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GP40's and GP40-2's seemed to be the backbone of Chessie System's locomotive fleet, at least in Chicago. Here's an example as a westbound hits the diamonds at Stateline on its way to Barr Yard. Guess which state I'm standing in....not the state the train is in. Weird, isn't it? OK, OK, so it isn't.....
On 10th June 1967, Newcastle-built Robert Stephenson & Hawthorns 0-6-0 tank 'No.39' (W/No.7764 built in 1954) heads the ‘S.L.S./M.L.S. Ashington Rail tour’ special charter train using former miners’ “Paddy Train” coaches, seen at Ashington No.1 Loop signal box, near Hirst Platforms station, between Linton and Ashington. Former main line coaches of North Eastern Railway and Furness Railway origin were purchased by the NCB and its predecessors and were used for their services operating between Ashington, Linton and Ellington collieries. This double-track section comprised a circular route of around twenty miles with several branches running off, and served Woodhorn, Newbiggin, Lynemouth and Linton collieries, as well as Longhirst drift mine. The fully-signalled route was not entirely completed until as late as August 1956, when a new link line was opened between Woodhorn and Lynemouth, thus completing the circuit, with halts at Ashington, Ellington, Linton, and North Moor. The passenger service had ceased running on 16th May 1966. Part of this section, retained by Network Rail, is now used by main line freight services to and from Lynemouth power station and until recently the Alcan aluminium smelter before its closure. The Ashington Group Railway, as it was known, required Board of Trade inspection and a signalling system, using both lower and upper-quadrant signal types. The 18x24-in outside cylinder tank locos, 'No.39' and 'No.40', were built especially for hauling the system’s workmen’s services, although in practice these locos were not used exclusively on the “Paddy Trains”. Some locos, including those used on the passenger services, were fitted with steam-powered generators and directional lights front and rear, to enable working around the clock.
© Gordon Edgar collection - All rights reserved. Please do not use my images without my explicit permission
+++ DISCLAIMER +++
Nothing you see here is real, even though the model, the conversion or the presented background story might be based historical facts. BEWARE!
Some background:
In the aftermath of the Second World War, Sweden required a strong air defense, utilizing the newly developed jet propulsion technology. The original concept had been designed around a mostly straight wing, but after Swedish engineers had obtained German research data on swept-wing designs, the prototype was altered to incorporate a 25° sweep. In order to make the wing as thin as possible, Saab elected to locate the retractable undercarriage in the aircraft's fuselage rather than into the wings.
Extensive wind tunnel testing had also influenced aspects of the aircraft's aerodynamics, such as stability and trim across the aircraft's speed range. In order to test the design of the swept wing further and avoid any surprises, it was decided to modify a Saab Safir. It received the designation Saab 201 and a full-scale swept wing for a series of flight tests. The first 'final' sketches of the aircraft, incorporating the new information, were drawn in January 1946.
The originally envisioned powerplant for the new fighter type was the de Havilland Goblin turbojet engine. However, in December 1945, information on the newer and more powerful de Havilland Ghost engine became available. The new engine was deemed to be ideal for Saab's in-development aircraft, as not only did the Ghost engine had provisions for the use of a central circular air intake, the overall diameter of the engine was favorable for the planned fuselage dimensions, too. Thus, following negotiations between de Havilland and Saab, the Ghost engine was selected to power the type and built in license as the RM 2.
By February 1946 the main outline of the proposed aircraft had been clearly defined. In autumn 1946, following the resolution of all major questions of principal and the completion of the project specification, the Swedish Air Force formally ordered the completion of the design and that three prototype aircraft be produced, giving the proposed type the designation J 29. After a thorough test program, production of the type commenced in 1948 and, in May 1951, the first deliveries of operational production aircraft were received by F 13 Norrköping. The J 29 proved to be very successful and several variants and updates of the Tunnan were produced, including a dedicated reconnaissance variant, a two seat trainer and an all-weather fighter with an onboard radar
However, Sweden foresaw that there would soon be a need for a jet fighter that could intercept bombers at high altitude and also successfully engage fighters. During September 1949, the Swedish Air Force, via the Swedish Defence Material Administration, released a requirement for a cutting-edge interceptor aircraft that was envisioned to be capable of attacking hostile bomber aircraft in the transonic speed range. As released, this requirement specified a top speed of Mach speed 1.4 to 1.5. (1956, the specified speed was revised and raised to Mach 1.7-1.8, and eventually led to the Saab 35 Draken). With the barely supersonic Saab 32 Lansen just under development, and intended for different roles than being a nimble day fighter, the company searched for a way to either achieve supersonic flight through modifications of an existing type or at least gather sufficient data and develop and try the new technologies necessary to meet the 1949 requirements.
Since Sweden did not have a truly supersonic aircraft in its inventory (not even an experimental type), Saab decided to convert the Saab 29 into a supersonic testbed, with the outlook to develop an interim day fighter that could replace the various Tunnan fighter versions and support the new Lansen fleet until a fully capable Mach 1.5+ interceptor was ready for service. Even though the type was regarded as a pure experimental aircraft, the designation remained close to the J29 nomenclature in order to secure military funding for the project and to confuse eventual spies. Consequently, the P29 was initially presented as a new J29 version (hence the “G” suffix).
The P29G was based on a heavily modified production J29B airframe, which was built in two versions and only in two specimens. Work on the first airframe started in 1952, just when the first Saab 32 prototype made its maiden flight. The initial challenge consisted of integrating two relatively compact axial flow jet engines with afterburners into the fuselage, since the J29’s original RM2, even in its late afterburner variant, was not able to safely deliver the necessary thrust for the intended supersonic flight program. After long negotiations, Saab was able to procure a small number of Westinghouse J34-WE-42 turbojets from the USA, which delivered as a pair 40% more thrust than the original RM2B. The engines were only delivered under the restriction that they would exclusively be used in connection with the supersonic research program.
Through a thorough re-construction, the Saab team was able to mount the new engines into the lower rear fuselage, and, internally, the air intake duct had to be modified and forked behind the landing gear wells. Due to the significantly widened rear fuselage, the P29G became quickly nicknamed “Kurviga Tunnan” (= “Curvy Barrel”). Even though the widened rear fuselage increased the aircraft’s frontal cross section, the modified shape had the (unintended) effect of area ruling, a welcome side benefit which became apparent during the flight test and which largely promoted the P29G’s gain of top speed.
Another special and unique feature of the P29G was a special wing attachment system. It consisted of two strengthened, open box spars in the fuselage with additional attachment points along the wing roots, which allowed different wings to be switched with relatively little effort. However, due to this modification, the wing tanks (with a total capacity of 900l inside of the J29s standard wings) were lost and only 2.150l in the Saab 29’s standard fuselage tanks could be carried – but this was, for a research aircraft, not regarded as a major weakness, and compensated for the wing attachment system’s additional weight. The original wing-mounted pitots were replaced by a single, massive sensor boom attached to the aircraft’s nose above the air intake, slightly set-off to starboard in order to give the pilot an unobstructed view.
The first P29G's maiden flight, marked “Gul Urban” (Yellow U), took place in July 1955. The aircraft behaved normally, even though the center of gravity had markedly shifted backwards and the overall gain of weight made the aircraft slightly unstable along the longitudinal axis. During the initial, careful attempts to break the sound barrier, it soon became apparent that both the original wings as well as the original air intake shape limited the P29G's potential. In its original form, the P29G could only barely pass Mach 1 in level flight.
As a consequence, the second P29G, which had been under conversion from another J29B airframe since mid-1954, received more thorough modifications. The air intake was lengthened and widened, and in order to make it more effective at supersonic speed it received a sharp lip. Wind tunnel tests with the first machine led to a modified tail, too: the fin was now taller and further swept back, the stabilizer was moved to a higher position, resulting in a cruciform layout. The original single-piece stabilizer was furthermore replaced by a two-piece, all-moving construction with a 45° sweep and a thinner profile. This not only improved the aerodynamics at high speed, it also suppressed the longitudinal instability problem, even though this was never really cured.
Due to the even higher all-up weight of the new aircraft, the landing gear was reinforced and the 2nd P29G received an experimental suspension system on its main legs with higher spring travel, which was designed for operations on semi-prepared airfields. This system had actually been designed for the updated J29 fighters (esp. the A32B attack variant), but it was not introduced into series production or the Saab 29E/F conversion program. Despite these massive changes, the P29G designation was retained, and the second machine, carrying the tactical code “Röd Urban” (Red U), was quickly nicknamed “Karpen” (“Carp”), due to its characteristic new intake shape, the long fin and its stocky shape.
The second P29G was ready for flight tests in August 1956, just in time to support the Saab 35’s ongoing development – the aircraft, which was eventually built to meet (and exceed) the Swedish Air Force’s 1949 supersonic interceptor requirement. The modifications proved to be successful and the P29G was, fitted with a 60° sweep wing and in clean configuration, able to achieve a maximum speed of 1.367 km/h (849 mph) in level flight, a formidable achievement (vs. the 1,060 km/h (660 mph) of the late J29F and the 1200 km/h (745 mph) of the J32B interceptor) for the post WWII design.
Several wing shapes and profiles were tested, including sweep angles from 25° to 63° as well as different shapes and profiles. Even though the machines carried provisions for the J29’s standard armament, the 20 mm cannons were normally not mounted and replaced with sensors and recording equipment. However, both machines were temporarily fitted with one or two guns in order to analyze the effects of firing the weapons at supersonic speed. Underwing ordnance was also almost never carried. In some tests, though, light bombs or unguided missiles were carried and deployed, or podded cine cameras were carried.
While the second P29G was used for high speed trials, the first machine remained in its original guise and took over low speed handling tests. Thanks to the unique wing switch mechanism, the supersonic research program could be held within a very tight schedule and lasted until late 1959. Thereafter, the P29Gs’ potential was of little use anymore, and the engine use agreement with the USA put an end to further use of the two aircraft, so that both P29Gs were retired from service in 1960. The 1st machine, outfitted with standard J29F wings and stripped off of its engines, remained in use as an instructional air at Malmslätt air base 1969, while the second machine was mothballed. However, both airframes were eventually scrapped in 1970.
General characteristics:
Crew: 1
Length: 11.66 m (38 ft 2 in) fuselage only,
13,97 m (45 ft 9 in) with pitot boom
Wingspan: varied*; 11.0 m (36 ft 1 in) with standard 25° sweep wings,
10.00 m (32 ft 9 ¾ in) with experimental 45° wings
Height: 4.54m (14 ft 10 ½ in)
Wing area: varied*; 24.15 m² (260.0 ft²) with standard 25° sweep wings
22.5 m² (242.2 ft²) with experimental 45° wings
Empty weight: 5,220 kg (11,500 lb)
Max. takeoff weight: 8,510 kg (18,744 lb)
Powerplant:
2× Westinghouse J34-WE-42 turbojets, each rated at 3,400 lbf (15 kN) dry thrust
and 4,200 lbf (19 kN) with full afterburner
Performance:
Maximum speed: 1.367 km/h (849 mph) were achieved*
Range: 790 km (490 mi)
Service ceiling: up to 17,250 m (56,500 ft)*
Rate of climb: up to 45 m/s (8,850 ft/min)*
*Varying figures due to different tested wing configurations
Armament:
None installed; provisions for 4x 20mm Hispano Mark V autocannon in the lower front fuselage.
Depending on the mounted wing type, various external loads could be carried, including a wide range of light bombs, 75 mm (3 in) air-to-air rockets, 145 mm (5.8 in) anti-armor rockets, 150 mm (6 in) HE (high-explosive) rockets or 180 mm (7.2 in) HE anti-ship rockets. Due to the lack of complex wiring or fuel plumbing, no guided weapons or drop tanks could be mounted, though.
The kit and its assembly:
Sweden is a prolific whiffing territory, and the Saab 29 offers some interesting options. This highly modified Tunnan, which is actually rather a kitbashing than a mere model kit modification, is/was a submission to the “More or less engines” group build at whatifmodelers.com in summer 2019.
I actually had the idea of a two-engine J29 in the back of my mind for a long time, spawned by a resin conversion set for the Hasegawa B-47 Stratojet kit that came with new intakes and exhaust sections for the four engine pods. The single engine pod parts had been spent a long time ago, but the twin engine parts were still waiting for a good use. Could the exhaust fit under/into a Tunnan…?
I even had a Matchbox J29 stashed away for this experiment long ago, as well as some donor parts like the wings, and the GB eventually offered the right motivation to put those things together that no one would expect to work.
So I pulled out all the stuff and started – a rather straightforward affair. Work started with the fuselage, which was, together with the (very nice) cockpit assembled OOB at first, the nose filled with as much lead as possible and with the lower rear section cut away, so the B-47 resin jet nozzles would end up at the same position as the original RM2B exhaust. Due to the pen nib fairing between them, though, the profile of the modified tail became (visually) more massive, and I had to fill some gaps under the tail boom (with styrene sheet and putty). The twin engines also turned out to be wider than expected – I had hoped for straight flanks, but the fuselage shape ended up with considerable bulges behind the landing gear wells. These were created with parts from drop tank halves and blended into the rest of the lower hill with PSR work. In the same wake the area under the fin was sculpted and re-created, too.
At that point it became clear that I had to do more on the fuselage, esp. the front end, in order to keep the aircraft visually balance. A convenient solution became an F-100 air intake, which I grafted onto the nose instead of the original circular and round-lipped orifice – with its sharp lip the Super Sabre piece was even a plausible change! The fuselage shapes and diameters differed considerably, though, more PSR became necessary.
Next came the wings: I had already set apart a pair of trapezoid wings with a 45° sweep angle – these were left over from a PM Model Ta 183 conversion some time ago. With their odd shape and size they were a perfect match for my project, even more so due to the fact that I could keep the original J29 wing attachment points, I just had to shorten and modify the trailing edge area on the fuselage. The result was very conclusive.
With the new nose and the wings in place, the overall proportions became clearer: still tail-heavy, but not unpleasant. At this time I was also certain that I had to modify the tail surfaces. The fin was too small and did not have enough sweep for the overall look, and the stabilizer, with its thick profile, rounded edges and the single, continuous rudder did not look supersonic at all. What followed was a long search in the donor banks for suitable replacements, and I eventually came up with a MiG-15 fin (Hobby Boss) which was later clipped at the top for a less recognizable profile. The stabilizers were more challenging, though. My solution eventually became a pair of modified stabilizers from a Matchbox Buccaneer(!), attached to the MiG-15 fin.
The design problems did not stop here, though: the landing gear caused some more headaches. I wanted to keep the OOB parts, but especially the main legs would leave the aircraft with a very goofy look through a short wheelbase and a rear axis position too much forward. In an attempt to save the situation I attached swing arms to the OOB struts, moving the axis maybe 5mm backwards and widening the track by 2mm at the same time. Not much in total, but it helped (a little, even though the aircraft is still very tail-heavy)
As a final addition – since the original, wing-mounted pitots of the J29 were gone now and would not go well with the wing-switching idea – I gave the P29G a large, nose-mounted pitot and sensor boom, placed on top of the nose. This part come, like the air intake, from an F-100.
Painting and markings:
I tend to be conservative when it comes to liveries for what-if models, and the P29G is no exception. At first, I thought that this build could become an operational supersonic daylight interceptor (the J29G), so that I could give the model full military markings and maybe a camouflage paint scheme. However, this idea would not work: the potential real life window for such an aircraft, based on the Saab 29, would be very narrow. And aircraft development in the late Fifties made quantum leaps within a very short period of time: While the J29A entered service, work on the Mach 2 Saab 35 was already underway – nobody would have accepted (or needed) a Mach 1 fighter, based on late Forties technology, at that time anymore, and there was the all-weather Saab J32B around, too. The update program with new wings and a more powerful afterburner engine was all that could be done to exploit the Tunnan’s potential, resulting in the (real world’s) J29E and F variants.
I eventually decided that the J29G would only be a prototype/research aircraft, consequently called P29G, and through this decision I became more or less settled upon a NMF finish with some colorful markings. Consequently, the model was painted with various shades of metal colors, primarily Polished Aluminum Metallizer from Humbrol, but also with Humbrol 191 and Matt Aluminum Metallizer as well as ModelMaster Steel Metallizer. Around the exhaust section, I also used Revell 91 (Iron) and ModelMaster Exhaust Metallizer. Some single panels and details were painted with Revell 99 (Aluminum), and I also used generic decal material in silver to simulate some smaller access panels. Grey decal sheet was used to simulate covers for the cannon nozzles.
The cockpit interior was painted, according to Saab 29 standard, in a dark greenish-grey (Revell 67), and bluish grey was used inside of the landing gear wells (Revell 57). The pitot boom received black and white stripes.
For markings I let myself get inspired from the real world Saab 29 and 32 prototypes, which were all marked with a colored “U” tactical code on the fin and also on the front fuselage, simply meaning “Utverding” (= “Test”). I found four red decals, and I also gave the aircraft a yellow cheatline, lent from an Airfix F-86D decal sheet. The Swedish roundels come from a generic aftermarket sheet, most stencils were taken from the Revell OOB sheet and a Printscale J29 sheet.
Before the model was sealed with semi-gloss acrylic varnish from Italeri, some grinded graphite was rubbed onto the rear fuselage, adding a metallic shine and simulating exhaust stains.
A thorough conversion – this has rather evolved into a kitbashing than just a kit conversion: not much from the original Matchbox J29 has been left over. But I like the outcome, even though things developed gradually from the simple idea of changing the number of engines on the Tunnan. One thing led to another. The resulting aircraft looks quite plausible, even though I am not totally happy with the landing gear, which appears to be rather far forward, despite surgical measures to mend the situation. The Ta 183 wings are a very good match, though, and I cannot help but recognize a certain French look, maybe due to the cruciform tail and the oval air intake? The P29G could also, with Argentinian marking, have become a revised version of the FMA Pulqui II?
Secrets lie deep within Jupiter, shrouded in the solar system's strongest magnetic field and most lethal radiation belts. On July 4, 2016, NASA's Juno spacecraft will plunge into uncharted territory, entering orbit around the gas giant and passing closer than any spacecraft before. Juno will see Jupiter for what it really is, but first it must pass the trial of orbit insertion. For more information: www.nasa.gov/juno and missionjuno.swri.edu
ASSEMBLY OF THE ADDITIVE MANUFACTURING INTEGRATED ENERGY (AMIE) 3D-PRINTED HOUSE.
Oak Ridge National Laboratory combines clean energy technologies into a 3D-printed building and vehicle to showcase a new approach to energy use, storage and consumption. It is a model for energy-efficient systems that link buildings, vehicles and the grid. ORNL team worked with industrial partners to manufacture and connect a natural-gas-powered hybrid electric vehicle with a solar-powered building to create an integrated energy system. The project's energy control center manages the system's electrical demand and load by balancing the intermittent power from the building's 3.2-kilowatt solar array with supplemental power from the vehicle.
For more information or additional images, please contact 202-586-5251.
The San Francisco Muni's 2019 heritage weekend September 7-8 featured the public debut of former Sacramento-Clay Line Car 19, built in 1883 by the Central Pacific Railroad Company in Sacramento. Now fully restored, it is the system's oldest (and largest) operating cable car. The weekend's festivities included public operation of the car on all of the surviving cable lines, including the non-revenue trackage.
More on this car's unique history can be found here: www.sfmta.com/blog/cable-car-19-make-historic-debut-muni-...
NASA Image
Astronomy has merged with Geological Sciences Spacecraft to study Mercury smallest planet,after Pluto planet.
Astronomy has merged with Geological Sciences to make new discovery has been interpreted through a lens that of Geological and Planetary Sciences'rocks are formed under the surface of the earth from the metamorphosis when magma erupts onto the surface from volcanoes
You can see Mercury the solar system’s smallest planet,after Pluto planet.
NASA's Messenger spacecraft slipped into orbit around Mercury on Thursday, 03-17-2011 Late on St. Patrick’s Day, Eastern time, a spacecraft makes historic voyage to Mercury captured by Mercury's gravity should have at least a year of photography become first object to orbit the planet closest to the Sun, so to study the mineralogy of Mercury, mapping its surface and magnetic and gravitational fields spacecraft has accomplished this engineering and scientific milestone at our solar system's to keep the spacecraft on track for its March 2011 orbit insertion, up-close measurements since Mariner 10 spacecraft's third and final flyby on March 16, 1975. When Mariner 10 flew by Mercury in the mid-1970s.
Uploaded by tonynetone on 10 Jul 08, 11.20PM CET.
Uploaded by tonynetone on Thursday, 03-20-2011
Tummel Bridge is a double arched hump-backed former military bridge crossing the River Tummel at Tummel Bridge, Perth & Kinross, Scotland. A Category A listed structure dating to 1730, it is now pedestrian-only. It stands immediately to the southeast of a modern road bridge, which carries the vehicular traffic of today's B846 road. Two worn milestones are at the northern end of the bridge.
Erected for the Board of Ordnance, to the order of Lieutenant General George Wade, its original purpose was as a military road. The Irvine Robertson papers at the National Records of Scotland contain, at GD1/53/97, the construction contract with John Stewart of Canagan [=Kynachan], for building the bridge, and the receipt by John Stewart for £50, in respect of above contract, 27 July 1730, and the bond by him and David Stewart, his eldest son, to maintain the bridge, 20 October 1730:
... the said John Stewart shall Build a Stone Bridge Strengthen'd with a double Arch over the River of Tumble, within less than a mile west of the house of the said Canagan, which Bridge is to have an Arch of at least forty two feet between the landstools for more if the breadth of the River shall require an Arch of a larger dimension. It is likewise to be twelve foot in breadth including the Parapet walls, which Walls are to be three foot high above the pavement, and at least one foot broad, and to be Cap'd with good flag Stones. The whole to be of good materials and well wrought, And to have an access to the same extending so far on both Sides to the Land, as to render it easily passable for Wheel Carriage or Canon, AND LIKEWISE to make sufficient Buttments that shall Confine the Water to pass under the Arch, that in extraordinary Floods it may not damage or undermine the foundation. For which Bridge and all Materials, and Charges relating thereto, the said Lieut General George Wade is to Pay to the said John Stewart, the Sum of two hundred pounds Sterling Viz Fifty pounds on the signing this contact, and one hundred and fifty Pounds as soon as the work is Compleated, which he promises to finish before the last day of October next ensuing, and the said John Stewart does oblige himself to give sufficient Security before the last Payment is made to uphold the said Bridge at his own Expense for the space of twenty years from the date hereof...
The bridge was renovated in 1973, and underwent conservation work in 2011.
The River Tummel is a river in Perth and Kinross, Scotland. Water from the Tummel is used in the Tummel hydro-electric power scheme, operated by SSE.
As a tributary of the River Tay, the Tummel is included as part of the River Tay Special Area of Conservation. The designation notes the river system's importance for salmon, otters, brook lampreys, river lampreys and sea lampreys.
Discharging from Loch Rannoch, it flows east to a point near the Falls of Tummel, where it bends to the southeast, a direction which it maintains until it falls into the River Tay, just below Logierait, after a course of 58 miles (93 km) from its source in Stob Ghabbar (3,565 ft (1,087 m)). Its only considerable affluent is the Garry, 24 miles (39 km) long, an impetuous river which issues from Loch Garry (2.5 mi (4.0 km) and 1,334 ft (407 m) above sea level). Some 2 miles from its outlet from Loch Rannoch the river expands into Dunalastair Water (or Dunalastair Reservoir), a man made loch formed by a weir, part of the Tummel Hydro Electric power scheme. About midway in its course the Tummel expands into Loch Tummel, between which and the confluence with the Garry occur the Pass and Falls of the Tummel, which are rather in the nature of rapids, the descent altogether amounting to 15 ft (4.6 m). Loch Tummel was previously 4.43 km (2.75 mi) long and 39 m (128 ft) deep, but with the construction of the Clunie Dam in 1950, the water level was raised by 4.5 metres, and Loch Tummel is now approximately 11 km (7 mi) long.
The scenery throughout this reach is most picturesque, culminating at the point above the eastern extremity of the loch, known as the "Queen's View" (Queen Victoria made the view famous in 1866, although it is said to have been named after Queen Isabel, wife of Robert the Bruce). The chief places of interest on the river are Kinloch Rannoch; Dunalastair, a rocky hill in well-wooded grounds, the embellishment of which was largely due to Alexander Robertson of Struan, the Jacobite and poet, from whom the spot takes its name (the stronghold of Alexander); Foss; Faskally House (beautifully situated on the left bank); Pitlochry; and Ballinluig.
The ancient name of the river, in its upper reaches at least, was the Dubhag
The Highlands is a historical region of Scotland. Culturally, the Highlands and the Lowlands diverged from the Late Middle Ages into the modern period, when Lowland Scots language replaced Scottish Gaelic throughout most of the Lowlands. The term is also used for the area north and west of the Highland Boundary Fault, although the exact boundaries are not clearly defined, particularly to the east. The Great Glen divides the Grampian Mountains to the southeast from the Northwest Highlands. The Scottish Gaelic name of A' Ghàidhealtachd literally means "the place of the Gaels" and traditionally, from a Gaelic-speaking point of view, includes both the Western Isles and the Highlands.
The area is very sparsely populated, with many mountain ranges dominating the region, and includes the highest mountain in the British Isles, Ben Nevis. During the 18th and early 19th centuries the population of the Highlands rose to around 300,000, but from c. 1841 and for the next 160 years, the natural increase in population was exceeded by emigration (mostly to Canada, the United States, Australia and New Zealand, and migration to the industrial cities of Scotland and England.) and passim The area is now one of the most sparsely populated in Europe. At 9.1/km2 (24/sq mi) in 2012, the population density in the Highlands and Islands is less than one seventh of Scotland's as a whole.
The Highland Council is the administrative body for much of the Highlands, with its administrative centre at Inverness. However, the Highlands also includes parts of the council areas of Aberdeenshire, Angus, Argyll and Bute, Moray, North Ayrshire, Perth and Kinross, Stirling and West Dunbartonshire.
The Scottish Highlands is the only area in the British Isles to have the taiga biome as it features concentrated populations of Scots pine forest: see Caledonian Forest. It is the most mountainous part of the United Kingdom.
Between the 15th century and the mid-20th century, the area differed from most of the Lowlands in terms of language. In Scottish Gaelic, the region is known as the Gàidhealtachd, because it was traditionally the Gaelic-speaking part of Scotland, although the language is now largely confined to The Hebrides. The terms are sometimes used interchangeably but have different meanings in their respective languages. Scottish English (in its Highland form) is the predominant language of the area today, though Highland English has been influenced by Gaelic speech to a significant extent. Historically, the "Highland line" distinguished the two Scottish cultures. While the Highland line broadly followed the geography of the Grampians in the south, it continued in the north, cutting off the north-eastern areas, that is Eastern Caithness, Orkney and Shetland, from the more Gaelic Highlands and Hebrides.
Historically, the major social unit of the Highlands was the clan. Scottish kings, particularly James VI, saw clans as a challenge to their authority; the Highlands was seen by many as a lawless region. The Scots of the Lowlands viewed the Highlanders as backward and more "Irish". The Highlands were seen as the overspill of Gaelic Ireland. They made this distinction by separating Germanic "Scots" English and the Gaelic by renaming it "Erse" a play on Eire. Following the Union of the Crowns, James VI had the military strength to back up any attempts to impose some control. The result was, in 1609, the Statutes of Iona which started the process of integrating clan leaders into Scottish society. The gradual changes continued into the 19th century, as clan chiefs thought of themselves less as patriarchal leaders of their people and more as commercial landlords. The first effect on the clansmen who were their tenants was the change to rents being payable in money rather than in kind. Later, rents were increased as Highland landowners sought to increase their income. This was followed, mostly in the period 1760–1850, by agricultural improvement that often (particularly in the Western Highlands) involved clearance of the population to make way for large scale sheep farms. Displaced tenants were set up in crofting communities in the process. The crofts were intended not to provide all the needs of their occupiers; they were expected to work in other industries such as kelping and fishing. Crofters came to rely substantially on seasonal migrant work, particularly in the Lowlands. This gave impetus to the learning of English, which was seen by many rural Gaelic speakers to be the essential "language of work".
Older historiography attributes the collapse of the clan system to the aftermath of the Jacobite risings. This is now thought less influential by historians. Following the Jacobite rising of 1745 the British government enacted a series of laws to try to suppress the clan system, including bans on the bearing of arms and the wearing of tartan, and limitations on the activities of the Scottish Episcopal Church. Most of this legislation was repealed by the end of the 18th century as the Jacobite threat subsided. There was soon a rehabilitation of Highland culture. Tartan was adopted for Highland regiments in the British Army, which poor Highlanders joined in large numbers in the era of the Revolutionary and Napoleonic Wars (1790–1815). Tartan had largely been abandoned by the ordinary people of the region, but in the 1820s, tartan and the kilt were adopted by members of the social elite, not just in Scotland, but across Europe. The international craze for tartan, and for idealising a romanticised Highlands, was set off by the Ossian cycle, and further popularised by the works of Walter Scott. His "staging" of the visit of King George IV to Scotland in 1822 and the king's wearing of tartan resulted in a massive upsurge in demand for kilts and tartans that could not be met by the Scottish woollen industry. Individual clan tartans were largely designated in this period and they became a major symbol of Scottish identity. This "Highlandism", by which all of Scotland was identified with the culture of the Highlands, was cemented by Queen Victoria's interest in the country, her adoption of Balmoral as a major royal retreat, and her interest in "tartenry".
Recurrent famine affected the Highlands for much of its history, with significant instances as late as 1817 in the Eastern Highlands and the early 1850s in the West. Over the 18th century, the region had developed a trade of black cattle into Lowland markets, and this was balanced by imports of meal into the area. There was a critical reliance on this trade to provide sufficient food, and it is seen as an essential prerequisite for the population growth that started in the 18th century. Most of the Highlands, particularly in the North and West was short of the arable land that was essential for the mixed, run rig based, communal farming that existed before agricultural improvement was introduced into the region.[a] Between the 1760s and the 1830s there was a substantial trade in unlicensed whisky that had been distilled in the Highlands. Lowland distillers (who were not able to avoid the heavy taxation of this product) complained that Highland whisky made up more than half the market. The development of the cattle trade is taken as evidence that the pre-improvement Highlands was not an immutable system, but did exploit the economic opportunities that came its way. The illicit whisky trade demonstrates the entrepreneurial ability of the peasant classes.
Agricultural improvement reached the Highlands mostly over the period 1760 to 1850. Agricultural advisors, factors, land surveyors and others educated in the thinking of Adam Smith were keen to put into practice the new ideas taught in Scottish universities. Highland landowners, many of whom were burdened with chronic debts, were generally receptive to the advice they offered and keen to increase the income from their land. In the East and South the resulting change was similar to that in the Lowlands, with the creation of larger farms with single tenants, enclosure of the old run rig fields, introduction of new crops (such as turnips), land drainage and, as a consequence of all this, eviction, as part of the Highland clearances, of many tenants and cottars. Some of those cleared found employment on the new, larger farms, others moved to the accessible towns of the Lowlands.
In the West and North, evicted tenants were usually given tenancies in newly created crofting communities, while their former holdings were converted into large sheep farms. Sheep farmers could pay substantially higher rents than the run rig farmers and were much less prone to falling into arrears. Each croft was limited in size so that the tenants would have to find work elsewhere. The major alternatives were fishing and the kelp industry. Landlords took control of the kelp shores, deducting the wages earned by their tenants from the rent due and retaining the large profits that could be earned at the high prices paid for the processed product during the Napoleonic wars.
When the Napoleonic wars finished in 1815, the Highland industries were affected by the return to a peacetime economy. The price of black cattle fell, nearly halving between 1810 and the 1830s. Kelp prices had peaked in 1810, but reduced from £9 a ton in 1823 to £3 13s 4d a ton in 1828. Wool prices were also badly affected. This worsened the financial problems of debt-encumbered landlords. Then, in 1846, potato blight arrived in the Highlands, wiping out the essential subsistence crop for the overcrowded crofting communities. As the famine struck, the government made clear to landlords that it was their responsibility to provide famine relief for their tenants. The result of the economic downturn had been that a large proportion of Highland estates were sold in the first half of the 19th century. T M Devine points out that in the region most affected by the potato famine, by 1846, 70 per cent of the landowners were new purchasers who had not owned Highland property before 1800. More landlords were obliged to sell due to the cost of famine relief. Those who were protected from the worst of the crisis were those with extensive rental income from sheep farms. Government loans were made available for drainage works, road building and other improvements and many crofters became temporary migrants – taking work in the Lowlands. When the potato famine ceased in 1856, this established a pattern of more extensive working away from the Highlands.
The unequal concentration of land ownership remained an emotional and controversial subject, of enormous importance to the Highland economy, and eventually became a cornerstone of liberal radicalism. The poor crofters were politically powerless, and many of them turned to religion. They embraced the popularly oriented, fervently evangelical Presbyterian revival after 1800. Most joined the breakaway "Free Church" after 1843. This evangelical movement was led by lay preachers who themselves came from the lower strata, and whose preaching was implicitly critical of the established order. The religious change energised the crofters and separated them from the landlords; it helped prepare them for their successful and violent challenge to the landlords in the 1880s through the Highland Land League. Violence erupted, starting on the Isle of Skye, when Highland landlords cleared their lands for sheep and deer parks. It was quietened when the government stepped in, passing the Crofters' Holdings (Scotland) Act, 1886 to reduce rents, guarantee fixity of tenure, and break up large estates to provide crofts for the homeless. This contrasted with the Irish Land War underway at the same time, where the Irish were intensely politicised through roots in Irish nationalism, while political dimensions were limited. In 1885 three Independent Crofter candidates were elected to Parliament, which listened to their pleas. The results included explicit security for the Scottish smallholders in the "crofting counties"; the legal right to bequeath tenancies to descendants; and the creation of a Crofting Commission. The Crofters as a political movement faded away by 1892, and the Liberal Party gained their votes.
Today, the Highlands are the largest of Scotland's whisky producing regions; the relevant area runs from Orkney to the Isle of Arran in the south and includes the northern isles and much of Inner and Outer Hebrides, Argyll, Stirlingshire, Arran, as well as sections of Perthshire and Aberdeenshire. (Other sources treat The Islands, except Islay, as a separate whisky producing region.) This massive area has over 30 distilleries, or 47 when the Islands sub-region is included in the count. According to one source, the top five are The Macallan, Glenfiddich, Aberlour, Glenfarclas and Balvenie. While Speyside is geographically within the Highlands, that region is specified as distinct in terms of whisky productions. Speyside single malt whiskies are produced by about 50 distilleries.
According to Visit Scotland, Highlands whisky is "fruity, sweet, spicy, malty". Another review states that Northern Highlands single malt is "sweet and full-bodied", the Eastern Highlands and Southern Highlands whiskies tend to be "lighter in texture" while the distilleries in the Western Highlands produce single malts with a "much peatier influence".
The Scottish Reformation achieved partial success in the Highlands. Roman Catholicism remained strong in some areas, owing to remote locations and the efforts of Franciscan missionaries from Ireland, who regularly came to celebrate Mass. There remain significant Catholic strongholds within the Highlands and Islands such as Moidart and Morar on the mainland and South Uist and Barra in the southern Outer Hebrides. The remoteness of the region and the lack of a Gaelic-speaking clergy undermined the missionary efforts of the established church. The later 18th century saw somewhat greater success, owing to the efforts of the SSPCK missionaries and to the disruption of traditional society after the Battle of Culloden in 1746. In the 19th century, the evangelical Free Churches, which were more accepting of Gaelic language and culture, grew rapidly, appealing much more strongly than did the established church.
For the most part, however, the Highlands are considered predominantly Protestant, belonging to the Church of Scotland. In contrast to the Catholic southern islands, the northern Outer Hebrides islands (Lewis, Harris and North Uist) have an exceptionally high proportion of their population belonging to the Protestant Free Church of Scotland or the Free Presbyterian Church of Scotland. The Outer Hebrides have been described as the last bastion of Calvinism in Britain and the Sabbath remains widely observed. Inverness and the surrounding area has a majority Protestant population, with most locals belonging to either The Kirk or the Free Church of Scotland. The church maintains a noticeable presence within the area, with church attendance notably higher than in other parts of Scotland. Religion continues to play an important role in Highland culture, with Sabbath observance still widely practised, particularly in the Hebrides.
In traditional Scottish geography, the Highlands refers to that part of Scotland north-west of the Highland Boundary Fault, which crosses mainland Scotland in a near-straight line from Helensburgh to Stonehaven. However the flat coastal lands that occupy parts of the counties of Nairnshire, Morayshire, Banffshire and Aberdeenshire are often excluded as they do not share the distinctive geographical and cultural features of the rest of the Highlands. The north-east of Caithness, as well as Orkney and Shetland, are also often excluded from the Highlands, although the Hebrides are usually included. The Highland area, as so defined, differed from the Lowlands in language and tradition, having preserved Gaelic speech and customs centuries after the anglicisation of the latter; this led to a growing perception of a divide, with the cultural distinction between Highlander and Lowlander first noted towards the end of the 14th century. In Aberdeenshire, the boundary between the Highlands and the Lowlands is not well defined. There is a stone beside the A93 road near the village of Dinnet on Royal Deeside which states 'You are now in the Highlands', although there are areas of Highland character to the east of this point.
A much wider definition of the Highlands is that used by the Scotch whisky industry. Highland single malts are produced at distilleries north of an imaginary line between Dundee and Greenock, thus including all of Aberdeenshire and Angus.
Inverness is regarded as the Capital of the Highlands, although less so in the Highland parts of Aberdeenshire, Angus, Perthshire and Stirlingshire which look more to Aberdeen, Dundee, Perth, and Stirling as their commercial centres.
The Highland Council area, created as one of the local government regions of Scotland, has been a unitary council area since 1996. The council area excludes a large area of the southern and eastern Highlands, and the Western Isles, but includes Caithness. Highlands is sometimes used, however, as a name for the council area, as in the former Highlands and Islands Fire and Rescue Service. Northern is also used to refer to the area, as in the former Northern Constabulary. These former bodies both covered the Highland council area and the island council areas of Orkney, Shetland and the Western Isles.
Much of the Highlands area overlaps the Highlands and Islands area. An electoral region called Highlands and Islands is used in elections to the Scottish Parliament: this area includes Orkney and Shetland, as well as the Highland Council local government area, the Western Isles and most of the Argyll and Bute and Moray local government areas. Highlands and Islands has, however, different meanings in different contexts. It means Highland (the local government area), Orkney, Shetland, and the Western Isles in Highlands and Islands Fire and Rescue Service. Northern, as in Northern Constabulary, refers to the same area as that covered by the fire and rescue service.
There have been trackways from the Lowlands to the Highlands since prehistoric times. Many traverse the Mounth, a spur of mountainous land that extends from the higher inland range to the North Sea slightly north of Stonehaven. The most well-known and historically important trackways are the Causey Mounth, Elsick Mounth, Cryne Corse Mounth and Cairnamounth.
Although most of the Highlands is geographically on the British mainland, it is somewhat less accessible than the rest of Britain; thus most UK couriers categorise it separately, alongside Northern Ireland, the Isle of Man, and other offshore islands. They thus charge additional fees for delivery to the Highlands, or exclude the area entirely. While the physical remoteness from the largest population centres inevitably leads to higher transit cost, there is confusion and consternation over the scale of the fees charged and the effectiveness of their communication, and the use of the word Mainland in their justification. Since the charges are often based on postcode areas, many far less remote areas, including some which are traditionally considered part of the lowlands, are also subject to these charges. Royal Mail is the only delivery network bound by a Universal Service Obligation to charge a uniform tariff across the UK. This, however, applies only to mail items and not larger packages which are dealt with by its Parcelforce division.
The Highlands lie to the north and west of the Highland Boundary Fault, which runs from Arran to Stonehaven. This part of Scotland is largely composed of ancient rocks from the Cambrian and Precambrian periods which were uplifted during the later Caledonian Orogeny. Smaller formations of Lewisian gneiss in the northwest are up to 3 billion years old. The overlying rocks of the Torridon Sandstone form mountains in the Torridon Hills such as Liathach and Beinn Eighe in Wester Ross.
These foundations are interspersed with many igneous intrusions of a more recent age, the remnants of which have formed mountain massifs such as the Cairngorms and the Cuillin of Skye. A significant exception to the above are the fossil-bearing beds of Old Red Sandstone found principally along the Moray Firth coast and partially down the Highland Boundary Fault. The Jurassic beds found in isolated locations on Skye and Applecross reflect the complex underlying geology. They are the original source of much North Sea oil. The Great Glen is formed along a transform fault which divides the Grampian Mountains to the southeast from the Northwest Highlands.
The entire region was covered by ice sheets during the Pleistocene ice ages, save perhaps for a few nunataks. The complex geomorphology includes incised valleys and lochs carved by the action of mountain streams and ice, and a topography of irregularly distributed mountains whose summits have similar heights above sea-level, but whose bases depend upon the amount of denudation to which the plateau has been subjected in various places.
Climate
The region is much warmer than other areas at similar latitudes (such as Kamchatka in Russia, or Labrador in Canada) because of the Gulf Stream making it cool, damp and temperate. The Köppen climate classification is "Cfb" at low altitudes, then becoming "Cfc", "Dfc" and "ET" at higher altitudes.
Places of interest
An Teallach
Aonach Mòr (Nevis Range ski centre)
Arrochar Alps
Balmoral Castle
Balquhidder
Battlefield of Culloden
Beinn Alligin
Beinn Eighe
Ben Cruachan hydro-electric power station
Ben Lomond
Ben Macdui (second highest mountain in Scotland and UK)
Ben Nevis (highest mountain in Scotland and UK)
Cairngorms National Park
Cairngorm Ski centre near Aviemore
Cairngorm Mountains
Caledonian Canal
Cape Wrath
Carrick Castle
Castle Stalker
Castle Tioram
Chanonry Point
Conic Hill
Culloden Moor
Dunadd
Duart Castle
Durness
Eilean Donan
Fingal's Cave (Staffa)
Fort George
Glen Coe
Glen Etive
Glen Kinglas
Glen Lyon
Glen Orchy
Glenshee Ski Centre
Glen Shiel
Glen Spean
Glenfinnan (and its railway station and viaduct)
Grampian Mountains
Hebrides
Highland Folk Museum – The first open-air museum in the UK.
Highland Wildlife Park
Inveraray Castle
Inveraray Jail
Inverness Castle
Inverewe Garden
Iona Abbey
Isle of Staffa
Kilchurn Castle
Kilmartin Glen
Liathach
Lecht Ski Centre
Loch Alsh
Loch Ard
Loch Awe
Loch Assynt
Loch Earn
Loch Etive
Loch Fyne
Loch Goil
Loch Katrine
Loch Leven
Loch Linnhe
Loch Lochy
Loch Lomond
Loch Lomond and the Trossachs National Park
Loch Lubnaig
Loch Maree
Loch Morar
Loch Morlich
Loch Ness
Loch Nevis
Loch Rannoch
Loch Tay
Lochranza
Luss
Meall a' Bhuiridh (Glencoe Ski Centre)
Scottish Sea Life Sanctuary at Loch Creran
Rannoch Moor
Red Cuillin
Rest and Be Thankful stretch of A83
River Carron, Wester Ross
River Spey
River Tay
Ross and Cromarty
Smoo Cave
Stob Coire a' Chàirn
Stac Polly
Strathspey Railway
Sutherland
Tor Castle
Torridon Hills
Urquhart Castle
West Highland Line (scenic railway)
West Highland Way (Long-distance footpath)
Wester Ross
+++ 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!
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+++ 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!
A billboard in Times Square displays a Windows error screen stating that the system's virus definitions are outdated. And some billboard IT guy needs a talking to... this has been showing up for a month! Original photo from Almost Sober.
Release Date: December 21, 2011
The crater at the center of this image is named Dickens, after Charles Dickens, the English novelist who lived from 1812 to 1870. Among Dickens' famous works is A Christmas Carol, the story of Bob Cratchit, his family, and horrible boss Mr. Scrooge. Scientists studying Mercury might consider the Mariner 10 mission to be Christmas Past, MESSENGER to be Christmas Present, and the European Bepi-Colombo mission to be Christmas Yet To Come.
This image was acquired as part of MDIS's high-resolution surface morphology base map. The surface morphology base map will cover more than 90% of Mercury's surface with an average resolution of 250 meters/pixel (0.16 miles/pixel or 820 feet/pixel). Images acquired for the surface morphology base map typically have off-vertical Sun angles (i.e., high incidence angles) and visible shadows so as to reveal clearly the topographic form of geologic features.
The MESSENGER spacecraft is the first ever to orbit the planet Mercury, and the spacecraft's seven scientific instruments and radio science investigation are unraveling the history and evolution of the Solar System's innermost planet. Visit the Why Mercury? section of this website to learn more about the key science questions that the MESSENGER mission is addressing. During the one-year primary mission, MDIS is scheduled to acquire more than 75,000 images in support of MESSENGER's science goals.
Credit: NASA/Johns Hopkins University Applied Physics Laboratory/Carnegie Institution of Washington
NASA Goddard Space Flight Center enables NASA’s mission through four scientific endeavors: Earth Science, Heliophysics, Solar System Exploration, and Astrophysics. Goddard plays a leading role in NASA’s accomplishments by contributing compelling scientific knowledge to advance the Agency’s mission.
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In the Chihuahuita Barrio. Muni's PCC 1073 matches this El Paso color scheme, one of the system's last before abandonment in 1974. August 16, 2018. © 2018 Peter Ehrlich
Van Damme State Park consists of beach and upland on the Mendocino Coast. Of all the park system's units along the Mendocino coast, Van Damme is perhaps the richest in terms of historical resources connected with the redwood lumber industry. Its story is a prime example of the struggles and eventual failures of a small, independent lumber operation.
Location/Directions
The park is located three miles south of the town of Mendocino on Highway 1. The highway runs through the park separating the campground and the Fern Canyon trail head to the east and the beach and parking lot to the west.
Seasons/Climate - Recommended clothing
The weather can be changeable; layered clothing is recommended.
Facilities - Activities
The park features the lush Fern Canyon scenic trail system; the Pygmy Forest where mature, cone-bearing cypress and pine trees stand six inches to eight feet tall; and the bog, or Cabbage Patch, where skunk cabbage grows in abundance. The park's ten miles of trail go along the fern-carpeted canyon of Little River. A paved road is used by joggers and bicyclists. The beach is popular with abalone divers.
Kayak Tours
Visitors can get a unique perspective of the coast line by taking the kayak tours, available through a concession agreement, at the Van Damme beach parking lot.
About the Park
Van Damme State Park was named for Charles Van Damme who was born at Little River in 1881, son of John and Louise Van Damme, early settlers of the region. John Van Damme and his wife were a Flemish couple. The patriarch of the family was born in Bredene, Belgium on May 22, 1832. New research indicates that John Van Damme was born in Bredene, Belgium, not Ostend. "Following the sea" for some years, Van Damme, upon his arrival in Mendocino County, later worked in the lumber mill at Little River. In this settlement all of his children were born, including Charles, whose love for the area prompted his acquiring, after some years as a successful operator of the Richmond-San Rafael ferry line, a plot of ground along the redwood coast. Upon his demise this area became a part of the State Park System in 1934.
In those early days lumbering was a major economic factor in the development of the northern coastline. Little River was built as a mill town in 1864 by Ruel Stickney, Silas Coombs and Tapping Reeves after the property, formally called Kents Cove, was purchased from W. H. Kent in 1862. Before long it had attained fame, not only as a lumber port, but as a shipyard as well. Alas, a stand of timber, if logged, does not last forever and by the end of the century, even though logging was periodically moved back into the headwaters of Little River, the mill was forced to close in 1893.
What was left of Little River soon deteriorated; the shipyard, the wharf, the town, several chutes for loading lumber and the lumber mill itself. Activity at the port, which once hummed with activity, declined. Little River's school, once attended by nearly 100 students, closed; its weekly steamship service ended, and a shipyard where, in 1874, Captain Thomas Peterson turned out full-size lumber schooners for the coast wide trade, phased out. Only the schooner Little River returned, to be wrecked on the very beach from which it originally departed.
Plagued by a lack of sufficient timber reserves, fires, substantial loss of business and trade, deterioration of the port's chutes and wharf, the end of coast wide shipping and the attendant decline in population, Little River reverted to a natural state. Its acquisition by the State Park System in 1934, and the subsequent addition of peripheral lands has preserved some of California's most interesting natural resources.
A former Conrail/PC/NH/VGN E33 sits in GE Transportation System's back lot adjacent to a former BCOL M630 in July 1991.
Rainy & windy weather was observed late this afternoon in San Jose, CA. Locally stronger gusts were witnessed. I miss this weather... It feels like it's been forever since I've seen rain!
Weather scenario/details:
At last, rain was finally making a return to California after a very dry February! Certainly, we were in for a lot of it! Although we were still in a drought, all this rain equals hazardous conditions... It may be too much of a good thing...
Here's a weather rundown: Why the sudden rains? An atmospheric river event was in store for California for early March 2016... Despite a very dry and mild February, a major pattern change toward a much wetter weather pattern was imminent. The 1st strong system of the series had hit by the first weekend of the month, bringing heavy rain, gusty winds, and heavy mountain snow. Wind & flood advisories were also issued with the first system of the series. The 1st system's strong cold front had approached the Bay Area by Saturday afternoon. Strong southerly winds have developed as the front passed thru. While this rain was to help replenish depleted water reservoirs and put a dent in the long-standing drought, the large amount of rain in a short time frame would lead to flooding and mudslides. Despite its drawbacks, the rainfall was beneficial to the state's water supply. Impacts from the 1st strong system had brought heavy rain & wind to my area in San Jose, CA. The 2nd system was expected to arrive by Sunday night and into Monday. At the time, the 2nd system appeared a bit stronger, bringing in more heavy rain, according to forecasters. Looks like this was El Nino's last hurrah this winter! Is a 'Miracle-March' imminent? Drive safe & stay dry out there, guys.
(Footage filmed Saturday, March 5, 2016 from around San Jose, CA)
With the lightweight aluminium front and rear axles from the BMW M3/M4 models, forged 19-inch aluminium wheels with mixed-size tyres, M Servotronic steering with two settings and suitably effective M compound brakes, the new BMW M2 Coupe has raised the bar once again in the compact high-performance sports car segment when it comes to driving dynamics. The electronically controlled Active M Differential, which optimises traction and directional stability, also plays a significant role here. And even greater driving pleasure is on the cards when the Dynamic Stability Control system’s M Dynamic Mode (MDM) is activated. MDM allows wheel slip and therefore moderate, controlled drifts on the track.
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Rainy weather was observed late this afternoon in San Jose, CA. A strong weather system was ushering in widespread moderate to heavy rainfall (and wind) to the area. I miss this weather... It feels like it's been forever since I've seen rain!
Weather scenario/details:
At last, rain was finally making a return to California after a very dry February! Certainly, we were in for a lot of it! Although we were still in a drought, all this rain equals hazardous conditions... It may be too much of a good thing...
Here's a weather rundown: Why the sudden rains? An atmospheric river event was in store for California for early March 2016... Despite a very dry and mild February, a major pattern change toward a much wetter weather pattern was imminent. The 1st strong system of the series had hit by the first weekend of the month, bringing heavy rain, gusty winds, and heavy mountain snow. Wind & flood advisories were also issued with the first system of the series. The 1st system's strong cold front had approached the Bay Area by Saturday afternoon. Strong southerly winds have developed as the front passed thru. While this rain was to help replenish depleted water reservoirs and put a dent in the long-standing drought, the large amount of rain in a short time frame would lead to flooding and mudslides. Despite its drawbacks, the rainfall was beneficial to the state's water supply. Impacts from the 1st strong system had brought heavy rain & wind to my area in San Jose, CA. The 2nd system was expected to arrive by Sunday night and into Monday. At the time, the 2nd system appeared a bit stronger, bringing in more heavy rain, according to forecasters. Looks like this was El Nino's last hurrah this winter! Is a 'Miracle-March' imminent? Drive safe & stay dry out there, guys.
(Footage filmed Saturday, March 5, 2016 from around San Jose, CA)
ADDITIVE MANUFACTURING INTEGRATED ENERGY (AMIE) DEMONSTRATION PROJECT.
Oak Ridge National Laboratory combines clean energy technologies into a 3D-printed building and vehicle to showcase a new approach to energy use, storage and consumption. It is a model for energy-efficient systems that link buildings, vehicles and the grid. ORNL team worked with industrial partners to manufacture and connect a natural-gas-powered hybrid electric vehicle with a solar-powered building to create an integrated energy system. The project's energy control center manages the system's electrical demand and load by balancing the intermittent power from the building's 3.2-kilowatt solar array with supplemental power from the vehicle.
For more information or additional images, please contact 202-586-5251.
This is the brand new Raspberry Pi 3 - as a cross eye 3D picture.
The Raspberry Pi is a mini computer for less than $40, which was invented to give kids a chance to learn about programming and electronics for cheap. In the 1980s, we had the VIC-20 and the C64 for learning about programming and computers at a low level and I think, at that time, I have practiced the basics, that I use in my job as an engineer every day. www.raspberrypi.org/
The Raspberry Pi 3 is the new flagship of the family. It has 64 bit quad-core processor running @ 1200MHz. It has on board Wifi and Bluetooth and 1GB RAM. The operating system(s) is installed on a micro SD card. That can be Raspbian, which is a Linux derivate.
The Raspberry Pis have a huge impact on the maker scene, one can build things like a media center, maybe robots, 3D printers, etc. etc. pp. with it. I have bought the first one about 4 years ago.
Directions for cross eye 3D: Look cross-eyed at the picture until you see three pictures, in the middle the two pictures are overlapping, here you can see it three dimensional.
The image above shows a stereographic projection of a mosaic centered on Mercury's north pole. This mosaic is made up of MDIS images acquired during its monochrome, color, monochrome stereo, high-incidence, albedo, three-color, and northern polar campaigns. Above 85 degrees north, the approximate location of the center of Prokofiev crater, many images were averaged together in order to obtain a mostly sunlit mosaic. Permanently shadowed craters at Mercury's poles are host to radar-bright deposits. Tune in on Thursday, November 29, to a NASA news conference about exciting new science results about Mercury's polar regions.
The MESSENGER spacecraft is the first ever to orbit the planet Mercury, and the spacecraft's seven scientific instruments and radio science investigation are unraveling the history and evolution of the Solar System's innermost planet. Visit the Why Mercury? section of this website to learn more about the key science questions that the MESSENGER mission is addressing. During the one-year primary mission, MESSENGER acquired 88,746 images and extensive other data sets. MESSENGER is now in a yearlong extended mission, during which plans call for the acquisition of more than 80,000 additional images to support MESSENGER's science goals.
Credit: NASA/Johns Hopkins University Applied Physics Laboratory/Carnegie Institution of Washington
NASA Goddard Space Flight Center enables NASA’s mission through four scientific endeavors: Earth Science, Heliophysics, Solar System Exploration, and Astrophysics. Goddard plays a leading role in NASA’s accomplishments by contributing compelling scientific knowledge to advance the Agency’s mission.
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Citi Bike is a privately owned public bicycle sharing system serving the New York City boroughs of the Bronx, Brooklyn, Manhattan, and Queens, as well as Jersey City, New Jersey. Named after lead sponsor Citigroup, it was operated by Motivate (formerly Alta Bicycle Share), with former Metropolitan Transportation Authority CEO Jay Walder as chief executive until September 30, 2018 when the company was acquired by Lyft. The system's bikes and stations use technology from Lyft.
--- wikipedia
On May 19, 2023, the Potomac Yard VT Metro station opened in Alexandria, Va. It is the city's 5th station and system's 98th overall.
Read more: New Potomac Yard Metro is Alexandria’s 5th and WMATA’s 98th station
Van Damme State Park consists of beach and upland on the Mendocino Coast. Of all the park system's units along the Mendocino coast, Van Damme is perhaps the richest in terms of historical resources connected with the redwood lumber industry. Its story is a prime example of the struggles and eventual failures of a small, independent lumber operation.
Location/Directions
The park is located three miles south of the town of Mendocino on Highway 1. The highway runs through the park separating the campground and the Fern Canyon trail head to the east and the beach and parking lot to the west.
Seasons/Climate - Recommended clothing
The weather can be changeable; layered clothing is recommended.
Facilities - Activities
The park features the lush Fern Canyon scenic trail system; the Pygmy Forest where mature, cone-bearing cypress and pine trees stand six inches to eight feet tall; and the bog, or Cabbage Patch, where skunk cabbage grows in abundance. The park's ten miles of trail go along the fern-carpeted canyon of Little River. A paved road is used by joggers and bicyclists. The beach is popular with abalone divers.
Kayak Tours
Visitors can get a unique perspective of the coast line by taking the kayak tours, available through a concession agreement, at the Van Damme beach parking lot.
About the Park
Van Damme State Park was named for Charles Van Damme who was born at Little River in 1881, son of John and Louise Van Damme, early settlers of the region. John Van Damme and his wife were a Flemish couple. The patriarch of the family was born in Bredene, Belgium on May 22, 1832. New research indicates that John Van Damme was born in Bredene, Belgium, not Ostend. "Following the sea" for some years, Van Damme, upon his arrival in Mendocino County, later worked in the lumber mill at Little River. In this settlement all of his children were born, including Charles, whose love for the area prompted his acquiring, after some years as a successful operator of the Richmond-San Rafael ferry line, a plot of ground along the redwood coast. Upon his demise this area became a part of the State Park System in 1934.
In those early days lumbering was a major economic factor in the development of the northern coastline. Little River was built as a mill town in 1864 by Ruel Stickney, Silas Coombs and Tapping Reeves after the property, formally called Kents Cove, was purchased from W. H. Kent in 1862. Before long it had attained fame, not only as a lumber port, but as a shipyard as well. Alas, a stand of timber, if logged, does not last forever and by the end of the century, even though logging was periodically moved back into the headwaters of Little River, the mill was forced to close in 1893.
What was left of Little River soon deteriorated; the shipyard, the wharf, the town, several chutes for loading lumber and the lumber mill itself. Activity at the port, which once hummed with activity, declined. Little River's school, once attended by nearly 100 students, closed; its weekly steamship service ended, and a shipyard where, in 1874, Captain Thomas Peterson turned out full-size lumber schooners for the coast wide trade, phased out. Only the schooner Little River returned, to be wrecked on the very beach from which it originally departed.
Plagued by a lack of sufficient timber reserves, fires, substantial loss of business and trade, deterioration of the port's chutes and wharf, the end of coast wide shipping and the attendant decline in population, Little River reverted to a natural state. Its acquisition by the State Park System in 1934, and the subsequent addition of peripheral lands has preserved some of California's most interesting natural resources.
This image is excerpted from a U.S. GAO report:
www.gao.gov/products/GAO-16-127
AIR TRAVEL AND COMMUNICABLE DISEASES: Comprehensive Federal Plan Needed for U.S. Aviation System's Preparedness
a) Central and South America region includes the Caribbean.
Van Damme State Park consists of beach and upland on the Mendocino Coast. Of all the park system's units along the Mendocino coast, Van Damme is perhaps the richest in terms of historical resources connected with the redwood lumber industry. Its story is a prime example of the struggles and eventual failures of a small, independent lumber operation.
Location/Directions
The park is located three miles south of the town of Mendocino on Highway 1. The highway runs through the park separating the campground and the Fern Canyon trail head to the east and the beach and parking lot to the west.
Seasons/Climate - Recommended clothing
The weather can be changeable; layered clothing is recommended.
Facilities - Activities
The park features the lush Fern Canyon scenic trail system; the Pygmy Forest where mature, cone-bearing cypress and pine trees stand six inches to eight feet tall; and the bog, or Cabbage Patch, where skunk cabbage grows in abundance. The park's ten miles of trail go along the fern-carpeted canyon of Little River. A paved road is used by joggers and bicyclists. The beach is popular with abalone divers.
Kayak Tours
Visitors can get a unique perspective of the coast line by taking the kayak tours, available through a concession agreement, at the Van Damme beach parking lot.
About the Park
Van Damme State Park was named for Charles Van Damme who was born at Little River in 1881, son of John and Louise Van Damme, early settlers of the region. John Van Damme and his wife were a Flemish couple. The patriarch of the family was born in Bredene, Belgium on May 22, 1832. New research indicates that John Van Damme was born in Bredene, Belgium, not Ostend. "Following the sea" for some years, Van Damme, upon his arrival in Mendocino County, later worked in the lumber mill at Little River. In this settlement all of his children were born, including Charles, whose love for the area prompted his acquiring, after some years as a successful operator of the Richmond-San Rafael ferry line, a plot of ground along the redwood coast. Upon his demise this area became a part of the State Park System in 1934.
In those early days lumbering was a major economic factor in the development of the northern coastline. Little River was built as a mill town in 1864 by Ruel Stickney, Silas Coombs and Tapping Reeves after the property, formally called Kents Cove, was purchased from W. H. Kent in 1862. Before long it had attained fame, not only as a lumber port, but as a shipyard as well. Alas, a stand of timber, if logged, does not last forever and by the end of the century, even though logging was periodically moved back into the headwaters of Little River, the mill was forced to close in 1893.
What was left of Little River soon deteriorated; the shipyard, the wharf, the town, several chutes for loading lumber and the lumber mill itself. Activity at the port, which once hummed with activity, declined. Little River's school, once attended by nearly 100 students, closed; its weekly steamship service ended, and a shipyard where, in 1874, Captain Thomas Peterson turned out full-size lumber schooners for the coast wide trade, phased out. Only the schooner Little River returned, to be wrecked on the very beach from which it originally departed.
Plagued by a lack of sufficient timber reserves, fires, substantial loss of business and trade, deterioration of the port's chutes and wharf, the end of coast wide shipping and the attendant decline in population, Little River reverted to a natural state. Its acquisition by the State Park System in 1934, and the subsequent addition of peripheral lands has preserved some of California's most interesting natural resources.
Observations by ESO’s planet-finding instrument, SPHERE, a high-contrast adaptive optics system installed on the third Unit Telescope of ESO’s Very Large Telescope, have revealed the edge-on disc of gas and dust present around the binary star system HD 106906AB.
HD 106906AB is a double star located in the constellation of Crux (The Southern Cross). Astronomers had long suspected that this 13 million-year-old stellar duo was encircled by a debris disc, due to the system’s youth and characteristic radiation. However, this disc had remained unseen — until now! The system’s spectacular debris disc can be seen towards the lower left area of this image. It is surrounding both stars, hence its name of circumbinary disc. The stars themselves are hidden behind a mask which prevent their glare from blinding the instrument.
These stars and the disc are also accompanied by an exoplanet, visible in the upper right, named HD 106906 b, which orbits around the binary star and its disc at a distance greater than any other exoplanet discovered to date — 650 times the average Earth–Sun distance, or nearly 97 billion kilometres. HD 106906 b has a mammoth mass of up to 11 times that of Jupiter, and a scorching surface temperature of 1500 degrees Celsius.
Thanks to SPHERE, HD 106906AB has become the first binary star system to have both an exoplanet and a debris disc successfully imaged, providing astronomers with a unique opportunity to study the complex process of circumbinary planet formation.
More information: www.eso.org/public/images/potw1543a/
Credit:
ESO, A. M. Lagrange (Université Grenoble Alpes)
NASA astronaut Doug Hurley and chief of the astronaut office Pat Forrester watch the launch of a SpaceX Falcon 9 rocket carrying the company's Crew Dragon spacecraft on the Demo-1 mission from firing room four of the Launch Control Center, Saturday, March 2, 2019 at the Kennedy Space Center in Florida. The Demo-1 mission will be the first launch of a commercially built and operated American spacecraft and space system designed for humans as part of NASA's Commercial Crew Program. The mission will serve as an end-to-end test of the system's capabilities. Photo Credit: (NASA/Joel Kowsky)
With the lightweight aluminium front and rear axles from the BMW M3/M4 models, forged 19-inch aluminium wheels with mixed-size tyres, M Servotronic steering with two settings and suitably effective M compound brakes, the new BMW M2 Coupe has raised the bar once again in the compact high-performance sports car segment when it comes to driving dynamics. The electronically controlled Active M Differential, which optimises traction and directional stability, also plays a significant role here. And even greater driving pleasure is on the cards when the Dynamic Stability Control system’s M Dynamic Mode (MDM) is activated. MDM allows wheel slip and therefore moderate, controlled drifts on the track.
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Moscow. MAKS 2011 Airshow.
www.youtube.com/watch?v=rcyCANwAZOQ&feature=related
The S-300 is a series of Russian long range surface-to-air missile systems produced by NPO Almaz, all based on the initial S-300P version. The S-300 system was developed to defend against aircraft and cruise missiles for the Soviet Air Defence Forces. Subsequent variations were developed to intercept ballistic missiles.
The S-300 system was first deployed by the Soviet Union in 1979, designed for the air defense of large industrial and administrative facilities, military bases, and control of airspace against enemy strike aircraft.
The project-managing developer of the S-300 is Russian Almaz corporation (government owned, aka "KB-1") which is currently a part of "Almaz-Antei" Air Defense Concern. S-300 uses missiles developed by MKB "Fakel" design bureau (a separate government corporation, aka "OKB-2").
The S-300 is regarded as one of the most potent anti-aircraft missile systems currently fielded. Its radars have the ability to simultaneously track up to 100 targets while engaging up to 12. S-300 deployment time is five minutes. The S-300 missiles are sealed rounds and require no maintenance over their lifetime. An evolved version of the S-300 system is the S-400 (NATO reporting name SA-21), entering limited service in 2004.
The S-300PMU-1 (Russian С-300ПМУ-1,US DoD designation SA-20A, NATO reporting name SA-20 Gargoyle) was also introduced in 1992 with the new and larger 48N6 missiles for the first time in a land-based system and introduced all the same performance improvements from the S300FM version including the increased speed, range, TVM guidance and ABM capability.[10] The warhead is slightly smaller than the naval version at 143 kg (315 lb). This version also saw the introduction of the new and more capable 30N6E TOMB STONE radar.
The S-300PMU-1 was introduced in 1999 and for the first time introduces several different kinds of missiles in a single system. In addition to the 5V55R, 48N6E and 48N6E2 missiles the S-300PMU-1 can utilise two new missiles, the 9M96E1 and 9M96E2. Both are significantly smaller than the previous missiles at 330 and 420 kg (728 and 926 lb respectively) and carry smaller 24 kg (53 lb) warhead. The 9M96E1 has an engagement range of 1–40 km (1–25 mi) and the 9M96E2 of 1–120 km (1–75 mi). They are still carried 4 per TEL. Rather than just relying on aerodynamic fins for manoeuvring, they use a gas-dynamic system which allows them to have an excellent probability of kill (Pk) despite the much smaller warhead. The Pk is estimated at 0.7 against a tactical ballistic missile for either missile. The S-300PMU-1 typically uses the 83M6E command and control system, although it is also compatible with the older Baikal-1E and Senezh-M1E CCS command and control systems. The 83M6E system incorporates the 64N6E (BIG BIRD) surveillance/detection radar. The fire control/illumination and guidance radar used is the 30N6E, optionally matched with a 76N6 low altitude detection radar and a 96L6E all altitude detection radar. The 83M6E command and control system can control up to 12 TELs, both the self propelled 5P85SE vehicle and the 5P85TE towed launchers. Generally support vehicles are also included, such as the 40V6M tow vehicle, intended for lifting of the antenna post.
S-300PMU-2 vehicles. From left to right: 64N6E2 detection radar, 54K6E2 command post and 5P85 TEL.The S-300PMU-2 Favorite (Russian С-300ПМУ-2 Фаворит – Favourite, DoD designation SA-20B), introduced in 1997, is an upgrade to the S-300PMU-1 with range extended once again to 195 km (121 mi) with the introduction of the 48N6E2 missile. This system is apparently capable against not just short range ballistic missiles, but now also medium range tactical ballistic missiles. It uses the 83M6E2 command and control system, consisting of the 54K6E2 command post vehicle and the 64N6E2 surveillance/detection radar. It employs the 30N6E2 fire control/illumination and guidance radar. Like the S-300PMU-1, 12 TELs can be controlled, with any mix of 5P85SE2 self propelled and 5P85TE2 trailer launchers. Optionally it can make use of the 96L6E all altitude detection radar and 76N6 low altitude detection radar, just like the S-300PMU-1.
A United Launch Alliance Atlas V rocket with Boeing’s CST-100 Starliner spacecraft onboard is seen on the launch pad at Space Launch Complex 41 ahead of the Orbital Flight Test mission, Wednesday, Dec. 18, 2019 at Cape Canaveral Air Force Station in Florida. The Orbital Flight Test with be Starliner’s maiden mission to the International Space Station for NASA's Commercial Crew Program. The mission, currently targeted for a 6:36 a.m. EST launch on Dec. 20, will serve as an end-to-end test of the system's capabilities. Photo Credit: (NASA/Joel Kowsky)
+++ 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 APS-4 was a light-weight, pod-mounted airborne search Radar which was suitable for either Airborne Interception (AI) or Air-to-Surface-Vessel (ASV) applications. It was a member of a series of early air-borne radar equipment and was initially designated as AS-H (“Air-to Surface, version H”). This very advanced equipment for its time was first used by the US Navy on board of carrier-borne night fighter aircraft like respective F6F Hellcat and F4U-2 Corsair variants. The Royal Air Force was impressed enough with the system's performance that it was adopted in 1943 for domestic airframes, too, as an alternative to the British AI radars used on board of early Mosquito, Beaufighter and Defiant night fighters.
One very successful carrier of the APS-4, in RAF service known as the AI Mk XV, was the De Havilland Mosquito in its NF Mk.XIX and NF Mk.30 night fighter incarnations. Aware of the performance and effectiveness of the American single engine aircraft, though, the RAF decided to test similar domestic airframes towards the end of WWII as well. The shorter range of a single engine night fighter would, compared with the bigger but also more sluggish two engine types, be compensated by higher speed, agility and rate of climb. These lighter aircraft were intended as a second defense for homeland defense, esp. around large cities or industrial sites.
One of these projects concerned the Supermarine Spitfire, more specifically the new types powered by a Rolly Royce Griffon engine. The Griffon provided a substantial performance increase over the Merlin-powered Spitfire Mk IX, but initially 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, leading to a slightly modified engine, the 65 series, which was eventually mounted in the Spitfire Mk XIV.
With this performance surplus, a night fighter, despite carrying the AI Mk XV equipment plus a second crew member, was still expected to offer a superior performance over German two-engine bombers that intruded British airspace and the heavy night fighters that lurked over the Channel and attacked grouping RAF night bomber formations before they entered Continental airspace.
From this idea, the Spitfire NF.XX was born, as an alternative to a Hawker Typhoon night fighter with a British radar and only a single crew member. In summer 1944 an initial prototype was built, converted from an early series production Mk. XIV airframe. Since the AI Mk XV came with a rather complicated and voluminous display, a second crew member was deemed necessary for effective operations, esp. at night and under poor visibility conditions. The radio operator would check the radar readings and verbally guide the pilot towards the target, who could concentrate on the flying job and keep the eyes on the surroundings.
In order to fit the equipment and the second crew member into the tight Spitfire airframe, and a separate compartment behind the pilot's cockpit and the real bulkhead was added. This second seat received a separate sliding canopy, resulting in a distinctive camel hump silhouette, which earned the Spitfire NF.XX quickly the nickname 'Camelback'. Supermarine had proposed a new service name for this aircraft, 'Nightfire', but it was not officially accepted, since the machine did not differ enough from the basic Spitfire day fighter to justify a completely new designation.
The AI Mk XV equipment and its antenna were carried in a bullet-shaped pod under the port wing, similar to the US Navy night fighters’ arrangement. The radar dish was designed to scan from side to side for AI applications, but it could also be commanded to look up and down by a few degrees. This enabled the aircraft to attack targets from above, and it could also search for surface vessels below, so that the aircraft could also act in ASV or pathfinder duties in a secondary role (much like the Mosquito night fighters, which frequently guided bomber formations to their targets).
In order to mount the pod to the outer wing and compensate for the gain of weight, the standard 0.303" Browning machine guns normally located there were deleted. Instead, the NF.XX was initially armed with two 20 mm Hispano cannon plus a pair of 0.5" machine guns, mounted in a fashion similar to the Spitfire's standard E wing.
The NF.XX was powered, like the Spitfire Mk. XIV, by the two-stage supercharged Griffon 65, producing 2,050 hp (1,528 kW). A five bladed Rotol propeller of 10 ft 5 in (3.18 m) in diameter was used, and for the night fighter role the standard single exhaust stubs gave way to a collector fairing on each side, which dampened flames and improved the crew's view in the darkness.
To help balance the heavy Griffon engine, the radio equipment was moved further back in the rear fuselage. Improved VHF radio equipment allowed for the aerial mast to be removed and replaced by a "whip" aerial further aft on the fuselage spine. Because of 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 introduced.
One problem that hampered all early Griffon-powered Spitfire variants also plagued the NF.XX, though: short legs. The NF.XX carried 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. With this internal capacity, the fighter's maximum range was just a little over 460 miles (740 km) since the new Griffon engine consumed much more fuel per hour than the Merlin engine of earlier variants, and the extra drag and weight through the radar equipment did not make things better.
As a simple remedy, a conformal, fixed belly tank between the radiators was devised. This carried an extra 90 gal, of fuel, extending the fighter's range to about 850 miles (1,370 km) – still not much for aerial patrol and extended loiter time for interceptions, but enough for short-notice home defense duties. Alternatively, a more conventional but jettisonable 100 gal. drop tank could be carried, but it produced considerably more drag and affected overall performance so dramatically that it was never used in service.
The first tests of the new aircraft were conducted in January 1945 and three pre-production machines (all converted Mk. XIV airframes) were allocated to night fighter units for field trials and direct comparison with two engine types. Despite its innate aerodynamic and weight penalties the Spitfire NF.XX still attained an impressive top speed of 400 mph (350 kn; 640 km/h) at 29,500 ft (9.000 m), even though in clean condition only. But it was still more than enough to take on much heavier German bombers and night fighters. The second crewman was another winning factor, since the pilot alone would be overloaded in the face of heavily armed enemy aircraft in the European theatre of operations and the local weather conditions.
Further initial experience with the type resulted in several ad hoc modifications: the wing span was increased in order to improve handling and climb performance, using standard wing tip extensions from Spitfire high altitude variants. Furthermore, a deeper rudder was added to the fin because the second cockpit created significant directional instability.
Armament was changed, too - more firepower and a longer range was deemed necessary to attack the German heavy night fighters, which themselves frequently carried defensive armament in the form of heavy machine guns. Consequently, the initial pair of 0.5" machine guns was deleted and replaced by an additional pair of 20 mm Hispano cannon, and all four guns received extended barrels for a higher weapon range.
In this form, the Spitfire NF.XX quickly entered RAF service in March 1945, but, in the meantime, the German night fighter threat had declined, so that only 50 machines were completed and delivered to RAF units in the UK until the end of hostilities.
The operational use of the machines was hampered by localized skin wrinkling on the wings and fuselage at load attachment points, a problem the type shared with the Mk. XIV day fighter. Even though Supermarine advised that the machines had not been seriously weakened, nor were they on the point of failure, the RAF nevertheless issued instructions in early 1945 that all F and FR Mk XIVs were to be retrospectively fitted with clipped wings to counter the threat. The NF.XX kept their elongated wing tips, however, and were simply limited to a top speed of 370 mph (600 km/h) and not allowed to dive anymore.
General characteristics:
Crew: 2 (pilot, radar operator)
Length: 32 ft 8 in (9.96 m)
Wingspan: 40 ft 2 in (12.2 m)
Height: 10 ft 0 in (3.05 m)
Wing area: 249.7 sq.ft (23.2 m²)
Airfoil: NACA 2213 (root), NACA 2209.4 (tip)
Empty weight: 8,680 lb (3,937 kg)
Gross weight: 10,700 lb (4,853 kg)
Max takeoff weight: 12,530 lb (5,683 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: 400 mph (640 km/h; 353 kn) in FS supercharger gear at 29,500 ft.
Combat range: 460 mi (741 km/400 nmi) with internal fuel only
850 mi (1,370 km/757 nmi)
Ferry range: 1,093 mi (1,759 km/950 nmi)
Service ceiling: 43,500 ft (13,259 m)
Rate of climb: 4,300 ft/min (21.8 m/s) in MS supercharger gear at 2,100 ft.
3,100 ft/min (15.8 m/s) in FS supercharger gear at 22,100 ft.
Time to altitude: 8 mins to 22,000 ft (at max weight)
Wing loading: 32.72 lb/sq ft (159.8 kg/m²)
Power/mass: 0.24
Armament:
4× 20 mm (0.787-in) Hispano Mk II cannon with 120 RPG in the wings
Provision for an auxiliary underfuselage tank, either a fixed conformal 90 gal tank or a
100 gal drop tank.
The kit and its assembly:
Well, Spitfire fans might call it crude to create a whiffy variant that incorporates so many ugly details. But this fever creation came into being through the simple thought: "What would a dedicated Spitfire night fighter with a radar look like?" From this initial creative spark I tried to build this fictional NF.XX variant with available late WWII technology from a Griffon-powered Spitfire.
The basis is the Airfix Spitfire PR.XIX kit, a nice and clean offering, even though the use of this photo recce variant meant some additional work. The radar pod comes wholesale from an F4U night fighter (Fujimi), since the wing installation appeared to me to be the only plausible (and proven) option.
The second cockpit and the "double bubble" canopy come from an RS Models Spitfire Mk.IX UTI trainer, which is/was a domestic conversion made in the Soviet Union. The kit comes with an extra two seater fuselage, so that, despite body donors, almost a complete Spitfire remains (just the cockpit missing, but this can be taken from the Airfix kit).
I also considered the Spitfire TR.IX arrangement, with a stepped bubble canopy, but found that the risen rear cockpit for the instructor would not make sense in a night fighter, so the UTI arrangement with separate canopies on the same level appeared to me to be the most suitable solution for this aircraft and its task.
Surgery was not easy, though: The whole cockpit area was dissected from the RS Models trainer and – together with the internal parts like the bulkheads, dashboards and seats – transplanted into an appropriate gap, cut into the Airfix kit fuselage. The windscreen position on both airframes was used as orientation benchmark.
Basically a simple idea, but, even though you have two Spitfire kits at hand, both models differ slightly from each other in many ways. Material thickness is different, as well as panel lines, which are all there on both models but simply do not fall in line. Internal width and available space is also different, esp. the rear bulkhead was not easy to integrate into the Airfix fuselage. It worked, somehow, but it consequently took some PSR effort and rescribing (at least, both donor kits have engraved details) in order to create this Griffon-powered two-seater.
The extended wings were created through the simple implantation of high altitude wing tips from an AZ Model Spitfire I/II/V/VI kit. They match very well with the Airfix PR.XIX wings, which were simply clipped at the correct position outside of the ailerons. Since the recce Spitfire comes without any weapons I added four brass barrels (Pavla) to the wings, plus respective bulges for the magazines (scratched from sprue) and casing ejector fairings under the wings.
I also changed the vertical rudder. Instead of the separate OOB part from the Spitfire PR.XIX I used a deeper and higher rudder from a late Seafire mark (left over from a Special Hobby kit, IIRC). The part lost its hook and the notch for its deployment mechanism, replaced by a piece of styrene that was PSRed into the rest of the rudder. It’s not an obvious change, but the bigger fin area is a good counterpart to the enlarged wings and the bulkier rear fuselage.
The conformal belly tank was scratched from the upper half of a Matchbox A-10 inner wing. There are aftermarket solutions available, but I simply did not want to spend as much money on a single resin part that no one will clearly see and that’s just as expensive as the whole Airfix basis kit. Some things are just ridiculous.
Painting and markings:
Very simple: classic late war RAF night fighter colors, with Medium Sea Grey and Dark Green (Humbrol 165 and 163, respectively) on the uppers surfaces, plus Night (I used Revell Acrylics 06, Tar Black, which is actually a very dark grey tone) underneath, with a high waterline and a black fin. Looks weird on a Spitfire, but also somewhat cool!? The model received a light black ink wash and some panel post-shading, using a blue-ish hue for the Night undersurfaces.
The interior is classic RAF Cockpit Green (Humbrol 78), the only catchy marking is the red propeller spinner – originally I just wanted to keep the spinner black, too, but found that to be too dull overall.
The markings come from different sources; the codes were created with single Dull Red letters from Xtradecal, roundels and other markings come from various other sheets. The added “G” to the serial number is, BTW, an indication that the aircraft had to be guarded all the time. A nice and appropriate detail for this high tech aircraft of its time. The roundels/fin flashes were taken from another Xtradecal sheet, IIRC they belong to an FAA SB2C Helldiver.
Finally, some wear marks were added with dry-brushed light grey and silver. Exhaust stains were added with dry-brushed dark and light grey, as well as some grinded graphite. A coat of matt acrylic varnish (Italeri) sealed the kit.
I feel a bit guilty of creating the probably ugliest Spitfire possible, with all the add-ons and the weird proportions through the second cockpit and the belly tank. Very massive, at least for this sleek aircraft. The night fighter paint scheme suits the Spitfire surprisingly well, though. Anyway, it’s whifworld, after all, and I tried to go through with the night fighter idea as good and consequential as possible – the fictional NF.XX is just my personal interpretation of the theme.
INTERIOR VIEW OF THE ADDITIVE MANUFACTURING INTEGRATED ENERGY (AMIE) 3D-PRINTED HOUSE.
Oak Ridge National Laboratory combines clean energy technologies into a 3D-printed building and vehicle to showcase a new approach to energy use, storage and consumption. It is a model for energy-efficient systems that link buildings, vehicles and the grid. ORNL team worked with industrial partners to manufacture and connect a natural-gas-powered hybrid electric vehicle with a solar-powered building to create an integrated energy system. The project's energy control center manages the system's electrical demand and load by balancing the intermittent power from the building's 3.2-kilowatt solar array with supplemental power from the vehicle.
For more information or additional images, please contact 202-586-5251.
NASA astronauts Nicole Mann and Josh Cassada watch as a United Launch Alliance Atlas V rocket with Boeing’s CST-100 Starliner spacecraft onboard is rolled to the launch pad at Space Launch Complex 41 ahead of the Orbital Flight Test mission, Wednesday, Dec. 18, 2019 at Cape Canaveral Air Force Station in Florida. The Orbital Flight Test with be Starliner’s maiden mission to the International Space Station for NASA's Commercial Crew Program. The mission, currently targeted for a 6:36 a.m. EST launch on Dec. 20, will serve as an end-to-end test of the system's capabilities. Photo Credit: (NASA/Joel Kowsky)
Found in my old bedroom closet a few months ago. Everything -- box, manuals, system -- is in amazing condition except for the system's screen, which is missing a few lines (yes, lines) of pixels. Oh, well, at least it still works well enough to play games.
For more info on this find, check out this recent blog post: www.thegaygamer.com/2012/04/from-back-of-my-boyhood-close...
With the lightweight aluminium front and rear axles from the BMW M3/M4 models, forged 19-inch aluminium wheels with mixed-size tyres, M Servotronic steering with two settings and suitably effective M compound brakes, the new BMW M2 Coupe has raised the bar once again in the compact high-performance sports car segment when it comes to driving dynamics. The electronically controlled Active M Differential, which optimises traction and directional stability, also plays a significant role here. And even greater driving pleasure is on the cards when the Dynamic Stability Control system’s M Dynamic Mode (MDM) is activated. MDM allows wheel slip and therefore moderate, controlled drifts on the track.
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Emma: “Well, my Z’s definitely buff an’ bitchin’, boot he’s by no means bronze…*scowls* an’ he is still a ten. Better than a ten! Yer rating system‘s rubbish!”
Chloe (amused) “No worries, Em. There’s a special category for Z. He’s Buff, Bihaku, and…”
Suki & Chloe: *in unison, while fist bumping* “Bitchinnn’!”
Emma: “Bihaku? That’s Japanese, innit? Whit’s it mean?”
Suki: “Beautiful white.”
Emma: *giggles* “Aye, that’s bang on, then! Z is beautiful white—like a marble statue in a museum….except he’s no’ cold. He’s verra, verra warm. In fact, sometimes in bed—”
Suki: “Eek, lemme stop you right there, Big Mac. He is still my brother; thus, this conversation could go real bad, real fast and cause me to blow some gnarly-ass chunks up in here.”
Candy: “Well, what about our guys? They’re not bronze, but they’re not bihaku, either. And they’re most definitely tens!”
Kumi (pointedly): “Obviously, that’s not up for debate, since Chlo’s got an altar to my guy’s shirtless visage on her wall.”
Yuri: *mutinous expression* “Lukas is vastly superior; hence, he cannot be defined by any frivolous rating system!”
Suki: “Whoa, chillz down, babies! No need to go all peasants storming the Bastille on us. Chlo’s real good at customizing our system to include the melanin-deficient. *turns to Chloe* Luke?”
Chloe: *purrs* “Buff, Brainy, and Bitchinnn’!”
Suki: “Big Guns?”
Chloe: “Buff, British, and Bitchinnn’!”
Suki: “Danny?”
Chloe: “Buff, Bad-ass, and Bitchinnn’!”
Kumi: “Damn, you are good, Chlo.”
Chloe (modestly): “Well, I am a life-long student of the Triple-B system. Y’all are just newbs.”
Emma: “Ken whit else is BBB? My wedding dress! It’s brilliant, brilliant, brilliant! *falls back onto the bed, squeals with unadulterated joy while doing a little wiggle dance*
Candy (straight-faced): “Huh, I think she likes the gown, guys.”
Kumi: “Duh, of course she does. We picked it out.”
Yuri (teasingly): Well, I am still not quite convinced. Are you certain it suits your taste, darling?”
Emma: *sits up, nods rapidly* “Aye! I love-love-love it! I spent at least half an hour starin’ at myself in it last night, after I kicked Z oot o’ our room so I could try it on!”
Kumi (dryly): “We know, Mouse. We were there, too, remember?”
Fashion Credits
**Any doll enhancements (i.e. freckles, piercings, eye color changes) were done by me unless otherwise stated.**
Yuri
Dress, Scarf, Shoes: Mattel – Barbie Collectibles – Lilly Pulitzer Gift Set
Bracelets: Me
Doll is a Nu.Fantasy Red Riding Hood Yuri transplanted to a NuFace body.
Kumi
Shorts: Moxie Boyz – Swim Magic Owen
Shirt: Clear lan
Belt: Randall Craig RTW – April in Paris
Hat: Sekiguchi Momoko – Berry Hunter
Shoes: Fashion Royalty – Capricious Natalia
Necklace: Me
Doll is a Nu.Fantasy Wild Wolf Kumi transplanted to a NuFace body.
Candy
Skirt: Best Friends Club Fashion
Top: Katalina
Belt: Cangaway (etsy.com)
Necklace & Bracelets: Me
Doll is a Making a Scene Erin transplanted to a Misaki body.
Emma
Dress: Nina
Belt: Randall Craig RTW – Lili Style Redux
Shoes: Mattel – Playline – Fashion Fever Mannequin
Barrette: Mattel – Barbie Collectibles – Juicy Couture Gift Set
Pride Bracelet Set – Knife’s Edge Designs (me)
Doll is a Style Mantra Eden.
Suki
Jeans: Mattel – Barbie Collectibles – Best Model South Beach – Removed front pockets.
Belt: me
Bikini Top: watbetty
Top: Mattel – Playline – Cali Girl Lea
Shoes: Mattel – Playline
Forest Floor Necklace: Knife’s Edge Designs (me)
Model is a London by Night Ayumi transplanted to a Misaki body.
Chloe
Playsuit: Jessica of Cozy Couture
Belt: Cangaway (etsy.com)
Boots: Snow’s Shopping Paradise (ebay.com)
Headband & Bracelets: Me
Model is a Costume Drama Giselle transplanted to a Poppy body and re-rooted by the amazing valmaxi!
The Space Shuttle orbiter is the spaceplane component of the Space Shuttle, a partially reusable orbital spacecraft system that was part of the discontinued Space Shuttle program. Operated from 1977 to 2011 by NASA, the U.S. space agency, this vehicle could carry astronauts and payloads into low Earth orbit, perform in-space operations, then re-enter the atmosphere and land as a glider, returning its crew and any on-board payload to the Earth.
Six orbiters were built for flight: Enterprise, Columbia, Challenger, Discovery, Atlantis, and Endeavour. All were built in Palmdale, California, by the Pittsburgh, Pennsylvania-based Rockwell International company. The first orbiter, Enterprise, made its maiden flight in 1977. An unpowered glider, it was carried by a modified Boeing 747 airliner called the Shuttle Carrier Aircraft and released for a series of atmospheric test flights and landings. Enterprise was partially disassembled and retired after completion of critical testing. The remaining orbiters were fully operational spacecraft, and were launched vertically as part of the Space Shuttle stack.
Columbia was the first space-worthy orbiter; it made its inaugural flight in 1981. Challenger, Discovery, and Atlantis followed in 1983, 1984, and 1985 respectively. In 1986, Challenger was destroyed in an accident shortly after its 10th launch. Endeavour was built as Challenger's successor, and was first launched in 1992. In 2003, Columbia was destroyed during re-entry, leaving just three remaining orbiters. Discovery completed its final flight on March 9, 2011, and Endeavour completed its final flight on June 1, 2011. Atlantis completed the final Shuttle flight, STS-135, on July 21, 2011.
In addition to their crews and payloads, the reusable orbiter carried most of the Space Shuttle System's liquid-propellant rocket system, but both the liquid hydrogen fuel and the liquid oxygen oxidizer for its three main rocket engines were fed from an external cryogenic propellant tank. Additionally, two reusable solid rocket boosters (SRBs) provided additional thrust for approximately the first two minutes of launch. The orbiters themselves did carry hypergolic propellants for their Reaction Control System (RCS) thrusters and Orbital Maneuvering System (OMS) engines.
Wikipedia: <a href="https://en.wikipedia.org/wiki/Space_Shuttle_orbiter" rel="noreferrer nofollow">en.wikipedia.org/wiki/Space_Shuttle_orbiter</a>
Les TGV Duplex sont des rames électriques TGV de la SNCF, mises en service de 1995 à 2012. Comme leur nom l'indique, elles sont constituées de voitures à deux niveaux. La circulation à l'intérieur de la rame s'effectue par le niveau supérieur, offrant ainsi plus de calme aux voyageurs installés dans le niveau inférieur de chaque voiture. L'étage inférieur de la voiture-bar n'est pas accessible aux voyageurs, car il est occupé par des équipements électriques. Les rames Duplex ont, pour une même longueur, une capacité de transport supérieure de 133 places à celle des TGV Réseau : une rame, composée de 8 voitures (200 mètres de longueur), dispose ainsi de 182 places en 1re classe et 328 en 2de classe, soit un total de 510 places. Par ailleurs, 634 places (uniquement de 2de classe) sont disponibles en aménagement « Ouigo ».
La conception de ces rames a été très poussée, en particulier dans le domaine de la réduction des masses (par l'emploi de l'aluminium au lieu de l'acier pour la structure des caisses, sauf les motrices), afin de respecter la règle de 17 tonnes à l'essieu obligatoire sur les lignes à grande vitesse françaises.
une rame hybride avait été créée à la suite d'un accident en 2003, une motrice Réseau ayant alors remplacé son homologue Duplex. De la fin janvier 2009 à septembre 2012, la rame 255 a circulé également avec cette configuration, à la suite de l'incendie en ligne d'une de ses motrices le 10 janvier 2009 à Pont-de-Veyle ; cela s'est aussi produit pour la rame 204 en 2008 (utilisation de la motrice 28003 précitée), la rame 290 de 2013 à 2015 (à la suite de l'incendie d'une de ses motrices le 23 septembre 2013, en gare de Lyon-Part-Dieu16), puis sur d'autres rames (comme les 218, 234 et 201) par la suite.
Source :
fr.wikipedia.org/wiki/TGV_Duplex
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Translation / Traduction 🇬🇧 UK
The TGV Duplex is a French high-speed train of the TGV family, manufactured by Alstom, and operated by the French national railway company SNCF. It is unique among TGV trains in that it features bi-level carriages. The Duplex inaugurated the third generation of TGV trainsets. It was specially designed to increase capacity on high-speed lines with saturated traffic. With two seating levels and a seating capacity of 508 passengers, the Duplex increases the passenger capacity. While the TGV Duplex started as a small component of the TGV fleet, it has become one of the system's workhorses.
Makemake, second brightest dwarf planet of the Kuiper belt, has a moon. Nicknamed MK2, Makemake's moon reflects sunlight with a charcoal-dark surface, about 1,300 times fainter than its parent body. Still, it was spotted in Hubble Space Telescope observations intended to search for faint companions with the same technique used to find the small satellites of Pluto. Just as for Pluto and its satellites, further observations of Makemake and orbiting moon will measure the system's mass and density and allow a broader understanding of the distant worlds. About 160 kilometers (100 miles) across compared to Makemake's 1,400 kilometer diameter, MK2's relative size and contrast are shown in this artist's vision. An imagined scene of an unexplored frontier of the Solar System, it looks back from a spacecraft's vantage as the dim Sun shines along the Milky Way. Of course, the Sun is over 50 times farther from Makemake than it is from planet Earth. via NASA ift.tt/26DRj0x
Newspaper ad from May, 1952 for the first cable TV service, then community antenna TV, in Wilkes-Barre PA showing the system's headend tower.
For a one-time installation fee of $129.99 subscribers could receive stations in Philadelphia and Binghamton NY for a monthly maintenance fee of $3.68.
The area is now served by Service Electric. A standard headend tower now stands here.
( more old negatives ..)
Now THIS was a comet !! (Hale-Bopp, cruising through a faint arc of Aurora.)
I've been taking a look at a couple of tiny faint little comets lately, whenever sky conditions permit, both delicate fuzzballs at the outer limits of visual capability, Comet Hartley 2, last seen in Monoceros, and so far just a brief glimpse of Ikeya-Murakami, in Virgo
I hope to live long enough to enjoy another monster comet like Hale-Bopp or Hyakutake ....
Kiev 19 SLR, Fuji 800 film.
Vicksburg, Mississippi est. 1825, pop. (2013) 23,542 • MS Delta
• aka Levee Street Depot • designed by D.H. Burnham & Co., Chicago
• example of both the Georgian Revival style's post-1900 influence on American public buildings & the increased prosperity of the of the Illinois Central (Gulf) railroad system's Mississippi corridor
• Yazoo & Mississippi Valley Railroad —Wikipedia • Mississippi Valley & Yazoo Railroad Station —World of Decay • Yazoo & Mississippi Valley —Mississippi Rails
• rehabbed as restaurant & office facility, late 1970s • damaged by flood, 2011 • now Old Depot Museum
• (L) Vicksburg Riverfront Murals • 32 panels depict Vicksburg's past • painted on the Levee St. floodwall, 2002-2009, by Louisiana muralist Robert Dafford (b. 1951) • Facebook
• Levee St. Station designated Mississippi Landmark, 149-VKS-0780-NR-ML, 2001 • National Register # 79001341, 1979
SpaceX CEO and Chief Designer Elon Musk, left, speaks with NASA astronauts Doug Hurley, center, and Bob Behnken, right, who are assigned to fly on the crewed Demo-2 mission after launch of a SpaceX Falcon 9 rocket carrying the company's Crew Dragon spacecraft on the Demo-1 mission from firing room four of the Launch Control Center, Saturday, March 2, 2019 at the Kennedy Space Center in Florida. The Demo-1 mission will be the first launch of a commercially built and operated American spacecraft and space system designed for humans as part of NASA's Commercial Crew Program. The mission will serve as an end-to-end test of the system's capabilities. Photo Credit: NASA/Joel Kowsky
+++ 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 Lockheed XFV (sometimes erroneously referred to as the "Salmon", even though this was actually the name of one of its test pilots and not an official designation) was an American experimental tailsitter prototype aircraft built by Lockheed in the early 1950s to demonstrate the operation of a vertical takeoff and landing (VTOL) fighter for protecting convoys.
The Lockheed XFV originated as a result of a proposal issued by the U.S. Navy in 1948 for an aircraft capable of vertical takeoff and landing (VTOL) aboard platforms mounted on the afterdecks of conventional ships. Both Convair and Lockheed competed for the contract, but in 1950 the requirement was revised with a call for a research aircraft capable of eventually evolving into a VTOL ship-based convoy escort fighter. On 19 April 1951, two prototypes were ordered from Lockheed under the designation XFO-1 (company designation was Model 081-40-01). Soon after the contract was awarded, the project designation changed to XFV-1 when the Navy's code for Lockheed was changed from O to V.
The XFV was powered by a 5,332 hp (3,976 kW) Allison YT40-A-6 turboprop engine, composed of two Allison T38 power sections driving three-bladed contra-rotating propellers via a common gearbox. The aircraft had no landing gear, just small castoring wheels at the tips of the tail surfaces which were a reflected cruciform v-tail (forming an x) that extended above and below the fuselage. The wings were diamond-shaped and relatively thin, with straight and sharp leading edges – somewhat foretelling the design of Lockheed’s Mach-2-capable F-104 Starfighter.
To begin flight testing, a temporary non-retractable undercarriage with long braced V-legs was attached to the fuselage, and fixed tail wheels attached to the lower pair of fins. In this form, the aircraft was trucked to Edwards AFB in November 1953 for ground testing and taxiing trials. During one of these tests, at a time when the aft section of the large spinner had not yet been fitted, Lockheed chief test pilot Herman "Fish" Salmon managed to taxi the aircraft past the liftoff speed, and the aircraft made a brief hop on 22 December 1953. The official first flight took place on 16 June 1954.
Full VTOL testing at Edwards AFB was delayed pending the availability of the 7,100 shp Allison T54, which was earmarked to replace the T40 and power eventual serial production aircraft. But the T54 faced severe development delays, esp. its gearbox. Another problem that arose with the new engine was that the propeller blade tips would reach supersonic speed and therefore compressibility problems.
After the brief unintentional hop, the prototype aircraft made a total of 32 flights. The XFV-1 was able to make a few transitions in flight from the conventional to the vertical flight mode and back, and had briefly held in hover at altitude, but the T40 output was simply not enough to ensure proper and secure VTOL operations. Performance remained limited by the confines of the flight test regime. Another issue that arose through the advancements of jet engine designs was the realization that the XFV's top speed would be eclipsed by contemporary fighters. Additionally, the purely manual handling of the aircraft esp. during landing was very demanding - the XFV could only be controlled by highly experienced pilots.
Both Navy and the Marines Corps were still interested in the concept, though, so that, in early 1955, the decision was made to build a limited pre-production series of the aircraft, the FV-2, for operational field tests and evaluation. The FV-2 was the proposed production version (Model 181-43-02), primarily conceived and optimized as a night/all-weather interceptor for point defense, and officially baptized “Solstice”. The FV-2 was powered by the T54-A-16 turboprop, which had eventually overcome its teething troubles and offered a combined power output equivalent of 7,500 shp (5,600 kW) from the propellers and the twin-engines’ residual thrust. Outwardly the different engine was recognizable through two separate circular exhausts which were introduced instead of the XFV’s single shallow ventral opening. The gearbox had been beefed up, too, with additional oil coolers in small ventral fairings behind the contraprops and the propeller blades were aerodynamically improved to better cope with the higher power output and rotation speed. Additionally, an automatic pitch control system was introduced to alleviate the pilot from the delicate control burdens during hover and flight mode transition.
Compared with the XFV, the FV-2 incorporated 150 lb (68 kg) of cockpit armor, along with a 1.5 in (38 mm) bullet-proof windscreen. A Sperry Corporation AN/APS-19 type radar was added in the fixed forward part of the nose spinner under an opaque perspex radome. The AN/APS-19 was primarily a target detection radar with only a limited tracking capability, and it had been introduced with the McDonnell F2H-2N. The radar had a theoretical maximum detection range of 60 km, but in real life air targets could only be detected at much shorter distances. At long ranges the radar was mainly used for navigation and to detect land masses or large ships.
Like the older AN/APS-6, the AN/APS-19 operated in a "Spiral Scan" search pattern. In a spiral scan the radar dish spins rapidly, scanning the area in front of the aircraft following a spiral path. As a result, however targets were not updated on every pass as the radar was pointing at a different angle on each pass. This also made the radar prone to ground clutter effects, which created "pulses" on the radar display. The AN/APS-19 was able to lock onto and track targets within a narrow cone, out to a maximum range of about 1 mile (1.5 km), but to do so the radar had to cease scanning.
The FV-2’s standard armament consisted of four Mk. 11 20 mm cannon fitted in pairs in the two detachable wingtip pods, with 250 rounds each, which fired outside of the wide propeller disc. Alternatively, forty-eight 2¾ in (70 mm) folding-fin rockets could be fitted in similar pods, which could be fired in salvoes against both air and ground targets. Instead of offensive armament, 200 US gal. (165 imp. gal./750 l) auxiliary tanks for ferry flights could be mounted onto the wing tips.
Until June 1956 a total of eleven FV-2s were built and delivered. With US Navy Air Development Squadron 8 (also known as VX-8) at NAS Atlantic City, a dedicated evaluation and maintenance unit for the FV-2 and the operations of VTOL aircraft in general was formed. VX-2 operated closely with its sister unit VX-3 (located at the same base) and operated the FV-2s alongside contemporary types like the Grumman F9F-8 Cougar, which at that time went through carrier-qualification aboard the USS Midway. The Cougars were soon joined by the new, supersonic F-8U-1 Crusaders, which arrived in December 1956. The advent of this supersonic navy jet type rendered the FV-2’s archaic technology and its performance more and more questionable, even though the VTOL concept’s potential and the institutions’ interest in it kept the test unit alive.
The FV-2s were in the following years put through a series of thorough field tests and frequently deployed to land bases all across the USA and abroad. Additionally, operational tests were also conducted on board of various ship types, ranging from carriers with wide flight decks to modified merchant ships with improvised landing platforms. The FV-2s also took part in US Navy and USMC maneuvers, and when not deployed elsewhere the training with new pilots at NAS Atlantic City continued.
During these tests, the demanding handling characteristics of the tailsitter concept in general and the FV-2 in specific were frequently confirmed. Once in flight, however, the FV-2 handled well and was a serious and agile dogfighter – but jet aircraft could easily avoid and outrun it.
Other operational problems soon became apparent, too: while the idea of a VTOL aircraft that was independent from runways or flight bases was highly attractive, the FV-2’s tailsitter concept required a complex and bulky maintenance infrastructure, with many ladders, working platforms and cranes. On the ground, the FV-2 could not move on its own and had to be pushed or towed. However, due to the aircraft’s high center of gravity it had to be handled with great care – two FV-2s were seriously damaged after they toppled over, one at NAS Atlantic City on the ground (it could be repaired and brought back into service), the other aboard a ship at heavy sea, where the aircraft totally got out of control on deck and fell into the sea as a total loss.
To make matters even worse, fundamental operational tasks like refueling, re-arming the aircraft between sorties or even just boarding it were a complicated and slow task, so that the aircraft’s theoretical conceptual benefits were countered by its cumbersome handling.
FV-2 operations furthermore revealed, despite the considerably increased power output of the T54 twin engine that more than compensated for the aircraft’s raised weight, only a marginal improvement of the aircraft’s performance; the FV-2 had simply reached the limits of propeller-driven aircraft. Just the rate of climb was markedly improved, and the extra power made the FV-2’s handling safer than the XFV’s, even though this advancement was only relative because the aircraft’s hazardous handling during transition and landing as well as other conceptual problems prevailed and could not be overcome. The FV-2’s range was also very limited, esp. when it did not carry the fuel tanks on the wing tips, so that the aircraft’s potential service spectrum remained very limited.
Six of the eleven FV-2s that were produced were lost in various accidents within only three years, five pilots were killed. The T54 engine remained unreliable, and the propeller control system which used 25 vacuum tubes was far from reliable, too. Due to the many problems, the FV-2s were grounded in 1959, and when VX-8 was disestablished on 1 March 1960, the whole project was cancelled and all remaining aircraft except for one airframe were scrapped. As of today, Bu.No. 53-3537 resides disassembled in storage at the National Museum of the United States Navy in the former Breech Mechanism Shop of the old Naval Gun Factory on the grounds of the Washington Navy Yard in Washington, D.C., United States, where it waits for restoration and eventual public presentation.
As a historic side note, the FV-2’s detachable wing tip gun pods had a longer and more successful service life: they were the basis for the Mk.4 HIPEG (High Performance External Gun) gun pods. This weapon system’s main purpose became strafing ground targets, and it received a different attachment system for underwing hardpoints and a bigger ammunition supply (750 RPG instead of just 250 on the FV-2). Approximately 1.200 Mk. 4 twin gun pods were manufactured by Hughes Tool Company, later Hughes Helicopter, in Culver City, California. While the system was tested and certified for use on the A-4, the A-6, the A-7, the F-4, and the OV-10, it only saw extended use on the A-4, the F-4, and the OV-10, esp. in Vietnam where the Mk. 4 pod was used extensively for close air support missions.
General characteristics:
Crew: 1
Length/Height: 36 ft 10.25 in (11.23 m)
Wingspan: 30 ft 10.1 in (9.4 m)
Wing area: 246 sq ft (22.85 m²)
Empty weight: 12,388 lb (5,624 kg)
Gross weight: 17,533 lb (7,960 kg)
Max. takeoff weight: 18,159 lb (8,244 kg)
Powerplant:
1× Allison T54-A-16 turboprop with 7,500 shp (5,600 kW) output equivalent,
driving a 6 blade contra-rotating propeller
Performance:
Maximum speed: 585 mph (941 km/h, 509 kn
Cruise speed: 410 mph (660 km/h, 360 kn)
Range: 500 mi (800 km, 430 nmi) with internal fuel
800 mi (1,300 km, 700 nmi) with ferry wing tip tanks
Service ceiling: 46,800 ft (14,300 m)
Rate of climb: 12,750 ft/min (75.0 m/s)
Wing loading: 73.7 lb/sq ft (360 kg/m²)
Armament:
4× 20 mm (.79 in) Mk. 11 machine cannon with a total of 1.000 rounds, or
48× 2.75 in (70 mm) rockets in wingtip pods, or
a pair of 200 US gal. (165 imp. gal./750 l) auxiliary tanks on the wing tips
The kit and its assembly:
Another submission to the “Fifties” group build at whatifmodellers-com, and a really nice what-if aircraft that perfectly fits into the time frame. I had this Pegasus kit in The Stash™ for quite a while and the plan to build an operational USN or USMC aircraft from it in the typical all-dark-blue livery from the early Fifties, and the group build was a good occasion to realize it.
The Pegasus kit was released in 1992, the only other option to build the XFV in 1:72 is a Valom kit which, as a bonus, features the aircraft’s fixed landing gear that was used during flight trials. The Pegasus offering is technically simple and robust, but it is nothing for those who are faint at heart. The warning that the kit requires an experienced builder is not to be underestimated, because the IP kit from the UK comes with white metal parts and no visual instructions, just a verbal description of the building steps. The IP parts (including the canopy, which is one piece, quite thick but also clear) and the decals look good, though.
The IP parts feature flash and uneven seam lines, sprue attachment points are quite thick. The grey IP material had on my specimen different grades of hard-/brittleness, the white metal parts (some of the propeller blades) were bent and had to be re-aligned. No IP parts would fit well (there are no locator pins or other physical aids), the cockpit tub was a mess to assemble and fit into the fuselage. PSR on any seam all around the hull. But even though this sound horrible, the kit goes together relatively easy – thanks to its simplicity.
I made some mods and upgrades, though. One of them was an internal axis construction made from styrene tubes that allow the two propeller discs to move separately (OOB, you just stack and glue the discs onto each other into a rigid nose cone), while the propeller tip with its radome remained fixed – just as in real life. However, due to the parts’ size and resistance against each other, the props could not move as freely as originally intended.
Separate parts for the air intakes as well as the wings and tail surfaces could be mounted with less problems than expected, even though - again – PSR was necessary to hide the seams.
Painting and markings:
As already mentioned, the livery would be rather conservative, because I wanted the aircraft to carry the uniform USN scheme in all-over FS 35042 with white markings, which was dropped in 1955, though. The XFV or a potential serial production derivative would just fit into this time frame, and might have carried the classic all-blue livery for a couple of years more, especially when operated by an evaluation unit. Its unit, VX-8, is totally fictional, though.
The cockpit interior was painted in Humbrol 80 (simulating bright zinc chromate primer), and to have some contrasts I added small red highlights on the fin pod tips and the gun pods' anti-flutter winglets. For some more variety the radome became earth brown with some good weathering, simulating an opaque perspex hood, and I added white (actually a very light gray) checkerboard markings on the "propeller rings", a bit inspired by the spinner markings on German WWII fighters. Subtle, but it looks good and breaks the otherwise very simple livery.
Some post-panel-shading with a lighter blue was done all over the hull, the exhaust area and the gun ports were painted with iron (Revell 91) and treated with graphite for a more metallic shine.
Silver decal stripe material was used to create the CoroGuard leading edges and the fine lines at the flaps on wings and fins - much easier than trying to solve this with paint and brush...
The decals were puzzled together from various dark blue USN aircraft, including a F8F, F9F and F4U sheet. The "XH" code was created with single 1cm hwite letters, the different font is not obvious, thanks to the letter combination.
Finally, the model was sealed with semi-gloss acrylic varnish (still shiny, but not too bright), the radome and the exhaust area were painted with matt varnsh, though.
A cool result, despite the rather dubious kit base. The Pegasus kit is seriously something for experienced builders, but the result looks convincing. The blue USN livery suits the XFV/FV-2 very well, it looks much more elegant than in the original NMF - even though it would, in real life, probably have received the new Gull Gray/White scheme (introduced in late 1955, IIRC, my FV-2 might have been one of the last aircraft to be painted blue). However, the blue scheme IMHO points out the aircraft's highly aerodynamic teardrop shape, esp. the flight pics make the aircraft almost look elegant!
President Joe Biden signs an executive order for 2022 Amendments to the Manual for Courts-Martial, strengthening the military justice system’s response to gender-based violence, Wednesday, January 26, 2022, in the Oval Office. (Official White House Photo by Adam Schultz)
Red-footed Boobies on a bar on Tern Island in the French Frigate Shoals, Hawaii.
Camera: Olympus OM-1
Lens: Olympus OM-System S Zuiko MC Auto-Zoom f/4 35-70mm.
Film: Kodak Ektachrome E100D Expired 10/20
Developer: The Darkroom
Back in the early days of my railroad photography (seven years old), my dad handed me whatever camera he had at the time and turned me loose in Chessie System's Riverside yard.
The former Baltimore and Ohio engine facility was filled with former Western Maryland power. A few precious frames of K64 were expended on a GP35, a SD40, and a F7.
I focused in on the GP35 as it appeared to have sustained an accident as the steps were closed off. Oh, to go back with today's photographic technology.