so that they were only commissioned to be used in an emergency.

 

However, beyond air-to-air weapons, the HF-26M could also carry ordnance of up to 1.000 kg (2.207 lb) on the ventral and inner wing hardpoints and up to 500 kg (1.100 lb) on the other pair of wing hardpoints, including iron bombs and/or unguided missile pods. However, the limited field of view from the cockpit over the radome as well as the relatively high wing loading did not recommend the aircraft for ground attack missions – even though these frequently happened during the conflict with Pakistan. For these tactical missions, many HF-26Ms lost their original overall natural metal finish and instead received camouflage paint schemes on squadron level, resulting in individual and sometimes even spectacular liveries. Most notable examples were the Teer fighters of No. 1 Squadron (The Tigers), which sported various camouflage adaptations of the unit’s eponym.

 

Despite its many deficiencies, the HF-26M became heavily involved in the Indo-Pakistan conflict. As the Indian Army tightened its grip in East Pakistan, the Indian Air Force continued with its attacks against Pakistan as the campaign developed into a series of daylight anti-airfield, anti-radar, and close-support attacks by fighter jets, with night attacks against airfields and strategic targets by Canberras and An-12s, while Pakistan responded with similar night attacks with its B-57s and C-130s.

The PAF deployed its F-6s mainly on defensive combat air patrol missions over their own bases, leaving the PAF unable to conduct effective offensive operations.  Sporadic raids by the IAF continued against PAF forward air bases in Pakistan until the end of the war, and interdiction and close-support operations were maintained. One of the most successful air raids by India into West Pakistan happened on 8 December 1971, when Indian Hunter aircraft from the Pathankot-based 20 Squadron, attacked the Pakistani base in Murid and destroyed 5 F-86 aircraft on the ground.

The PAF played a more limited role in the operations, even though they were reinforced by Mirages from an unidentified Middle Eastern ally (whose identity remains unknown). The IAF was able to conduct a wide range of missions – troop support; air combat; deep penetration strikes; para-dropping behind enemy lines; feints to draw enemy fighters away from the actual target; bombing and reconnaissance. India flew 1,978 sorties in the East and about 4,000 in Pakistan, while the PAF flew about 30 and 2,840 at the respective fronts.  More than 80 percent of IAF sorties were close-support and interdiction and about 45 IAF aircraft were lost, including three HF-26Ms. Pakistan lost 60 to 75 aircraft, not including any F-86s, Mirage IIIs, or the six Jordanian F-104s which failed to return to their donors. The imbalance in air losses was explained by the IAF's considerably higher sortie rate and its emphasis on ground-attack missions. The PAF, which was solely focused on air combat, was reluctant to oppose these massive attacks and rather took refuge at Iranian air bases or in concrete bunkers, refusing to offer fights and respective losses.

 

After the war, the HF-26M was officially regarded as outdated, and as license production of the improved MiG-21FL (designated HAL Type 77 and nicknamed “Trishul” = Trident) and later of the MiG-21M (HAL Type 88) was organized in India, the aircraft were quickly retired from frontline units. They kept on serving into the Eighties, though, but now restricted to their original interceptor role. Beyond the upgrades from the Indo-Pakistani War, only a few upgrades were made. For instance, the new R-60 AAM was introduced to the HF-26M and around 1978 small (but fixed) canards were retrofitted to the air intakes behind the cockpit that improved the Teer’s poor slow speed control and high landing speed as well as the aircraft’s overall maneuverability.

A radar upgrade, together with the introduction of better air-to-ai missiles with a higher range and look down/shoot down capability was considered but never carried out. Furthermore, the idea of a true HF-26 2nd generation variant, powered by a pair of Tumansky R-11F-300 afterburner jet engines (from the license-built MiG-21FLs), was dropped, too – even though this powerplant eventually promised to fulfill the Teer’s design promise of Mach 2 top speed. A total of only 82 HF-26s (including thirteen two-seat trainers with a lengthened fuselage and reduced fuel capacity, plus eight prototypes) were built. The last aircraft were retired from IAF service in 1988 and replaced with Mirage 2000 fighters procured from France that were armed with the Matra Super 530 AAM.

  

General characteristics:

Crew: 1

Length: 14.97 m (49 ft ½ in)

Wingspan: 9.43 m (30 ft 11 in)

Height: 4.03 m (13 ft 2½ in)

Wing area: 30.6 m² (285 sq ft)

Empty weight: 7,000 kg (15,432 lb)

Gross weight: 10,954 kg (24,149 lb) with full internal fuel

Max takeoff weight: 15,700 kg (34,613 lb) with external stores

 

Powerplant:

2× Tumansky RD-9 afterburning turbojet engines; 29 kN (6,600 lbf) dry thrust each

and 36.78 kN (8,270 lbf) with afterburner

 

Performance:

Maximum speed: 1,700 km/h (1,056 mph; 917 kn; Mach 1.6) at 11,000 m (36,000 ft)

1,350 km/h (840 mph, 730 kn; Mach 1.1) at sea level

Combat range: 725 km (450 mi, 391 nmi) with internal fuel only

Ferry range: 1,700 km (1,100 mi, 920 nmi) with four drop tanks

Service ceiling: 18,100 m (59,400 ft)

g limits: +6.5

Time to altitude: 9,145 m (30,003 ft) in 1 minute 30 seconds

Wing loading: 555 kg/m² (114 lb/sq ft)

 

Armament

6× hardpoints (four underwing and two under the fuselage) for a total of 2.500 kg (5.500 lb);

Typical interceptor payload:

- two IR-guided R-3 or R-60 air-to-air-missiles or

two PTB-490 drop tanks on the outer underwing stations

- two semi-active radar-guided ‚Saanp’ air-to-air missiles or two more R-3 or R-60 AAMs

on inner underwing stations

- two 500 l drop tanks or two gun pods with a 23 mm GSh-23L autocannon and 200 RPG

each under the fuselage

  

The kit and its assembly:

This whiffy delta-wing fighter was inspired when I recently sliced up a PM Model Su-15 kit for my side-by-side-engine BAC Lightning build. At an early stage of the conversion, I held the Su-15 fuselage with its molded delta wings in my hand and wondered if a shortened tail section (as well as a shorter overall fuselage to keep proportions balanced) could make a delta-wing jet fighter from the Flagon base? Only a hardware experiment could yield an answer, and since the Su-15’s overall outlines look a bit retro I settled at an early stage on India as potential designer and operator, as “the thing the HF-24 Marut never was”.

 

True to the initial idea, work started on the tail, and I chopped off the fuselage behind the wings’ trailing edge. Some PSR was necessary to blend the separate exhaust section into the fuselage, which had to be reduced in depth through wedges that I cut out under the wings trailing edge, plus some good amount of glue and sheer force the bend the section a bit upwards. The PM Model's jet exhausts were drilled open, and I added afterburner dummies inside - anything would look better than the bleak vertical walls inside after only 2-3 mm! The original fin was omitted, because it was a bit too large for the new, smaller aircraft and its shape reminded a lot of the Suchoj heavy fighter family. It was replaced with a Mirage III/V fin, left over from a (crappy!) Pioneer 2 IAI Nesher kit.

 

Once the rear section was complete, I had to adjust the front end - and here the kitbashing started. First, I chopped off the cockpit section in front of the molded air intake - the Su-15’s long radome and the cockpit on top of the fuselage did not work anymore. As a remedy I remembered another Su-15 conversion I did a (long) while ago: I created a model of a planned ground attack derivative, the T-58Sh, and, as a part of the extensive body work, I transplanted the slanted nose from an academy MiG-27 between the air intakes – a stunt that was relatively easy and which appreciably lowered the cockpit position. For the HF-26M I did something similar, I just transplanted a cockpit from a Hasegawa/Academy MiG-23 with its ogival radome that size-wise better matched with the rest of the leftover Su-15 airframe.

 

The MiG-23 cockpit matched perfectly with the Su-15's front end, just the spinal area behind the cockpit had to be raised/re-sculpted to blend the parts smoothly together. For a different look from the Su-15 ancestry I also transplanted the front sections of the MiG-23 air intakes with their shorter ramps. Some mods had to be made to the Su-15 intake stubs, but the MiG-23 intakes were an almost perfect fit in size and shape and easy to integrate into the modified front hill. The result looks very natural!

However, when the fuselage was complete, I found that the nose appeared to be a bit too long, leaving the whole new hull with the wings somewhat off balance. As a remedy I decided at a rather late stage to shorten the nose and took out a 6 mm section in front of the cockpit - a stunt I had not planned, but sometimes you can judge things only after certain work stages. Some serious PSR was necessary to re-adjust the conical nose shape, which now looked more Mirage III-ish than planned!

 

The cockpit was taken mostly OOB, I just replaced the ejection seat and gave it a trigger handle made from thin wire. With the basic airframe complete it was time for details. The PM Model Su-15s massive and rather crude main landing gear was replaced with something more delicate from the scrap box, even though I retained the main wheels. The front landing gear was taken wholesale from the MiG-23, but had to be shortened for a proper stance.

A display holder adapter was integrated into the belly for the flight scenes, hidden well between the ventral ordnance.

 

The hardpoints, including missile launch rails, came from the MiG-23; the pylons had to be adjusted to match the Su-15's wing profile shape, the Anab missiles lost their tail sections to create the fictional Indian 'Saanp' AAMs. The R-3s on the outer stations were left over from a MP MiG-21. The ventral pylons belong to Academy MiG-23/27s, one came from the donor kit, the other was found in the spares box. The PTB-490 drop tanks also came from a KP MiG-21 (or one of its many reincarnations, not certain).

  

Painting and markings:

The paint scheme for this fictional aircraft was largely inspired by a picture of a whiffy and very attractive Saab 37 Viggen (an 1:72 Airfix kit) in IAF colors, apparently a model from a contest. BTW, India actually considered buying the Viggen for its Air Force!

IAF aircraft were and are known for their exotic and sometimes gawdy paint schemes, and with IAF MiG-21 “C 992” there’s even a very popular (yet obscure) aircraft that sported literal tiger stripes. The IAF Viggen model was surely inspired by this real aircraft, and I adopted something similar for my HF-26M.

 

IAF 1 Squadron was therefore settled, and for the paint scheme I opted for a "stripish" scheme, but not as "tigeresque" as "C 992". I found a suitable benchmark in a recent Libyian MiG-21, which carried a very disruptive two-tone grey scheme. I adapted this pattern to the HA-26M airframe and replaced its colors, similar to the IAF Viggen model, which became a greenish sand tone (a mix of Humbrol 121 with some 159; I later found out that I could have used Humbrol 83 from the beginning, though...) and a very dark olive drab (Humbrol 66, which looks like a dull dark brown in contrast with the sand tone), with bluish grey (Humbrol 247) undersides. With the large delta wings, this turned out to look very good and even effective!

 

For that special "Indian touch" I gave the aircraft a high-contrast fin in a design that I had seen on a real camouflaged IAF MiG-21bis: an overall dark green base with a broad, red vertical stripe which was also the shield for the fin flash and the aircraft's tactical code (on the original bare metal). The fin was first painted in green (Humbrol 2), the red stripe was created with orange-red decal sheet material. Similar material was also used to create the bare metal field for the tactical code, the yellow bars on the splitter plates and for the thin white canopy sealing.

 

After basic painting was done the model received an overall black ink washing, post-panel shading and extensive dry-brushing with aluminum and iron for a rather worn look.

The missiles became classic white, while the drop tanks, as a contrast to the camouflaged belly, were left in bare metal.

 

Decals/markings came primarily from a Begemot MiG-25 kit, the tactical codes on the fin and under the wings originally belong to an RAF post-WWII Spitfire, just the first serial letter was omitted. Stencils are few and they came from various sources. A compromise is the unit badge on the fin: I needed a tiger motif, and the only suitable option I found was the tiger head emblem on a white disc from RAF No. 74 Squadron, from the Matchbox BAC Lightning F.6&F.2A kit. It fits stylistically well, though. ;-)

 

Finally, the model was sealed with matt acrylic varnish (except for the black radome, which became a bit glossy) and finally assembled.

  

A spontaneous build, and the last one that I completed in 2022. However, despite a vague design plan the model evolved as it grew. Bashing the primitive PM Model Su-15 with the Academy MiG-23 parts was easier than expected, though, and the resulting fictional aircraft looks sturdy but quite believable - even though it appears to me like the unexpected child of a Mirage III/F-4 Phantom II intercourse, or like a juvenile CF-105 Arrow, just with mid-wings? Nevertheless, the disruptive paint scheme suits the delta wing fighter well, and the green/red fin is a striking contrast - it's a colorful model, but not garish.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some Background:

During the 1950s, Hindustan Aircraft Limited (HAL) had developed and produced several types of trainer aircraft, such as the HAL HT-2. However, elements within the firm were eager to expand into the then-new realm of supersonic fighter aircraft. Around the same time, the Indian government was in the process of formulating a new Air Staff Requirement for a Mach 2-capable combat aircraft to equip the Indian Air Force (IAF). However, as HAL lacked the necessary experience in both developing and manufacturing frontline combat fighters, it was clear that external guidance would be invaluable; this assistance was embodied by Kurt Tank.

 

In 1956, HAL formally began design work on the supersonic fighter project. The Indian government, led by Jawaharlal Nehru, authorized the development of the aircraft, stating that it would aid in the development of a modern aircraft industry in India. The first phase of the project sought to develop an airframe suitable for travelling at supersonic speeds, and able to effectively perform combat missions as a fighter aircraft, while the second phase sought to domestically design and produce an engine capable of propelling the aircraft. Early on, there was an explicit adherence to satisfying the IAF's requirements for a capable fighter bomber; attributes such as a twin-engine configuration and a speed of Mach 1.4 to 1.5 were quickly emphasized, and this led to the HF-24 Marut.

 

On 24 June 1961, the first prototype Marut conducted its maiden flight. It was powered by the same Bristol Siddeley Orpheus 703 turbojets that had powered the Folland Gnat, also being manufactured by HAL at that time. On 1 April 1967, the first production Marut was delivered to the IAF. While originally intended only as an interim measure during testing, HAL decided to power production Maruts with a pair of unreheated Orpheus 703s, meaning the aircraft could not attain supersonic speed. Although originally conceived to operate around Mach 2 the Marut in fact was barely capable of reaching Mach 1 due to the lack of suitably powerful engines.

 

The IAF were reluctant to procure a fighter aircraft only marginally superior to its existing fleet of British-built Hawker Hunters. However, in 1961, the Indian Government decided to procure the Marut, nevertheless, but only 147 aircraft, including 18 two-seat trainers, were completed out of a planned 214. Just after the decision to build the lukewarm Marut, the development of a more advanced aircraft with the desired supersonic performance was initiated.

 

This enterprise started star-crossed, though: after the Indian Government conducted its first nuclear tests at Pokhran, international pressure prevented the import of better engines of Western origin, or at times, even spares for the Orpheus engines, so that the Marut never realized its full potential due to insufficient power, and it was relatively obsolescent by the time it reached production.

Due to these restrictions India looked for other sources for supersonic aircraft and eventually settled upon the MiG-21 F-13 from the Soviet Union, which entered service in 1964. While fast and agile, the Fishbed was only a short-range daylight interceptor. It lacked proper range for escort missions and air space patrols, and it had no radar that enabled it to conduct all-weather interceptions. To fill this operational gap, the new indigenous HF-26 project was launched around the same time.

 

For the nascent Indian aircraft industry, HF-26 had a demanding requirements specification: the aircraft was to achieve Mach 2 top speed at high altitude and carry a radar with a guided missile armament that allowed interceptions in any weather, day and night. The powerplant question was left open, but it was clear from the start that a Soviet engine would be needed, since an indigenous development of a suitable powerplant would take much too long and block vital resources, and western alternatives were out of reach. The mission profile and the performance requirements quickly defined the planned aircraft’s layout: To fit a radar, the air intakes with movable ramps to feed the engines were placed on the fuselage flanks. To make sure the aircraft would fulfill its high-performance demands, it was right from the outset powered by two engines, and it was decided to give it delta wings, a popular design among high-speed aircraft of the time – exemplified by the highly successful Dassault Mirage III (which was to be delivered to Pakistan in 1967). With two engines, the HF-26 would be a heavier aircraft than the Mirage III, though, and it was planned to operate the aircraft from semi-prepared airfields, so that it would receive a robust landing gear with low-pressure tires and a brake parachute.

 

In 1962 India was able to negotiate the delivery of Tumansky RD-9 turbojet engines from the Soviet Union, even though no afterburner was part of the deal – this had to be indigenously developed by Hindustan Aeronautics Limited (HAL). However, this meant that the afterburner could be tailored to the HF-26, and this task would provide HAL with valuable engineering experience, too.

Now knowing the powerplant, HAL created a single-seater airframe around it, a rather robust design that superficially reminded of the French Mirage III, but there were fundamental differences. The HF-26 had boxy air intakes with movable ramps to control the airflow to the two engines and a relatively wide fuselage to hold them and most of the fuel in tanks between the air ducts behind the cockpit. The aircraft had a single swept fin and a rather small mid-positioned delta-wing with a 60° sweep. The pilot sat under a tight canopy that offered - similar to the Mirage III - only limited all-round vision.

The HF-26's conical nose radome covered an antenna for a ‘Garud’ interception radar – which was in fact a downgraded Soviet ‘Oryol' (Eagle; NATO reporting name 'Skip Spin') system that guided the HF-26’s main armament, a pair of semi-active radar homing (SARH) ‚Saanp’ missiles.

 

The Saanp missile was developed specifically for the HF-26 in India but used many components of Soviet origin, too, so that they were compatible with the radar. In performance, the Saanp was comparable with the French Matra R.530 air-to-air missile, even though the aerodynamic layout was reversed, with steering fins at the front end, right behind the SARH seaker head - overall the missile reminded of an enlarged AIM-4 Falcon. The missile weighed 180 kg and had a length of 3.5 m. Power came from a two-stage solid rocket that offered a maximum thrust of 80 kN for 2.7 s during the launch phase plus 6.5 s cruise. Maximum speed was Mach 2.7 and operational range was 1.5 to 20 km (0.9 to 12.5 miles). Two of these missiles could be carried on the main wing hardpoints in front of the landing gear wells. Alternatively, infrared-guided R-3 (AA-2 ‘Atoll’) short-range AAMs could be carried by the HF-26, too, and typically two of these were carried on the outer underwing hardpoints, which were plumbed to accept drop tanks (typically supersonic PTB-490s that were carried by the IAF's MiG-21s, too) . Initially, no internal gun was envisioned, as the HF-26 was supposed to be a pure high-speed/high-altitude interceptor that would not engage in dogfights. Two more hardpoints under the fuselage were plumbed, too, for a total of six external stations.

 

Due to its wing planform, the HF-26 was soon aptly called “Teer” (= Arrow), and with Soviet help the first prototype was rolled out in early 1964 and presented to the public. The first flight, however, would take place almost a year later in January 1965, due to many technical problems, and these were soon complemented by aerodynamic problems. The original delta-winged HF-26 had poor take-off and landing characteristics, and directional stability was weak, too. While a second prototype was under construction in April 1965 the first aircraft was lost after it had entered a spin from which the pilot could not escape – the aircraft crashed and its pilot was killed during the attempt to eject.

 

After this loss HAL investigated an enlarged fin and a modified wing design with deeper wingtips with lower sweep, which increased wing area and improved low speed handling, too. Furthermore, the fuselage shape had to be modified, too, to reduce supersonic drag, and a more pronounced area ruling was introduced. The indigenous afterburner for the RD-9 engines was unstable and troublesome, too.

It took until 1968 and three more flying prototypes (plus two static airframes) to refine the Teer for serial production service introduction. In this highly modified form, the aircraft was re-designated HF-26M and the first machines were delivered to IAF No. 3 Squadron in late 1969. However, it would take several months until a fully operational status could be achieved. By that time, it was already clear that the Teer, much like the HF-24 Marut before, could not live up to its expectations and was at the brink of becoming obsolete as it entered service. The RD-9 was not a modern engine anymore, and despite its indigenous afterburner – which turned out not only to be chronically unreliable but also to be very thirsty when engaged – the Teer had a disappointing performance: The fighter only achieved a top speed of Mach 1.6 at full power, and with full external load it hardly broke the wall of sound in level flight. Its main armament, the Saanp AAM, also turned out to be unreliable even under ideal conditions.

 

However, the HF-26M came just in time to take part in the Indo-Pakistani War of 1971 and was, despite its weaknesses, extensively used – even though not necessarily in its intended role. High-flying slow bombers were not fielded during the conflict, and the Teer remained, despite its on-board radar, heavily dependent on ground control interception (GCI) to vector its pilot onto targets coming in at medium and even low altitude. The HF-26M had no capability against low-flying aircraft either, so that pilots had to engage incoming, low-flying enemy aircraft after visual identification – a task the IAF’s nimble MiG-21s were much better suited for. Escorts and air cover missions for fighter-bombers were flown, too, but the HF-26M’s limited range only made it a suitable companion for the equally short-legged Su-7s. The IAF Canberras were frequently deployed on longer range missions, but the HF-26Ms simply could not follow them all the time; for a sufficient range the Teer had to carry four drop tanks, what increased drag and only left the outer pair of underwing hardpoints (which were not plumbed) free for a pair of AA-2 missiles. With the imminent danger of aerial close range combat, though, During the conflict with Pakistan, most HF-26M's were retrofitted with rear-view mirrors in their canopies to improve the pilot's field of view, and a passive IR sensor was added in a small fairing under the nose to improve the aircraft's all-weather capabilities and avoid active radar emissions that would warn potential prey too early.

 

The lack of an internal gun turned out to be another great weakness of the Teer, and this was only lightly mended through the use of external gun pods. Two of these cigar-shaped pods that resembled the Soviet UPK-23 pod could be carried on the two ventral pylons, and each contained a 23 mm Gryazev-Shipunov GSh-23L autocannon of Soviet origin with 200 rounds. Technically these pods were very similar to the conformal GP-9 pods carried by the IAF MiG-21FLs. While the gun pods considerably improved the HF-26M’s firepower and versatility, the pods were draggy, blocked valuable hardpoints (from extra fuel) and their recoil tended to damage the pylons as well as the underlying aircraft structure, so that they were only commissioned to be used in an emergency.

 

However, beyond air-to-air weapons, the HF-26M could also carry ordnance of up to 1.000 kg (2.207 lb) on the ventral and inner wing hardpoints and up to 500 kg (1.100 lb) on the other pair of wing hardpoints, including iron bombs and/or unguided missile pods. However, the limited field of view from the cockpit over the radome as well as the relatively high wing loading did not recommend the aircraft for ground attack missions – even though these frequently happened during the conflict with Pakistan. For these tactical missions, many HF-26Ms lost their original overall natural metal finish and instead received camouflage paint schemes on squadron level, resulting in individual and sometimes even spectacular liveries. Most notable examples were the Teer fighters of No. 1 Squadron (The Tigers), which sported various camouflage adaptations of the unit’s eponym.

 

Despite its many deficiencies, the HF-26M became heavily involved in the Indo-Pakistan conflict. As the Indian Army tightened its grip in East Pakistan, the Indian Air Force continued with its attacks against Pakistan as the campaign developed into a series of daylight anti-airfield, anti-radar, and close-support attacks by fighter jets, with night attacks against airfields and strategic targets by Canberras and An-12s, while Pakistan responded with similar night attacks with its B-57s and C-130s.

The PAF deployed its F-6s mainly on defensive combat air patrol missions over their own bases, leaving the PAF unable to conduct effective offensive operations.  Sporadic raids by the IAF continued against PAF forward air bases in Pakistan until the end of the war, and interdiction and close-support operations were maintained. One of the most successful air raids by India into West Pakistan happened on 8 December 1971, when Indian Hunter aircraft from the Pathankot-based 20 Squadron, attacked the Pakistani base in Murid and destroyed 5 F-86 aircraft on the ground.

The PAF played a more limited role in the operations, even though they were reinforced by Mirages from an unidentified Middle Eastern ally (whose identity remains unknown). The IAF was able to conduct a wide range of missions – troop support; air combat; deep penetration strikes; para-dropping behind enemy lines; feints to draw enemy fighters away from the actual target; bombing and reconnaissance. India flew 1,978 sorties in the East and about 4,000 in Pakistan, while the PAF flew about 30 and 2,840 at the respective fronts.  More than 80 percent of IAF sorties were close-support and interdiction and about 45 IAF aircraft were lost, including three HF-26Ms. Pakistan lost 60 to 75 aircraft, not including any F-86s, Mirage IIIs, or the six Jordanian F-104s which failed to return to their donors. The imbalance in air losses was explained by the IAF's considerably higher sortie rate and its emphasis on ground-attack missions. The PAF, which was solely focused on air combat, was reluctant to oppose these massive attacks and rather took refuge at Iranian air bases or in concrete bunkers, refusing to offer fights and respective losses.

 

After the war, the HF-26M was officially regarded as outdated, and as license production of the improved MiG-21FL (designated HAL Type 77 and nicknamed “Trishul” = Trident) and later of the MiG-21M (HAL Type 88) was organized in India, the aircraft were quickly retired from frontline units. They kept on serving into the Eighties, though, but now restricted to their original interceptor role. Beyond the upgrades from the Indo-Pakistani War, only a few upgrades were made. For instance, the new R-60 AAM was introduced to the HF-26M and around 1978 small (but fixed) canards were retrofitted to the air intakes behind the cockpit that improved the Teer’s poor slow speed control and high landing speed as well as the aircraft’s overall maneuverability.

A radar upgrade, together with the introduction of better air-to-ai missiles with a higher range and look down/shoot down capability was considered but never carried out. Furthermore, the idea of a true HF-26 2nd generation variant, powered by a pair of Tumansky R-11F-300 afterburner jet engines (from the license-built MiG-21FLs), was dropped, too – even though this powerplant eventually promised to fulfill the Teer’s design promise of Mach 2 top speed. A total of only 82 HF-26s (including thirteen two-seat trainers with a lengthened fuselage and reduced fuel capacity, plus eight prototypes) were built. The last aircraft were retired from IAF service in 1988 and replaced with Mirage 2000 fighters procured from France that were armed with the Matra Super 530 AAM.

  

General characteristics:

Crew: 1

Length: 14.97 m (49 ft ½ in)

Wingspan: 9.43 m (30 ft 11 in)

Height: 4.03 m (13 ft 2½ in)

Wing area: 30.6 m² (285 sq ft)

Empty weight: 7,000 kg (15,432 lb)

Gross weight: 10,954 kg (24,149 lb) with full internal fuel

Max takeoff weight: 15,700 kg (34,613 lb) with external stores

 

Powerplant:

2× Tumansky RD-9 afterburning turbojet engines; 29 kN (6,600 lbf) dry thrust each

and 36.78 kN (8,270 lbf) with afterburner

 

Performance:

Maximum speed: 1,700 km/h (1,056 mph; 917 kn; Mach 1.6) at 11,000 m (36,000 ft)

1,350 km/h (840 mph, 730 kn; Mach 1.1) at sea level

Combat range: 725 km (450 mi, 391 nmi) with internal fuel only

Ferry range: 1,700 km (1,100 mi, 920 nmi) with four drop tanks

Service ceiling: 18,100 m (59,400 ft)

g limits: +6.5

Time to altitude: 9,145 m (30,003 ft) in 1 minute 30 seconds

Wing loading: 555 kg/m² (114 lb/sq ft)

 

Armament

6× hardpoints (four underwing and two under the fuselage) for a total of 2.500 kg (5.500 lb);

Typical interceptor payload:

- two IR-guided R-3 or R-60 air-to-air-missiles or

two PTB-490 drop tanks on the outer underwing stations

- two semi-active radar-guided ‚Saanp’ air-to-air missiles or two more R-3 or R-60 AAMs

on inner underwing stations

- two 500 l drop tanks or two gun pods with a 23 mm GSh-23L autocannon and 200 RPG

each under the fuselage

  

The kit and its assembly:

This whiffy delta-wing fighter was inspired when I recently sliced up a PM Model Su-15 kit for my side-by-side-engine BAC Lightning build. At an early stage of the conversion, I held the Su-15 fuselage with its molded delta wings in my hand and wondered if a shortened tail section (as well as a shorter overall fuselage to keep proportions balanced) could make a delta-wing jet fighter from the Flagon base? Only a hardware experiment could yield an answer, and since the Su-15’s overall outlines look a bit retro I settled at an early stage on India as potential designer and operator, as “the thing the HF-24 Marut never was”.

 

True to the initial idea, work started on the tail, and I chopped off the fuselage behind the wings’ trailing edge. Some PSR was necessary to blend the separate exhaust section into the fuselage, which had to be reduced in depth through wedges that I cut out under the wings trailing edge, plus some good amount of glue and sheer force the bend the section a bit upwards. The PM Model's jet exhausts were drilled open, and I added afterburner dummies inside - anything would look better than the bleak vertical walls inside after only 2-3 mm! The original fin was omitted, because it was a bit too large for the new, smaller aircraft and its shape reminded a lot of the Suchoj heavy fighter family. It was replaced with a Mirage III/V fin, left over from a (crappy!) Pioneer 2 IAI Nesher kit.

 

Once the rear section was complete, I had to adjust the front end - and here the kitbashing started. First, I chopped off the cockpit section in front of the molded air intake - the Su-15’s long radome and the cockpit on top of the fuselage did not work anymore. As a remedy I remembered another Su-15 conversion I did a (long) while ago: I created a model of a planned ground attack derivative, the T-58Sh, and, as a part of the extensive body work, I transplanted the slanted nose from an academy MiG-27 between the air intakes – a stunt that was relatively easy and which appreciably lowered the cockpit position. For the HF-26M I did something similar, I just transplanted a cockpit from a Hasegawa/Academy MiG-23 with its ogival radome that size-wise better matched with the rest of the leftover Su-15 airframe.

 

The MiG-23 cockpit matched perfectly with the Su-15's front end, just the spinal area behind the cockpit had to be raised/re-sculpted to blend the parts smoothly together. For a different look from the Su-15 ancestry I also transplanted the front sections of the MiG-23 air intakes with their shorter ramps. Some mods had to be made to the Su-15 intake stubs, but the MiG-23 intakes were an almost perfect fit in size and shape and easy to integrate into the modified front hill. The result looks very natural!

However, when the fuselage was complete, I found that the nose appeared to be a bit too long, leaving the whole new hull with the wings somewhat off balance. As a remedy I decided at a rather late stage to shorten the nose and took out a 6 mm section in front of the cockpit - a stunt I had not planned, but sometimes you can judge things only after certain work stages. Some serious PSR was necessary to re-adjust the conical nose shape, which now looked more Mirage III-ish than planned!

 

The cockpit was taken mostly OOB, I just replaced the ejection seat and gave it a trigger handle made from thin wire. With the basic airframe complete it was time for details. The PM Model Su-15s massive and rather crude main landing gear was replaced with something more delicate from the scrap box, even though I retained the main wheels. The front landing gear was taken wholesale from the MiG-23, but had to be shortened for a proper stance.

A display holder adapter was integrated into the belly for the flight scenes, hidden well between the ventral ordnance.

 

The hardpoints, including missile launch rails, came from the MiG-23; the pylons had to be adjusted to match the Su-15's wing profile shape, the Anab missiles lost their tail sections to create the fictional Indian 'Saanp' AAMs. The R-3s on the outer stations were left over from a MP MiG-21. The ventral pylons belong to Academy MiG-23/27s, one came from the donor kit, the other was found in the spares box. The PTB-490 drop tanks also came from a KP MiG-21 (or one of its many reincarnations, not certain).

  

Painting and markings:

The paint scheme for this fictional aircraft was largely inspired by a picture of a whiffy and very attractive Saab 37 Viggen (an 1:72 Airfix kit) in IAF colors, apparently a model from a contest. BTW, India actually considered buying the Viggen for its Air Force!

IAF aircraft were and are known for their exotic and sometimes gawdy paint schemes, and with IAF MiG-21 “C 992” there’s even a very popular (yet obscure) aircraft that sported literal tiger stripes. The IAF Viggen model was surely inspired by this real aircraft, and I adopted something similar for my HF-26M.

 

IAF 1 Squadron was therefore settled, and for the paint scheme I opted for a "stripish" scheme, but not as "tigeresque" as "C 992". I found a suitable benchmark in a recent Libyian MiG-21, which carried a very disruptive two-tone grey scheme. I adapted this pattern to the HA-26M airframe and replaced its colors, similar to the IAF Viggen model, which became a greenish sand tone (a mix of Humbrol 121 with some 159; I later found out that I could have used Humbrol 83 from the beginning, though...) and a very dark olive drab (Humbrol 66, which looks like a dull dark brown in contrast with the sand tone), with bluish grey (Humbrol 247) undersides. With the large delta wings, this turned out to look very good and even effective!

 

For that special "Indian touch" I gave the aircraft a high-contrast fin in a design that I had seen on a real camouflaged IAF MiG-21bis: an overall dark green base with a broad, red vertical stripe which was also the shield for the fin flash and the aircraft's tactical code (on the original bare metal). The fin was first painted in green (Humbrol 2), the red stripe was created with orange-red decal sheet material. Similar material was also used to create the bare metal field for the tactical code, the yellow bars on the splitter plates and for the thin white canopy sealing.

 

After basic painting was done the model received an overall black ink washing, post-panel shading and extensive dry-brushing with aluminum and iron for a rather worn look.

The missiles became classic white, while the drop tanks, as a contrast to the camouflaged belly, were left in bare metal.

 

Decals/markings came primarily from a Begemot MiG-25 kit, the tactical codes on the fin and under the wings originally belong to an RAF post-WWII Spitfire, just the first serial letter was omitted. Stencils are few and they came from various sources. A compromise is the unit badge on the fin: I needed a tiger motif, and the only suitable option I found was the tiger head emblem on a white disc from RAF No. 74 Squadron, from the Matchbox BAC Lightning F.6&F.2A kit. It fits stylistically well, though. ;-)

 

Finally, the model was sealed with matt acrylic varnish (except for the black radome, which became a bit glossy) and finally assembled.

  

A spontaneous build, and the last one that I completed in 2022. However, despite a vague design plan the model evolved as it grew. Bashing the primitive PM Model Su-15 with the Academy MiG-23 parts was easier than expected, though, and the resulting fictional aircraft looks sturdy but quite believable - even though it appears to me like the unexpected child of a Mirage III/F-4 Phantom II intercourse, or like a juvenile CF-105 Arrow, just with mid-wings? Nevertheless, the disruptive paint scheme suits the delta wing fighter well, and the green/red fin is a striking contrast - it's a colorful model, but not garish.