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Fact Community Transport NX57 FZC

 

Iveco Daily

 

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July 2015

Protesters at the Womens March in Oakland. Today Conway explained the White House is offering "alternative" facts in reference to Trumps false claims over his inaugural attendance numbers. This is getting more Orwellian by the minute!

+++ 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 ASTA (Aerospace Technologies of Australia, formerly Government Aircraft Factories) Baza development was started in 1995 when the Royal Australian Air Force was searching for a two-seat training aircraft that would allow the transition from initial training on piston-engined aircraft to jets, and could also be used for weapon training and CAS/reconnaissance duties.

 

ASTA responded with a low-wing two-turboprop-engined all-metal monoplane with retractable landing gear, capable of operating from unprepared strips when operationally required. The aircraft, internally coded “A-31”, was of conventional, all-metal (mainly duralumin) construction. The unswept cantilever wings have 3° of dihedral and are fitted with slotted trailing-edge flaps.

 

The A-31 had a tandem cockpit arrangement; the crew of two was seated under the upward opening clamshell canopy on Martin-Baker Mk 6AP6A zero/zero ejection seats and were provided with dual controls.

 

Armor plating was fitted to protect the crew and engines from hostile ground fire. The aircraft was powered by a pair of Garrett TPE 331 engines, driving sets of three-bladed propellers which were also capable of being used as air brakes.

 

The A-31 was designed for operations from short, rough airstrips.[The retractable tricycle landing gear, with a single nose wheel and twin main wheels retracting into the engine nacelles, is therefore fitted with low pressure tires to suit operations on rough ground, while the undercarriage legs are tall to give good clearance for underslung weapon loads. The undercarriage, flaps and brakes are operated hydraulically, with no pneumatic systems.

 

Two JATO rockets can be fitted under the fuselage to allow extra-short take-off. Fuel is fed from two fuselage tanks of combined capacity of 800 L (180 imp gal; 210 US gal) and two self-sealing tanks of 460 L (100 imp gal; 120 US gal) in the wings.

 

Fixed armament of the A-31 consisted of two 30mm Aden cannons mounted under the cockpits with 200 rounds each. A total of nine hardpoints were fitted for the carriage of external stores such as bombs, rockets or external fuel tanks, with one of 1,000 kg (2,200 lb) capacity mounted under the fuselage and the remaining two pairs of 500 kg (1,100 lb) capacity beneath the wing roots and wings inside of the engine nacelles, and two more pairs of hardpoints outside of the engines for another 500 kg and 227 kg, respectively. Total external weapons load was limited to 6,800 lb (3,085 kg) of weapons, though.

 

Onboard armaments were aimed by a simple reflector sight, since no all weather/night capabilities were called for – even though provisions were made that external sensors could be carried (e. g. a TISEO or a PAVE Spike pod).

 

Severe competition arose through the BAe Hawk, though: the Royal Australian Air Force ordered 33 Hawk 127 Lead-in Fighters (LIFs) in June 1997, 12 of which were produced in the UK and 21 in Australia – and this procurement severely hampered the A-31’s progress. The initial plan to build 66 aircraft for domestic use, with prospects for export, e. g. to Sri Lanka, Indonesia or Turkey, was cut down to a mere 32 aircraft which were to be used in conjunction with the Australian Army in the FAC role and against mobile ground targets.

 

This extended role required an upgrade with additional avionics, an optional forward looking infrared (FLIR) sensor and a laser ranger in an extended nose section, which lead to the Mk. II configuration - effectively, only five machines were produced as Mk.I types, and they were updated to Mk. II configuration even before delivery to the RAAF in August 1999.

 

Since then, the ASTA A-31 has been used in concunction with RAAF's Pilatus PC-9 and BAe Hawk Mk. 127 trainers. Beyond educational duties the type is also employed for Fleet support to Navy operations and for close air support to Army operations.

 

The 'Baza' (christened by a small sized bird of prey found in the forests of South Asia and Southeast Asia) has even seen serious military duty and already fired in anger: since August 2007, a detachment of No. 114 Mobile Control and Reporting Unit RAAF has been on active service at Kandahar Airfield in southern Afghanistan, and a constant detachment of six A-31's from RAAF 76 Suqadron has been assigned to armed reconnaissance and protection of approximately 75 personnel deployed with the AN/TPS-77 radar, assigned the responsibility to co-ordinate coalition air operations.

  

General characteristics:

Crew: 2

Length (incl. Pitot): 14.69 m (48 ft 1 ½ in)

Wingspan: 14.97 m (49 ft)

Height: 3, 75 m (12 ft 3 in)

Wing area: 30.30 m2 (326.1 sq ft)

Aspect ratio: 6.9:1

Airfoil: NACA 642A215 at root, NACA641 at tip

Empty weight: 4,020 kg (8,863 lb)

Max takeoff weight: 6,800 kg (14,991 lb)

Internal fuel capacity: 1,280 L (280 imp gal; 340 US gal)

 

Powerplant:

2 × Garrett TPE 331-11U-601G turboprop engines, 820 kW (1.100 hp) each

 

Performance:

Maximum speed: 515 km/h (311 mph; 270 kn) at 4.570 m (15.000 ft)

Cruising speed: 430 km/h (267 mph; 232 kn) at 2.500 m (8.200 ft)

Stall speed: 143 km/h (89 mph; 77 kn) (flaps and undercarriage down)

Never exceed speed: 750 km/h (466 mph; 405 kn)

Range:1.611 km (1.000 mi; 868 nmi), clean and internal fuel only

Ferry range: 3,710 km (2,305 mi; 2,003 nmi) max internal and external fuel

Service ceiling: 10,000 m (32,808 ft)

g limits: +6/-3 g

Rate of climb: 6.5 m/s (1.276 ft/min)

 

Armament:

2× 30 mm ADEN cannons in the lower nose

Up to 6,800 lb (3,085 kg) of weapons on nine external hardpoints

  

The kit and its assembly:

Like many of my whifs, this was spawned by a project at whatifmodelers.com from fellow user silverwindblade that ran under the handle "COIN aircraft from a Hawk" - and in fact, the BAe Hawk's fuselage with its staggered cockpit and good field of view appears as a good basis for a conversion.

 

I liked the idea VERY much, and while silverwindblade's work would rather develop into a futuristic canard layout aircraft, I decided to keep the COIN aircraft rather conservative - the FMA 58 'Pucara' from Argentina would be a proper benchmark.

 

The basis here is the Italeri BAe Hawk Mk. 127 kit which comes with the longer nose and modified wings for the RAAF version, as well as with false decals.

Anyway, I'd only use the fuselage, anything else is implanted, partly from unlikely donation kits! Wings incl. engine nacelles and stablizers come from the vintage box scale (1:166?) Revell Convair R3Y-2 Tradewind flying boat(!), the fin from an Academy OV-10 Bronco.

 

The landing gear was puzzled together, among other from parts of a 1:200 Concorde, the propellers were scratched.

 

Biggest mod to the fuselage is the dissection of the air intakes (and their blending with the fuselage) as well as a new tail section where the Adour jet engine's exhaust had been.

  

Painting and markings:

This model was agood excuse to finally apply an SIOP color scheme, which was originally carried by USAF's strategic bombers like B-52 or FB-111. But what actually inspired me were Australian C-130s - it took some time to figure out that their scheme were the USAF's SIOP colors (FS 34201, 34159 and 34079). But that made the Baza's potential user's choice (and fictional origin) easy.

 

As a COIN role aircraft I settled on a wraparound scheme. I found a pattern scheme on an USN Aggerssor A-4 Skyhawk that had been painted in SIOP colors, too, and adapted it for the model. Basic colors were Humbrol 31, 84 and 116, good approximations - the result looks odd, but suits the Baza well.

 

Later, panels were emphasized through dry painting with lighter shades and a light black ink wash was applied.

 

The landing gear became classic white, the cockpit interior medium gray - nothing fancy.

 

The markings were improvised - the Italeri Hawk Mk. 127 features RAAF 'roos, but these are printed in black - wrong for the OOB kit, but very welcome on my aircraft. The rest was salvaged from the scrap box, the tactical code A-31-06 created with single letters from TL Modellbau.

PAYPAL $15.00 GRIMETIMEMAGAZINE@GMAIL.COM

sorry i couldn't edit the picture. i felt like i haven't posted anything in a while. and i wanted to post these facts today, and i was to lazy to put "niley facts" x)

so yeah, these are REAL facts, so dont complain the badassity of it ;)

 

P.S. i've been seeing these facts on people's twitters and they don't even credit me. I just know for sure they're my facts, js. so, if i see them on someone's twitter without giving me credit again, i'm not posting anymore Niley facts. k? goood:)

 

64. E! says Nick is alot of the inspiration on Can't Be Tamed

 

65. Miley Cyrus was at the recording of the Year 3000 video.

 

66. Miley owns a JONAS shirt.

 

67. Nick was given a survey when he was 13, and wrote "Miley Cyrus" as his celebrity crush.

 

68. Billy Ray called Nick "a good kid" on Larry King in 09

 

69. Ryan: Are you in love with Nick Jonas? Miley; I AM NOT IN LOVE WITH NICK JONAS! R: Is he in love with you? M: Yes. Ryan: Have you made out with him? Miley: NO! Ryan; Will you makeout with him? Miley: Yes. (2007)

 

70. On Miley's can't be tamed album, "Scars" & "Take Me Along" is supposedly about Nick Jonas.

 

71. Nick sang Before The Storm in the same place he and Miley broke up. Hartford, Conneticut. (August 13, 2010.)

 

72. That same night, Noah tweeted Nick, "Hey Nick its noah! See ya. xoxo" She also tweeted about rockin out to Year 3000 and it being her favorite song. (August 13, 2010.)

 

73. Nick supposedly danced to Party In The USA at the Road Dogs Game. (August 6th, 2010)

 

74. Miley used to carry band-aids around specially for Nicks diabetes

 

75. Miley is RUMORED to be texting Nick a lot. A source says "They are not done and could possibly get together this fall"

 

76. Nick reportedly turned down a Duet with miley 'cause he was too busy touring with his brothers.

 

77. Nick changed the lyrics AGAIN to Still in Love With You from "You're not Listening" to "You're my destiny." [September 5, 2010]

 

78. Nick always smiles when Miley is mentioned to him at an interiew.

 

79. Nick and Miley both LOVE the band Coldplay.

 

80. Nick and Miley both got the new iPhone4 recently.

 

81. Paranoid is not about Miley, but it's rumored to be about Selena or Taylor Swift.

 

82. On the set of "Send it On", Joe & Nick would always make fun of Miley and say that she's the youngest of the cast. <-- this made me LOL. x)

 

83. Frankie Jonas & Noah Cyrus are team Niley.

 

84. "We wrote the song after a personal experience that made us grow in the ways of love and relationship And being able to perform this song with an old friend was truly amazing ." -Nick.

 

85. “We have one of those things where it’s kind of always there. She’s so important to me, and I’m really lucky.” - Nick.

 

86. Miley tweeted once: "Watching Beauty and The Beast :) Why can't I be more like Belle?" and Nick said his favorite Disney princess is Belle. [September 3, 2010.]

 

&

 

87. Nick couldn't stop smiling at the interview With Paul when they mentioned Miley. www.youtube.com/watch?v=Dp8qSeOks7k <-- BTW, love this interview! it's frickin hilarious. you should watch the whole thing x)

+++ 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 Dassault-Breguet Super Étendard (trans. "battle flag") is a French carrier-borne strike fighter aircraft designed by Dassault-Breguet for service with the French Navy. The aircraft was an advanced development of the Étendard IVM, the first of three prototypes, an IVM modified with the new engine and some of the new avionics, made its maiden flight on 28 October 1974. Original intentions were for 100 Super Étendard aircraft to be ordered for the French Navy, however the order placed was for 60 of the new model with options for a further 20; further budget cuts lead to only 71 Super Étendards being purchased in the end for the Aéronavele, with deliveries starting in June 1978.

 

In the first year of production, 15 Super Étendards were produced for the French Navy, allowing the formation of the first operational squadron in 1979. Dassault produced the aircraft at a rough rate of two per month, which was kept up until 1983.

 

Foreign customers were few: The Argentinian Navy would place an order for 14 aircraft to meet their requirements for a capable new fighter that could operate from their sole aircraft carrier. Furthermore a total of five Super Étendards were loaned to Iraq in 1983 while the country was waiting for deliveries of Agave-equipped Dassault Mirage F1s, capable of launching Exocet missiles that had been ordered. A third user of the Super Étendard with a similar background to the Iraq solution was the German Navy, with its land-based air arm, called the Marineflieger.

 

In the late 70ies, the German air force was about to replace its Starfighters, which had never been the Marinefliegers' first choice. Actually, in 1958 Germany chose the Starfighter to replace the already outdated F-84 and F-86 versions in use by then. For political reasons the Marineflieger had to join this decision, though their demands were quite different. The German Navy was looking for a two-seat, twin-engined aircraft to replace the old Seahawks, with the Hawker Siddeley Buccaneer being their favourized aircraft.

 

Neverthless, a rather political decision to buy the Starfighter for both German air arms was made, and consequently total of 132 Starfighters were acquired for naval service, including F-104G as maritime attack aircraft (equipped with Kormoran anti-ship missiles), RF-104G for maritime reconaissance and TF-104G as trainers. In addition to this, a small number of two-seat F-104F saw operational use with the Navy's Jet Air Wings. Introduction of the F-104 into naval air arm service began in september 1963, with MFG 1 being the first unit to be equipped with Germany's new standard weapon system. Sister Wing MFG 2 joined the Starfighter club in march of the following year.

 

Anyway, almost 20 years later and with the advent of the Panavia Tornado, the Marineflieger would finally receive the aircraft they had originally been calling, and the F-104Gs were starting to be phased out from 1980 on. Production of the Tornado and its delivery to both Luftwaffe (which had priority) and Marineflieger wings was lagging behind schedule, though, and in order to bridge that gap Germany decided in Febraury 1981 to lease the relatively new French Super Étendard. The Douglas A-4 Skyhawk and LTV A-7 Corsair II had been considered, too, but the French type eventually turned out to be the most economical and modern solution.

 

A total of 16 aircraft were ordered, and these were diverted from the running production lines. Delivery started in early 1982, when the scheduled Starfighter retirement and replacement was about to begin. All machines are allocated to MFG 2. In parallel, MFG 1 had the honours to be the first Bundeswehr unit to be equipped with the Tornado IDS multirole aircraft, as they started conversion in 1982. Before that, the multi-national conversion units in the UK had already received the initial Tornado trainer aircraft since 1980.

 

The German Super Étendards were given the tactical codes of 42+01 to 42+16 and were originally delivered in the standard Marineflieger camouflage of uniform grey upper surfaces (RAL 7012, Basaltgrau) and light grey lower sides (RAL 7035, Lichtgrau), in a pattern that was identical to the French aircraft.

 

Outwardly the German Super Étendards did not differ from its French cousins, since the aircraft were to be given back after only a few years of use - it was planned to keep the French fighters until 1986, when all Starfighters would have been replaced by Tornados. The Marineflieger "Sue" (nicknamed "Susi" or "Suse" by German crews, an abbreviation of the German female first name "Susanne") had no special features, as these were more or less French stock aircraft, but some components and avionics were changed.

 

For instance, the German aircraft were modfied to carry and launch up to two AS.34 Kormoran missiles, and they were already prepared to carry the updated Kormoran 2 with a digital data bus, a bigger warhead and longer range. They were also able to carry indigenous equipment like the 'Cerberus' ECM pod or the Swedish BOZ-101 chaff/flare pod - both of these as well as the Kromoran 2 were also to carried by the Tornados, and the Super Étendards would already be used fotr practice and evaluation.

The new AGM-88 HARM missile was reserved for the Tornado, though, so that the Super Étendard was primarily tasked with anti-ship and CAS tasks. For self-defense, the German Super Étendards were able to carry the AIM-9 Sidewinder instead of the French Matra Magic AAM. An Orpheus IV reconnaissance pod could be carried on thone of the inner wing pylons, with a drop tank for balance on the other side.

 

In the course of their short German service (which actually lasted until 1987, when the last Starfighter was retired from Marineflieger service), the Super Étendards were also used to test experimental camouflage schemes. 42+10, 42+12 and 42+15 started to carry very different liveries from 1983, and the results eventually lead to the Marineflieger Tornados' 'Norm 87' wrap-around paint scheme, consisting of RAL 7009 (Grüngrau), 7012 (Basaltgrau) and 5008 (Graublau).

 

No aircraft was lost during the leasing service. All aircraft were, after a major overhaul, integrated into the Aéronavale from 1988 on.

   

General characteristics

Crew: 1

Length: 14.31 m (45 ft 11½ in)

Wingspan: 9.60 m (31 ft 6 in)

Height: 3.86 m (12 ft 8 in)

Wing area: 28.4 m² (306.7 ft²)

Empty weight: 6,500 kg (14,330 lb)

Max. takeoff weight: 12,000 kg (26,455 lb)

Powerplant: 1 × SNECMA Atar 8K-50 turbojet, 49.0 kN (11,025 lbf)

 

Performance

Maximum speed: 1,000 km/h (637 knots, 733 mph) at low level

Range: 1,820 km (983 nmi, 1,130 mi)

Service ceiling: 13,700 m (44,900 ft)

Rate of climb: 100 m/s[62] (19,700 ft/min)

Wing loading: 423 kg/m² (86.3 lb/ft²)

Thrust/weight: 0.42

 

Armament

2× 30 mm (1.18 in) DEFA 552 cannons with 125 RPG

4× underwing and 2× under-fuselage hardpoints with a capacity of 2,100 kg (4,600 lb) maximum

   

The kit and its assembly:

The idea for this model was inspired by a profile designed by fellow user PantherG at whatifmodelers.com, showing a German Super Étendard in a fictional Marineflieger style paint scheme. I've been fascinated by the Tornado's Norm '87 scheme - but rather not by the Tornado itself. So I was happy to have an "excuse" to build a respective what-if model, taking a virtual idea to hardware.

 

The model is the standard Academy Super Étendard in 1:72, which is well-detailed - only the cockpit can take some attention, esp. the ejection seat, which I replaced completely, and I also added a Matchbox pilot which had to have its legs cut off, since the cockpit seems to be designed for Asian body measures... pretty tight in there!

 

Basically the kit was kept OOB. Only changes were made to the ordnance, which was taken from a German Tornado (Italeri). I also drilled open the air brakes' holes under the fuselage, and lowered the flaps for a more lively look. Overall, the Sue is rather clean and not really interesting - so any additional detail helps, I guess.

  

Painting and markings:

This took some legwork, since I wanted to stay true to reality, despite creating a whif.

 

The tactical code 42+XX has so far never been allocated to a German aircraft type, but it would perfectly fit in time before the Tornado (which has 43+XX and higher numbers).

 

The paint scheme is supposed to be experimental - and actually both Luftwaffe and Marineflieger had been testing tactical camouflage schemes for air superiority as well as ground attack purposes on a wide range of aircraft in the 70ies and 80ies, including F-4F, RF-4E, Alpha Jets and later also Tornados. Anyway, I decided to stay close to the "real" Norm 87 scheme, which is a bit different from what PantherG suggested in his drawings.

 

The colors I used are authentic: RAL 7009 "Grüngrau" is Revell 67, RAL 7012 "Basaltgrau" is Revell 77 and RAL 5008 "Graublau" is available as Xtracolor X264. Consulting real RAL color samples as benchmarks, I muist say that the Revell tones are very good, but the Xtracolor paint is pretty far off. X264 is rather a dark petrol blue, reminiscent of FS35042. Graublau is much more dull and grey-ish, rather a bluish FS36081 - and on real aircraft it almost looks like tar, no blue hue at all to detect.

Anyway, I still used X264, since my 42+15 would sport an experimental paint scheme, so it would not matter much - and X264 would still be the darkest tone of the paint scheme, with good contrast to RAL 7009 and 7012, which are very similar and have almost no contrast. Interesting scheme, though, esp. due to its large color bandages all around the hull instead of smaller patches or stripes.

 

Best alternative I could find is Humbrol 77, which is still too greenish, though - mixing it 1:1 with Humbrol 32 might yield something that comes close to RAL 5008.

 

With a little shading with lighter tones (including RLM 71 from Testors, Humbrol 79 and 77, as well as some acryllic dark grey as an overall filter), a black ink wash and some dry-brushing the contrast was enhanced and the surface slightly weathered. German aircraft were kept in good shape, but at times the weather and sunlight would take their toll and bleach the colors, esp. on the upper sides - RAL 7012 would quickly deteriorate into a relatively light grey with a slight, purple hue!

 

Both Cerberus and BOZ-101 pods were painted in different shades of grey, though, as if they'd belong to a differently camouflaged Marineflieger aircraft. The Kormoran missiles were painted according to pics of the real thing, in a dark olive drab color.

 

National markings and some German stencils were taken from an Xtradecal sheet for German Tornados, as well as from a sheet of an Italeri Tornado with Luftwaffe markings. The tactical codes were created from single digits from a respective TL Modellbau decal sheet.

 

Cockpit interior was painted in a very dark grey, according to pictures from the real Sue. The air intake interior and the landing gear wells were kept in aluminum (Humbrol 56), while the landing gear struts received a mix of aluminum and white.

   

In the end, a simple project: only a fantasy paint scheme and some minor changed details to the OOB kit. But the German wraparound scheme suits the Sue well, and its service introduction in France as well as the retirement of the German Starfighters in the early 80ies makes this a potentially convincing and plausible whif. And, honestly, it was actually a relief from some recent major kit conversions and kitbashings - and a tribute to the creative spirit of PantherG at whatifmodelers.com. ^^

Some of you may have noticed that, unfortunately, owing to the fact that a certain person who sells truck photos on eBay commercially has been lifting my images from this album and selling them I have had to remove 2300 photos that didn't have a watermark. I have now run around 1700 through Lightroom and added a watermark with the intention of bulk uploading them again. Rather than watermark the existing (hidden) files in Flickr one at a time it will be easier to do it this way. I definitely won’t be adding individual tags with the make and model of each vehicle I will just add generic transport tags. Each photo is named after the vehicle and reg in any case. For anyone new to these images there is a chapter and verse explanation below. It is staggering how many times I get asked questions that a quick scan would answer or just as likely I can’t possibly answer – I didn’t take them, but, just to clarify-I do own the copyright- and I do pursue copyright theft.

 

This is a collection of scanned prints from a collection of photographs taken by the late Jim Taylor A number of years ago I was offered a large number of photographs taken by Jim Taylor, a transport photographer based in Huddersfield. The collection, 30,000 prints, 20,000 negatives – and copyright! – had been offered to me and one of the national transport magazines previously by a friend of Jim's, on behalf of Jim's wife. I initially turned them down, already having over 30,000 of my own prints filed away and taking space up. Several months later the prints were still for sale – at what was, apparently, the going rate. It was a lot of money and I deliberated for quite a while before deciding to buy them. I did however buy them directly from Jim’s wife and she delivered them personally – just to quash the occasional rumour from people who can’t mind their own business. Although some prints were sold elsewhere, particularly the popular big fleet stuff, I should have the negatives, unfortunately they came to me in a random mix, 1200 to a box, without any sort of indexing and as such it would be impossible to match negatives to prints, or, to even find a print of any particular vehicle. I have only ever looked at a handful myself unless I am scanning them. The prints are generally in excellent condition and I initially stored them in a bedroom without ever looking at any of them. In 2006 I built an extension and they had to be well protected from dust and moved a few times. Ultimately my former 6x7 box room office has become their (and my own work’s) permanent home.

I hope to avoid posting images that Jim had not taken his self, however should I inadvertently infringe another photographers copyright, please inform me by email and I will resolve the issue immediately. There are copyright issues with some of the photographs that were sold to me. A Flickr member from Scotland drew my attention to some of his own work amongst the first uploads of Jim’s work. I had a quick look through some of the 30 boxes of prints and decided that for the time being the safest thing for me to do was withdraw the majority of the earlier uploaded scans and deal with the problem – which I did. whilst the vast majority of the prints are Jims, there is a problem defining copyright of some of them, this is something that the seller did not make clear at the time. I am reasonably confident that I have since been successful in identifying Jims own work. His early work consists of many thousands of lustre 6x4 prints which are difficult to scan well, later work is almost entirely 7x5 glossy, much easier to scan. Not all of the prints are pin sharp but I can generally print successfully to A4 from a scan.

 

You may notice photographs being duplicated in this Album, unfortunately there are multiple copies of many prints (for swapping) and as I have to have a system of archiving and backing up I can only guess - using memory - if I have scanned a print before. The bigger fleets have so many similar vehicles and registration numbers that it is impossible to get it right all of the time. It is easier to scan and process a print than check my files - on three different PC’s - for duplicates. There has not been, nor will there ever be, any intention to knowingly breach anyone else's copyright. I have presented the Jim Taylor collection as exactly that-The Jim Taylor Collection- his work not mine, my own work is quite obviously mine.

Unfortunately, many truck spotters have swapped and traded their work without copyright marking it as theirs. These people never anticipated the ease with which images would be shared online in the future. I would guess that having swapped and traded photos for many years that it is almost impossible to control their future use. Anyone wanting to control the future use of their work would have been well advised to copyright mark their work (as many did) and would be well advised not to post them on photo sharing sites without a watermark as the whole point of these sites is to share the image, it is very easy for those that wish, to lift any image, despite security settings, indeed, Flickr itself, warns you that this is the case. It was this abuse and theft of my material that led me to watermark all of my later uploads. I may yet withdraw non-watermarked photos, I haven’t decided yet. (I did in the end)

To anyone reading the above it will be quite obvious that I can’t provide information regarding specific photos or potential future uploads – I didn’t take them! There are many vehicles that were well known to me as Jim only lived down the road from me (although I didn’t know him), however scanning, titling, tagging and uploading is laborious and time consuming enough, I do however provide a fair amount of information with my own transport (and other) photos. I am aware that there are requests from other Flickr users that are unanswered, I stumble across them months or years after they were posted, this isn’t deliberate. Some weekends one or two “enthusiasts” can add many hundreds of photos as favourites, this pushes requests that are in the comments section ten or twenty pages out of sight and I miss them. I also have notifications switched off, I receive around 50 emails a day through work and I don’t want even more from Flickr. Other requests, like many other things, I just plain forget – no excuses! Uploads of Jim’s photos will be infrequent as it is a boring pastime and I would much rather work on my own output.

 

F.A.C.T.S. 2013

Ghent, Belgien

 

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www.flickr.com/photos/mchenryarts/

www.facebook.com/McHenryArts

I consider myself a very lucky woman. Because, even if it made me suffer a lot, I always had the courage to accept the facts, and not to lie to myself.

And I don't like to delete good memories.They are a part of me, of the person I am, and of the better person I can be!

Have a great saturday you all, I'm going to town tonight, to see a show: maybe I'll take some good shot!

ciaoooo :)))

C.B. Tryon, Typographer

+++ 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 origins of the mighty Hawker Harpy date back until the late 1940ies, when the British MoD issued a specification for "an interceptor fighter with supersonic performance" under the handle F.23/49. In May 1949 OR.268 was prepared and finally issued in April 1950. It called for a twin-engine single-seat supersonic fighter to operate in Europe and desirably any other part of the world. The initial design requirements were not too demanding: a top speed of at least Mach 1.2 was called for, with climb to 50.000' (15.240m) in no more than 360 seconds. The fighter had to have a rate of climb of at least 1.000'/min (305m/min) and a minimum endurance from take-off to landing of at least 60min. At least two 30mm Aden cannon were to be carried.

 

At this stage, two companies submitted proposals: English Electric with the P.1, which should become the eventual winning design as the formidable Mach 2-capable BAC Lightning, and Hawker with the P.1082 and P.1086 designs. P.1082 was a sleek, supersonic development of the Hawker Hunter, which was rejected, as it only featured a single, reheated engine and too little future development potential. P.1086 vaguely resembled the later Soviet Su-15 interceptor with two engines side by side in the rear fuselage, fed by lateral air intakes and featured a cropped delta wing, paired with swept tail surfaces. P.1086 was rejected, too, as it fell short in performance in comparison with the P.1, even though the range would have been better.

 

As the Lightning entered production and service after a long and troublesome development phase until the late 1950ies, technical advances and new threats through supersonic bombers like the Tupolev Tu-22, armed with long range air-to-ground missiles had emerged. While the Lightning was an excellent interceptor with an outstanding rate of climb and a top speed of more than Mach 2.0at height, it had several shortcomings that could never really be rectified: one flaw was its limited payload of two guided AAMs (initially IR-guided Firestreaks, later radar-guided Red Top AAMs), but its biggest shortcoming was the very limited range that left esp. in the northern regions of Great Britain a defense gap.

 

This led in in 1955 to the requirement for a 'Day-Night High Altitude Fighter Aircraft' under OR.239/F.155, which was to be able to operate against enemy bombers coming in at 60.000' (18.288m) altitude and at Mach 1.3, with service entry as soon as possible and not beyond 1963 (the BAC Lightning was considered to be sufficient until about 1960). A new radar was to be developed for the aircraft, operated by a second crew member.

 

Almost all British manufacturers submitted designs, including Hawker with several proposals like the P.1103, a large aircraft based on the Hunter with a chin air intake and missile rails on its wing tips. There was also the P.1110, a much revised P.1086 design - basically an enlarged and much refined version of the 1950 concept, but now with an area-ruled fuselage and powered by two Sapphire Sa.7LR engines, rated at 11.000lb (48.9kN) dry thrust and at 15.400lb (68.4kN) with full afterburner and optimized for high altitude duty.

 

The P.1110 was still a single-seater, though, equipped with the same AI.23B radar as the BAC Lightning, which it was to support, not to replace. The Ferranti AI.23 radar supported autonomous search, automatic target tracking, and ranging for all weapons, while the pilot attack sight provided gyroscopically derived lead angle and backup stadiametric ranging for gun firing. The radar and gunsight were collectively designated the AIRPASS: Airborne Interception Radar and Pilot Attack Sight System.

 

The P.1110’s selling point was its long range (the combat radius exceeded the Lightning’s maximum range), coupled with a top speed of more than Mach 2 and the ability to carry up to six (normal payload would be four) AAMs, plus two internal cannons. Another factor that made the Hawker aircraft attractive was that it was a simple design, bearing no visible development risk, and that the bigger radome offered the option to install not only a larger antenna, but also offered the possibility to install an overall much more powerful radar system that would be more suitable for the primary long-range interception task of the type.

 

Even though Fairey’s (based on the famous Delta research aircraft) and Armstrong Whitworth’s designs were officially favored, things went in a totally different direction: in early 1957 the MoD issued its infamous White Paper that basically rang the death knell to all new fighter developments - axing the F.155 program in favor of ground-based missile defense systems – the manned fighter was considered obsolete over night!

 

Anyway, things would not change that fast in real life, and this gave way for the “last manned fighter” for the RAF: the P.1110. It was clear that it was just a stopgap solution, as the Lightning would, if any interceptor development was cut down, be the only operative interceptor for Great Britain in the near future, leaving the aforementioned weak spots esp. at the northern borders. A foreign potential option for the required aircraft, the mighty CF-105 'Arrow' from Canada, had also been recently cancelled, so the modified P.1110 was seen as the most cost-efficient domestic solution.

 

Work started fast and at good pace: the first P.1110 prototype (a total of four were to be built, one of them only a static airframe for ground tests) already made its maiden flight in September 1959. As it relied on proven avionics the type became ready for service in early 1961. The new aircraft was christened ‘Harpy F.1’ and it served alongside the BAC Lightning interceptors on long range patrol flights, high altitude interceptions and in QRA service. It partly replaced older Gloster Javelin versions in the all-weather fighter role.

 

Beyond the primary missile-toting interceptor role the Harpy could also carry an impressive load of up to 10.000 lb (4.540 kg) of other ordnance, including Matra rocket pods and iron or cluster bombs of up to 1.000 lb (454 kg) caliber.

 

The Harpy was a big aircraft and not really suited for dogfight scenarios, but it had - in contrast to the Lightning - a spacious cockpit which made long flights agreeable. Take-off and landing speeds were comparatively high, though, with a take-off speed of 231 mph (370 km/h). While the controls were responsive and precise, the aircraft was unforgiving of pilot error. Indeed, the type's attrition rate was high: 18 aircraft would be lost through accidents.

 

As only 65 were built, operating the type was costly, and towards the late 1960s already a more economical solution was searched for. The aging Lightning fleet also started to call for a replacement. The pure missile air defense had quickly turned out to be a political error, but in its wake it had caused severe consequences for Britain's aircraft industry, as aircraft development had been cut back. Eventually, as domestic types were lacking, the Spey-engined McDonnell F-4 Phantom II entered RAF service (after having been bought for the Royal Navy in the first place) in 1969.

 

Both Lightning and Harpy suffered in service under the high work load for the pilot, who had not only to engage a potential enemy at high speed but also had to operate the radar and weapons system at the same time. Another limiting factor for both types' effectiveness was the more and more obsolete Firestreak and Red Top missiles, which only had an effective range of up to 7.5 miles (12 km) and relied on IR homing. Plans to outfit the Lightning with American Falcons, Sparrows or even Sidewinders in 1958 were fruitless (either necessitating an altogether new fire control system or limiting the aircraft's performance), so that the Harpy would not benefit from more capable weapons, too - even though it offered the better development basis with its bigger radome, range and payload.

 

Only few hardware updates were actually made during the Hawker Harpy’s active service period, including the addition of a removable, fixed in-flight refueling probe, an improved escape system along with additional room for more electronic counter-measures equipment. By 1973 all machines were modified accordingly and re-designated F.1A.

 

Both Harpy and Lightning were hard to replace, though, as the RAF Phantoms initially also had to fill out an attack and reconnaissance role (a gap which was to be filled with the SEPECAT Jaguar), so both interceptors soldiered on until the early 1980ies. Both were replaced by the Phantoms, the large Harpy made its final flight in May 1982 while the last Lightning was retired in 1988, as the Tornado ADV was under development and would unite what even the couple of Harpy and Lighning never achieved in their service career.

  

General characteristics:

Crew: 1

Length: 21.52 m (70 ft 7 in)

Wingspan: 9.34 m (30 ft 8 in)

Height: 5.41 m (17 ft 9 in)

Wing area: 42.2 m² (454 ft 3 in)

Empty weight: 10,371 kg (22,864 lb)

Loaded weight: 15,288 kg (33,704 lbf)

Max. take-off weight: 18,879 kg (41,621 lbf)

 

Powerplant:

2× reheated Armstrong Siddeley Sapphire Sa.7LR engines, rated at 11.000lb (48.9kN) dry thrust and at 15.400lb (68.4kN) with afterburner

 

Performance:

Maximum speed: Mach 2.1

Combat radius with 5 min combat: 647 nmi (746 mi, 1,200 km)

Ferry range: 1.403 nmi (1.615 mi, 2.600 km) with 3 external fuel tanks

Service ceiling: 18.100 m (59.383 ft)

Rate of climb: 83 m/s (16.405 ft/min)

Wing loading: 447.4 kg/m² (MAX T-O Weight) (91.63 lb/ft² (MAX T-O Weight))

Thrust/weight: 0.5; 0.91 with afterburner (MAX T-O Weight)

 

Armament:

2× Aden 30mm (1.18”) cannons under the air intakes with 120 RPG

7× hard points (6 under wing and one centerline hard point) for air-to-air missiles (Firestreak or, from 1965 on, primarily Red Top), fuel on three wet pylons, or bombs, Matra pods with 18 unguided 68mm SNEB rockets, for a total maximum load of 10.000 lb (4.540 kg)

  

The kit and its assembly:

Hopefully royalists will forgive me for this... but did you ever see an aircraft and get the spontaneous idea what it actually could be or have been? Well, the Chinese J-8II is such a case. In fact, the J-8 was born as a scaled-up MiG-21F with two engines, and it was later modified to carry a nose radome and lateral air intakes. Somehow this large jet fighter had IMHO a British look about it… I couldn't help, it HAD to become an RAF aircraft! Totally anachronistic, but worth the try ;).

 

Anyway, it is still SO retro that I had to put even the modernized version back in time by about 20 years, when it would have been up to date. Just for reference: imagine that the real J-8II entered service in China when the Harpy was retired after 20 years of service in my fictional background story…

  

Well, to be honest I have had this one on my idea list for a long time, but as it would ‘just’ be an almost OOB build I always held in back, favoring more complicated works. Anyway, as I had a Trumpeter J-8II kit in store AND appropriate decals I decided to work the Harpy out as the first kit in 2014.

 

As already mentioned, this is an almost OOB build of the Trumpeter J-8II (NATO code 'Finback B'), with only minor modifications. The kit is very nice: Fit is good, you get recessed panel lines, as many details as you can ask for – just some fit issues with the fuselage halves and slight sink holes at the air intakes. While you need some putty, anyway, the thing goes together very easily.

 

Personal mods to create the Hawker Harpy include a Matchbox pilot figure for the cockpit, two fins ('Finback A' style) instead of the J-8II's single MiG-23 style folding fin, new drop tanks (from a Matchbox Hawker Hunter, with fins added) and four Red Top missiles (from an Eastern Express Sea Vixen) – all for a convincing RAF look.

 

Other small mods include e. g. getting rid of some typical Soviet-style antennae (even though I kept the almost iconic anti-flutter weights on the tailplane) and the GSh-23-2 cannon fairing under the fuselage, which was replaced by two single gun fairings for 30mm Aden cannons under the air intakes.

  

Painting and markings:

Classic RAF colors from the Sixties, with Dark Slate Gray/Dark Sea Gray from above and Light Aircraft Gray below (Humbrol 163, 164 and 166, respectively). The aircraft received a light black ink wash in order to emphasize the kit’s fine engraved panel lines, as well as some dry-painting with lighter shades (including Dark Slate Gray/Dark Sea Gray from Modelmaster – these tones are a tad lighter than the Humbrol counterparts, and Humbrol 196, RAL 7035).

 

The cockpit interior was painted in dark gray, while the landing gear wells and the other interiors were left in Aluminum. The landing gear was painted in Steel, the wheel discs white and the air brakes in red from the inside.

 

Decals/markings come from an Xtradecal sheet for RAF Phantom FG.1/FGR.2s, "XL196" is, AFAIK, a ‘free’ (never used) RAF serial number that fits around 1962. Some additional stencils and markings were painted onto the fuselage by brush.

 

After decal application the kit received an overall coat of semi-gloss Tamiya acrylic varnish.

  

The Hawker Harpy is/was simple kit travesty, but IMHO the resulting ‘British product’ looks very convincing and late-1950ies style?

 

The Zender Fact 4 Spider at the Essen Motorshow.

 

Scanned photograph from 1993.

NEAR IS PROUD TO ANNOUNCE the next chapter in the on-going struggle against The Man to document our railroad. NEAR will release a quarterly photo book (and accompanying DVD when available) highlighting the photography of several railroaders from North America. First up, our long time partner Wade Arthur and his Zine/DVD combo "FICTIONAL FACTS". Pre orders start NOV 1st!

Some of you may have noticed that, unfortunately, owing to the fact that a certain person who sells truck photos on eBay commercially has been lifting my images from this album and selling them I have had to remove 2300 photos that didn't have a watermark. I have now run around 1700 through Lightroom and added a watermark with the intention of bulk uploading them again. Rather than watermark the existing (hidden) files in Flickr one at a time it will be easier to do it this way. I definitely won’t be adding individual tags with the make and model of each vehicle I will just add generic transport tags. Each photo is named after the vehicle and reg in any case. For anyone new to these images there is a chapter and verse explanation below. It is staggering how many times I get asked questions that a quick scan would answer or just as likely I can’t possibly answer – I didn’t take them, but, just to clarify-I do own the copyright- and I do pursue copyright theft.

  

This is a collection of scanned prints from a collection of photographs taken by the late Jim Taylor A number of years ago I was offered a large number of photographs taken by Jim Taylor, a transport photographer based in Huddersfield. The collection, 30,000 prints, 20,000 negatives – and copyright! – had been offered to me and one of the national transport magazines previously by a friend of Jim's, on behalf of Jim's wife. I initially turned them down, already having over 30,000 of my own prints filed away and taking space up. Several months later the prints were still for sale – at what was, apparently, the going rate. It was a lot of money and I deliberated for quite a while before deciding to buy them. I did however buy them directly from Jim’s wife and she delivered them personally – just to quash the occasional rumour from people who can’t mind their own business. Although some prints were sold elsewhere, particularly the popular big fleet stuff, I should have the negatives, unfortunately they came to me in a random mix, 1200 to a box, without any sort of indexing and as such it would be impossible to match negatives to prints, or, to even find a print of any particular vehicle. I have only ever looked at a handful myself unless I am scanning them. The prints are generally in excellent condition and I initially stored them in a bedroom without ever looking at any of them. In 2006 I built an extension and they had to be well protected from dust and moved a few times. Ultimately my former 6x7 box room office has become their (and my own work’s) permanent home.

 

I hope to avoid posting images that Jim had not taken his self, however should I inadvertently infringe another photographers copyright, please inform me by email and I will resolve the issue immediately. There are copyright issues with some of the photographs that were sold to me. A Flickr member from Scotland drew my attention to some of his own work amongst the first uploads of Jim’s work. I had a quick look through some of the 30 boxes of prints and decided that for the time being the safest thing for me to do was withdraw the majority of the earlier uploaded scans and deal with the problem – which I did. whilst the vast majority of the prints are Jims, there is a problem defining copyright of some of them, this is something that the seller did not make clear at the time. I am reasonably confident that I have since been successful in identifying Jims own work. His early work consists of many thousands of lustre 6x4 prints which are difficult to scan well, later work is almost entirely 7x5 glossy, much easier to scan. Not all of the prints are pin sharp but I can generally print successfully to A4 from a scan.

  

You may notice photographs being duplicated in this Album, unfortunately there are multiple copies of many prints (for swapping) and as I have to have a system of archiving and backing up I can only guess - using memory - if I have scanned a print before. The bigger fleets have so many similar vehicles and registration numbers that it is impossible to get it right all of the time. It is easier to scan and process a print than check my files - on three different PC’s - for duplicates. There has not been, nor will there ever be, any intention to knowingly breach anyone else's copyright. I have presented the Jim Taylor collection as exactly that-The Jim Taylor Collection- his work not mine, my own work is quite obviously mine.

 

Unfortunately, many truck spotters have swapped and traded their work without copyright marking it as theirs. These people never anticipated the ease with which images would be shared online in the future. I would guess that having swapped and traded photos for many years that it is almost impossible to control their future use. Anyone wanting to control the future use of their work would have been well advised to copyright mark their work (as many did) and would be well advised not to post them on photo sharing sites without a watermark as the whole point of these sites is to share the image, it is very easy for those that wish, to lift any image, despite security settings, indeed, Flickr itself, warns you that this is the case. It was this abuse and theft of my material that led me to watermark all of my later uploads. I may yet withdraw non-watermarked photos, I haven’t decided yet. (I did in the end)

 

To anyone reading the above it will be quite obvious that I can’t provide information regarding specific photos or potential future uploads – I didn’t take them! There are many vehicles that were well known to me as Jim only lived down the road from me (although I didn’t know him), however scanning, titling, tagging and uploading is laborious and time consuming enough, I do however provide a fair amount of information with my own transport (and other) photos. I am aware that there are requests from other Flickr users that are unanswered, I stumble across them months or years after they were posted, this isn’t deliberate. Some weekends one or two “enthusiasts” can add many hundreds of photos as favourites, this pushes requests that are in the comments section ten or twenty pages out of sight and I miss them. I also have notifications switched off, I receive around 50 emails a day through work and I don’t want even more from Flickr. Other requests, like many other things, I just plain forget – no excuses! Uploads of Jim’s photos will be infrequent as it is a boring pastime and I would much rather work on my own output.

     

NASA Armstrong Fact Sheet: D-558-II ''Skyrocket''

 

The Douglas D-558-II "Skyrockets" were among the early transonic research airplanes like the X-1, X-4, X-5, and X-92A. Three of the single-seat, swept-wing aircraft flew from 1948 to 1956 in a joint program involving the National Advisory Committee for Aeronautics (NACA), with its flight research done at the NACA's Muroc Flight Test Unit in California, redesignated in 1949 the High-Speed Flight Research Station (HSFRS); the Navy-Marine Corps; and the Douglas Aircraft Co. The HSFRS is now known as the NASA Dryden Flight Research Center. The Skyrocket made aviation history when it became the first airplane to fly twice the speed of sound.

NASA Armstrong Fact Sheet: D-558-II Skyrocket

The Douglas D-558-II "Skyrockets" were among the early transonic research airplanes like the X-1, X-4, X-5, and X-92A. Three of the single-seat, swept-wing aircraft flew from 1948 to 1956 in a joint program involving the National Advisory Committee for Aeronautics (NACA), with its flight research done at the NACA's Muroc Flight Test Unit in California, redesignated in 1949 the High-Speed Flight Research Station (HSFRS); the Navy-Marine Corps; and the Douglas Aircraft Co. The HSFRS is now known as the NASA Dryden Flight Research Center. The Skyrocket made aviation history when it became the first airplane to fly twice the speed of sound.

 

The II in the aircraft's designation referred to the fact that the Skyrocket was the phase-two version of what had originally been conceived as a three-phase program, with the phase-one aircraft having straight wings. The third phase, which never came to fruition, would have involved constructing a mock-up of a combat-type aircraft embodying the results from the testing of the phase one and two aircraft.

 

The D-558-II was first flown on Feb. 4, 1948, by John Martin, a Douglas test pilot. An NACA pilot, Scott Crossfield, became the first person to fly faster than twice the speed of sound when he piloted the D-558-II to its maximum speed of Mach 2.005 (1,291 mph) at 62,000 feet altitude on Nov. 20, 1953. Its peak altitude, 83,235 feet, a record in its day, was reached with Lt. Col. Marion Carl at the controls.

 

The three aircraft gathered a great deal of data about pitch-up and the coupling of lateral (yaw) and longitudinal (pitch) motions; wing and tail loads, lift, drag, and buffeting characteristics of swept-wing aircraft at transonic and supersonic speeds; and the effects of the rocket exhaust plume on lateral dynamic stability throughout the speed range. (Plume effects were a new experience for aircraft.) The number three aircraft also gathered information about the effects of external stores (bomb shapes, drop tanks) upon the aircraft's behavior in the transonic region (roughly 0.7 to 1.3 times the speed of sound).

 

In correlation with data from other early transonic research aircraft such as the XF-92A, this information contributed to solutions to the pitch-up problem in swept-wing aircraft.

  

Design

 

The need for transonic research airplanes grew out of two conditions that existed in the early 1940s. One was the absence of accurate wind tunnel data for the speed range from roughly Mach 0.8 to 1.2. The other was the fact that fighter aircraft like the P-38 "Lightning" were approaching these speeds in dives and breaking apart from the effects of compressibility-increased density and disturbed airflow as the speed approached that of sound, creating shock waves. People in the aeronautics community - especially the NACA, the Army Air Forces (AAF), and the Navy-agreed on the need for a research airplane with enough structural strength to withstand compressibility effects in the transonic region. The AAF preferred a rocket-powered aircraft and funded the X-1, while the NACA and Navy preferred a more conservative design and pursued the D-558, with the NACA also supporting the X-1 research.

 

The Navy contracted with Douglas to design the airplane, and in the course of the design process, the D-558 came to be divided into two separate phases, with phase one being a straight-wing turbojet aircraft and phase two consisting of a swept-wing design with turbojet and rocket propulsion. At the NACA's suggestion, based on the research of Robert Jones at Langley and captured German documents, Douglas and the Navy had agreed to the swept-wing design, and to provide sufficient power to propel the swept-wing airplane past Mach 1, they also agreed to add rocket propulsion.

 

Then, to fit both a turbojet and rocket engine in the phase two aircraft required a new fuselage. Like the D-558-I, the Skyrocket featured a horizontal stabilizer high on the vertical tail to avoid the wake from the wing. As with the X-1 and the D-558-I, the Skyrocket also featured, at NACA suggestion, a horizontal stabilizer that was thinner than the wing and movable in flight so as to avoid simultaneous shock wave effects for the wing and horizontal tail and to provide pitch (nose up or down) control when shock waves made the elevators ineffective. While Douglas was constructing the D-558-IIs, the NACA continued to furnish the contractor data it needed on aircraft performance based on tests in Langley wind tunnels and with rocket-propelled models from the Wallops Island Pilotless Aircraft Research Station.

  

Program History

 

The three airplanes flew a total of 313 times-123 by the number one aircraft (Bureau No. 37973-NACA 143), 103 by the second Skyrocket (Bureau No. 37974-NACA 144), and 87 by airplane number three (Bureau No. 37975-NACA 145). Skyrocket 143 flew all but one of its missions as part of the Douglas contractor program to test the airplane's performance.

 

NACA aircraft 143 was initially powered by a Westinghouse J-34-40 turbojet engine configured only for ground take-offs, but in 1954-55 the contractor modified it to an all-rocket air-launch capability featuring an LR8-RM-6, 4-chamber Reaction Motors engine rated at 6,000 pounds of thrust at sea level (the Navy designation for the Air Force's LR-11 used in the X-1). In this configuration, NACA research pilot John McKay flew the airplane only once for familiarization on September 17, 1956. The 123 flights of NACA 143 served to validate wind-tunnel predictions of the airplane's performance, except for the fact that the airplane experienced less drag above Mach 0.85 than the wind tunnels had indicated.

 

NACA 144 also began its flight program with a turbojet powerplant. NACA pilots Robert A. Champine and John H. Griffith flew 21 times in this configuration to test airspeed calibrations and to research longitudinal and lateral stability and control. In the process, during August of 1949 they encountered pitch-up problems, which NACA engineers recognized as serious because they could produce a limiting and dangerous restriction on flight performance. Hence, they determined to make a complete investigation of the problem.

 

In 1950, Douglas replaced the turbojet with an LR-8 rocket engine, and its pilot, William B. Bridgeman, flew the aircraft seven times up to a speed of Mach 1.88 (1.88 times the speed of sound) and an altitude of 79,494 feet (the latter an unofficial world's altitude record at the time, achieved on August 15, 1951). In the rocket configuration, a Navy P2B (Navy version of the B-29) launched the airplane at approximately 30,000 feet after taking off from the ground with the Skyrocket attached beneath its bomb bay. During Bridgeman's supersonic flights, he encountered a violent rolling motion known as lateral instability that was less pronounced on the Mach 1.88 flight on August 7, 1951, than on a Mach 1.85 flight in June when he pushed over to a low angle of attack (angle of the fuselage or wing to the prevailing wind direction).

 

The NACA engineers studied the behavior of the aircraft before beginning their own flight research in the airplane in September 1951. Over the next couple of years, NACA pilot A. Scott Crossfield flew the airplane 20 times to gather data on longitudinal and lateral stability and control, wing and tail loads, and lift, drag, and buffeting characteristics at speeds up to Mach 1.878.

 

At that point, Marine Lt. Col. Marion Carl flew the airplane to a new (unofficial) altitude record of 83,235 feet on August 21, 1953, and to a maximum speed of Mach 1.728.

 

Following Carl's completion of these flights for the Navy, NACA technicians at the High-Speed Flight Research Station (HSFRS) near Mojave, CA, outfitted the LR-8 engine's cylinders with nozzle extensions to prevent the exhaust gas from affecting the rudders at supersonic speeds. This addition also increased the engine's thrust by 6.5 percent at Mach 1.7 and 70,000 feet.

 

Even before Marion Carl had flown the Skyrocket, HSFRS Chief Walter C. Williams had petitioned NACA headquarters unsuccessfully to fly the aircraft to Mach 2 to garner the research data at that speed. Finally, after Crossfield had secured the agreement of the Navy's Bureau of Aeronautics, NACA director Hugh L. Dryden relaxed the organization's usual practice of leaving record setting to others and consented to attempting a flight to Mach 2.

 

In addition to adding the nozzle extensions, the NACA flight team at the HSFRS chilled the fuel (alcohol) so more could be poured into the tank and waxed the fuselage to reduce drag. With these preparations and employing a flight plan devised by project engineer Herman O. Ankenbruck to fly to approximately 72,000 feet and push over into a slight dive, Crossfield made aviation history on November 20, 1953, when he flew to Mach 2.005 (1,291 miles per hour). He became the first pilot to reach Mach 2 in this, the only flight in which the Skyrocket flew that fast.

 

Following this flight, Crossfield and NACA pilots Joseph A. Walker and John B. McKay flew the airplane for such purposes as to gather data on pressure distribution, structural loads, and structural heating, with the last flight in the program occurring on December 20, 1956, when McKay obtained dynamic stability data and sound-pressure levels at transonic speeds and above.

 

Meanwhile, NACA 145 had completed 21 contractor flights by Douglas pilots Eugene F. May and Bill Bridgeman in November 1950. In this jet-and-rocket-propelled craft, Scott Crossfield and Walter Jones began the NACA's investigation of pitch-up lasting from September 1951 well into the summer of 1953. They flew the Skyrocket with a variety of wing-fence, wing-slat, and leading-edge chord extension configurations, performing various maneuvers as well as straight-and-level flying at transonic speeds. While fences significantly aided recovery from pitch-up conditions, leading edge chord extensions did not, disproving wind-tunnel tests to the contrary. Slats (long, narrow auxiliary airfoils) in the fully open position eliminated pitch-up except in the speed range around Mach 0.8 to 0.85.

 

In June 1954, Crossfield began an investigation of the effects of external stores (bomb shapes and fuel tanks) upon the aircraft's transonic behavior. McKay and Stanley Butchart completed the NACA's investigation of this issue, with McKay flying the final mission on August 28, 1956.

 

Besides setting several records, the Skyrocket pilots had gathered important data and understanding about what would and would not work to provide stable, controlled flight of a swept-wing aircraft in the transonic and supersonic flight regimes. The data they gathered also helped to enable a better correlation of wind-tunnel test results with actual flight values, enhancing the abilities of designers to produce more capable aircraft for the armed services, especially those with swept wings. Moreover, data on such matters as stability and control from this and other early research airplanes aided in the design of the century series of fighter airplanes, all of which featured the movable horizontal stabilizers first employed on the X-1 and D-558 series.

  

The Aircraft

 

All three of the Skyrockets had a height of 12 feet 8 inches, a length of 42 feet, and 35-degree swept wings with a span of 25 feet.

 

Image right: D-558-II wing configurations.

 

Until configured for air launch, NACA 143 featured a Westinghouse J-34-40 turbojet engine rated at 3,000 lb of static thrust. It carried 260 gallons of aviation gasoline and weighed 10,572 lb at take-off.

 

NACA 144 (and NACA 143 after modification in 1955) was powered by an LR-8-RM-6 rocket engine rated at 6,000 pounds of static thrust. Its propellants were 345 gallons of liquid oxygen and 378 gallons of diluted ethyl alcohol. In its launch configuration, it weighed 15,787 lb.

 

NACA 145 had both an LR-8-RM-5 rocket engine rated at 6,000 pounds of static thrust and featured a Westinghouse J-34-40 turbojet engine rated at 3,000 pounds of static thrust. It carried 170 gallons of liquid oxygen, 192 gallons of diluted ethyl alcohol, and 260 gallons of aviation gasoline for a launch weight of 15,266 lb.

 

NACA 143 is currently in storage at the Planes of Fame Museum, Ontario, CA. The second Skyrocket, NACA 144, is in the Smithsonian Institution's National Air and Space Museum in Washington, DC. NACA 145 is on display in front of the Antelope Valley College in Lancaster, CA.

  

P2B-1S BuNo 84029 (Formerly B-29-95-BW 45-21787) “Fertile Myrtle” (which carried the Douglas D-558-II Skyrocket research aircraft) was donated to an aviation museum in Oakland, California in 1984. It was sold to the Kermit Weeks Aviation Museum of Miami, Florida, and is on the US Civil register as N29KW. There may be an attempt to restore this plane to flying condition, using as parts some airframes acquired from the US Naval Weapons Center at China Lake, California.

+++ DISCLAIMER +++

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

 

Some background:

In October 1951, a heavy tank project was underway to mount an oscillating turret with an automatically loading 120mm Gun on the hull of the 120mm Gun Tank T43. (The T43 would later be serialized as the 120mm Gun Tank M103, America’s last heavy tank.). This was the T57, and the Rheem Manufacturing Company were granted a contract to design and build two pilot turrets and autoloading systems.

During the T57’s development, it became clear that it was feasible to mount a lighter armored version of the T57 turret on the hull of the 90mm Gun Tank T48 (The T48 later became the 90mm Gun Tank M48 Patton). This combination granted the possibility of creating a ‘heavy gun tank’ that was considerably lighter (and therefore more agile and tactically flexible) than any previously designed.

In May 1953, a development project was started to create such a tank. It would be designated the 120mm Gun Tank T77, and another contract was signed with Rheem to create two pilot tanks. The T77 weighed about 50 tons, with armor of the hull being up to 110mm thick. It was originally powered by a 650 hp Continental AVSI-1790-6 V12, air-cooled twin-turbo gasoline engine. This would propel the tank to a speed of 30 mph (48 km/h). The tank was supported on a torsion bar suspension, attached to six road wheels. The drive sprocket was at the rear, while the idler was at the front. The idler wheel was of the compensating type, meaning it was attached to the closest roadwheel by an actuating arm. When the roadwheel reacted to terrain, the idler was pushed out or pulled in, keeping constant track tension. The return of the track was supported by five rollers.

 

The T77 had a crew of four: The driver’s position was standard for M48 hulls, located centrally in the bow at the front of the hull. Arrangements inside the turret were standard, too: The loader was positioned to the left of the gun, the gunner was on the right with the commander behind him.

 

The T77’s oscillating turret could be easily mounted to the unmodified 2.1 m (85 inch) turret ring of the M48 hull, and on other tanks, too. It consisted of two actuating parts: a collar that was attached to the turret ring, allowing 360° horizontal traverse, and a pivoting upper part with a long cylindrical ‘nose’ and a low profile flat bustle that held the gun, which could elevate to a maximum of 15 degrees, and depress 8 degrees. It also held the complex loading mechanism and the turret crew.

Both turret halves utilized cast homogeneous steel armor. The sides of the collar were made to be round and bulbous in shape to protect the trunnions that the upper half pivoted on. Armor around the face was 127mm (5 inches) thick, angled at 60 degrees, what meant an effective 10 in (254 mm) equivalent of RHA at the turret front. Maximum armor strength was 137mm (5.3 inches) on the convex sides of the turret, and this dropped to 51 mm (2 inches) on the bustle.

Though it looked like two, there were actually three hatches in the turret’s roof: There was a small hatch on the left for the loader, and the slightly raised cupola for the commander on the right, which featured six periscopes. These two standard hatches were part of a third large, powered hatch, which took up most of the middle of the roof, granting a larger escape route for the crew but also allowed internal turret equipment to be removed easily. It was also a convenient way to replenish the ammunition storage, even though a use under battle conditions was prohibitive. In front of the loader’s hatch was a periscope, housings for a stereoscopic rangefinder were mounted on the sides of the swiveling turret part, and there was another periscope above the gunner’s position, too. Behind the large hatch was the ejection port for spent cartridges, to its right was the armored housing for the ventilator.

 

The initial Rheem Company turret concept had the gun rigidly mounted to the turret without a recoil system, and the long gun barrel protruded from a narrow nose. The gun featured a quick change barrel but was otherwise basically identical to the 120mm Gun T123E1, the gun being trialed on the T43/M103. However, for the T57/77 turret and the autoloader, it was modified to accept single piece ammunition, unlike the T43/M103, which used separately loading ammo due to the round’s high weight. This new gun was attached to the turret via a conical adapter that surrounded the breech end of the gun. One end screwed directly into the breech, while the front half extended through the ‘nose’ and was secured in place by a large nut. The force created by the firing of the gun and the projectile traveling down the rifled barrel was resisted by rooting the adapter both the breech block and turret ring. As there was no inertia from recoil to automatically open the horizontally sliding breech block, a hydraulic cylinder was introduced. Upon firing the main gun, this hydraulic cylinder was triggered via an electric switch. This new variant of the T123 cannon was designated the 120mm Gun T179. It was fitted with a bore evacuator (fume extractor) and a simple, T-shaped muzzle brake.

A single .30 Caliber (7.62mm) machine gun was mounted coaxially, and another such weapon or a medium 0.5” machine gun could be attached to a mount on the commander’s cupola.

 

Using standard Armor-Piercing Ballistic Cap Tracer Rounds, the T179 was capable of penetrating 221-millimetre (8.7 in) of 30-degree sloped rolled-homogenous armor at 1,000 yards and 196-millimetre (7.7 in) at 2,000 yards. It could also penetrate 124-millimetre (4.9 in) 60-degree sloped rolled-homogenous armor at 1,000 yards and 114-millimetre (4.5 in) at 2,000 yards.

 

The T179’s automatic loader was located below the gun and it gave the weapon a projected rate of fire of 30 rounds per minute, even though this was only of theoretical nature because its cylinder magazine only held 8 rounds. After these had been expended, it had to be manually re-loaded by the crew from the inside, and the cannon could not be operated at that time. Ammunition types such as High-Explosive (HE), High-Explosive Anti-Tank (HEAT), Armor Piercing (AP), or Armor-Piercing Ballistic-Capped (APBC) could be fired and be selected from the magazine via a control panel by either the gunner or the tank commander, so that it was possible to quickly adapt to a changing tactical situation – as long as the right rounds had been loaded into the magazine beforehand.

 

The cannon itself was fed by a ramming arm that actuated between positions relative to the breech and magazine, operating in five major steps:

1) The hydraulically operated ramming arm withdrew a round and aligned it with the breach.

2) The rammer then pushed the round into the breach, triggering it to close.

3) Gun was fired.

4) Effect of gun firing trips the electric switch that opens the breech.

5) Rammer picks up a fresh round, at the same time ejecting the spent cartridge through a trap door in the roof of the turret bustle.

 

Beyond the 8 rounds ready-for fire in the magazine, the main gun had only a very limited ammunition supply due to the large size of the 1-piece rounds: only 21 more 120 mm rounds could be stored in the hull and at the base of the turret.

 

After thorough trials, the T77 was, powered by a more fuel-efficient Continental AVDS-1790-2 V12, air-cooled twin-turbo diesel engine with 750 bhp (560 kW), accepted as a replacement for the U.S. Army‘s unloved heavy M103 and introduced as the M77. The first M77s were assembled at the Detroit Arsenal Tank Plant in March 1964. However, the M77 was primarily a support vehicle for standard tank units and reserved for special operations. Therefore, the type’s production numbers remained low: only 173 tanks were eventually built until 1968 and exclusively allocated to U.S. Army units in Western Germany, with a focus on West Berlin and Southern Germany (e.g. in the Fulda Gap), where they were to repel assaults from Eastern Germany and defend vital installations or critical bottlenecks.

 

Due to its high rate of fire and long range, the M77 was ideally suited for defensive tasks and hit-and-run tactics. But this was, unfortunately, the type’s only selling point: The oscillating turret turned out to be complex, concerning both handling as well as maintenance, and in practice it did not offer the same weapon stability as the M48’s or the later M60’s conventional design, especially when firing during movement. The cramped interior and the many mechanical parts of the bulky autoloader inside of the turret did not make the tank popular among its crews, either. Several accidents occurred during manoeuvers while the loader tried to refill the magazine under combat pressure. A further weakness was the type’s low ammunition stock and the fact that, despite the autoloader, there was still a loader necessary to feed the magazine. The low ammunition stock also heavily limited the tactical value of the tank: typically, the M77 had to leave its position after expending all of its ammunition and move to a second line position, where the huge one-piece rounds could be replenished under safer conditions. But this bound other resources, e. g. support vehicles, and typically the former position had to be given up or supplanted by another vehicle. Operating the M77 effectively turned out to be a logistic nightmare.

 

During its career, the M77 saw only one major upgrade in the mid-Seventies: The M77A1 was outfitted with a new multi-chamber muzzle brake, muzzle reference and crosswind sensors (the latter was mounted in a small mast on the rear of the turret) and an improved turret stabilization system along with an upgraded turret electrical system. All of these measures were intended to improve the tank’s 1st shot kill probability, esp. at long range. A large AN/VSS-1(V)1 white/IR searchlight was added above the gun barrel, too. All tanks in service were upgraded in this fashion, no new tanks were built. Unlike the M48, neither the M77 nor the Rheem turret or its autoloader system were cleared for export, even though Israel showed interest.

 

In the early Eighties, there were further plans for another upgrade of the M77 fleet to a potential A2 status. This would have introduced a laser rangefinder (instead of the purely optical device) and a solid state M21 ballistic computer with a digital databus. The M21 would have allowed a pre-programmed selection and fire sequence of different ammunition types from the magazine’s chambers, plus better range and super-elevation correction. However, this did not happen because the M77 had become obsolete through the simple depletion of its exotic 120 mm ammunition from the army’s stocks. Therefore, another plan examined the possibilities of replacing the T179 gun with the 105 mm M68 rifled anti-tank gun, a license-built version of the British L7 gun, which had, despite the smaller caliber, a performance comparable to the bigger 120 mm T179. But since the M48 chassis and its armor concept had become outdated by the time, too, the M77A1 fleet was by 1986 fully replaced by the M60A3, the US Army’s new standard MBT.

  

Specifications:

Crew: 4 (commander, driver, loader, gunner)

Weight: 51 tons

Length: 6.946 m (22 ft 9.5 in) hull only, 10,66 m (34 ft 11 in) overall w. gun forward

Width: 3.63 m (11 ft 11 in)

Height: 3.08 m (10 ft 1 in)

Suspension: Torsion-bar

Ground clearance: 1 ft 6.2 in (0.46 m)

Fuel capacity: 385 US gal (1,457 l)

 

Armor:

0.5 – 5.3 in (13 – 137 mm)

 

Performance:

Speed:

- Maximum, road: 30 mph (48 km/h)

- Sustained, road: 25 mph (40 km/h)

- Cross country: 9.3 to 15.5 mph (15 to 25 km/h)

Climbing capability:

- 40% side slope and 60% max grade

- Vertical obstacle of 36 inches (91 cm)

- 102 inches (2.59 m) trench crossing

Fording depth: Unprepared: 4 ft (1.219 m), prepared: 8 ft (2.438 m)

Operational range: 287 ml (463 km) on road

Power/weight: 16.6 hp (12.4 kW)/tonne

 

Engine:

1× Continental AVDS-1790-2 V12, air-cooled twin-turbo diesel engine, 750 bhp (560 kW)

 

Transmission:

General Motors CD-850-3, 2-Fw/1-Rv speed GB

 

Armament:

1× 120 mm T179 L/60 rifled anti-tank gun with an autoloader and a total of 29 rounds

1× co-axial 7.62 mm M240C machine gun with 3.000 rounds

1× .50 cal (12.7 mm) M2 Browning (600 rounds) or .30 cal (7.62 mm) M73 machine

anti-aircraft machine gun (1.000 rounds) on the commander’s cupola with 600 rounds

  

The kit and its assembly:

This is another fictional creation, but, like many of my whif builds, it is rooted in reality and an extrapolation of what could have been. The oscillating tower with the M103’s 120 mm cannon and an autoloader was actually developed, and there were several tank projects that made use of it. The T77 was the final proposal, but, like the T57 on the M103 basis and other designs from the Rheem Company, the T77’s development was arduously slow, so that the project was finally canceled in 1957 by the US Ordnance Department. Two turrets were actually built, though, but they were scrapped in February 1958, and the T77 only existed on paper or in model form.

 

The impulse for this build actually came from a 1:72 resin turret for the T57 project from ModelTrans/Silesian Models. I found the concept cool and the turret had a very futuristic look, so that I bought a set with the vague intention to use it for a mecha conversion someday. Then it gathered dust in the stash, until I recently stumbled upon the 1:72 M103 kit from Dragon and considered a T57 build. But this kit is very rare and expensive, at least here in Germany, so I shelved this plan again. However, I started to play with the idea of a U.S. Army vehicle with a Rheem Company turret. Then I found a Revell M60 kit in the stash and considered it for a whiffy build, but eventually rejected the idea because a turret concept from the late Fifties would hardly make its way onto a tank from the late Seventies or later. When I did further research concerning the Rheem turret, I came across the real T77 project on the basis of the M48, and dug out an ESCI M48A5 from the pile (realizing that I had already hoarded three of them…!), so the M77 project was finally born.

 

Otherwise, the build was a straightforward affair. The T57 turret is a massive resin piece with a separate barrel and very fine surface details. Some of them, delicate lugs, were unfortunately broken off, already OOB but also by me while handling the pieces. They could be easily replaced with brass wire, though, which was also used to add small rails to the collar. The very long and thin barrel was replaced with a white metal aftermarket piece. It’s actually a barrel for a Soviet T-10 with a complex muzzle brake (made from brass), but the size was just fine and looks very good on this fictional tank.

Some details were added to the turret or transplanted from the M48 kit, e. g. the prominent IR searchlight or the machine gun on the commander cupola. Furthermore, I added a textile seal to the gap between the turret sections and to the barrel’s root, made from paper tissue drenched in thinned white glue. The same method was used to create the searchlight cover, too.

 

Since the turret base had a smaller diameter than the M48’s attachment opening, I had to improvise a suitable adapter with styrene strips. The M48A5 hull itself was taken OOB.

  

Painting and markings:

I was happy that I could place this model into a later time frame, so that the U.S. Army’s uniform Olive Drab times were already over. In the 1970s, the US Mobility Equipment Research & Design Command (MERDC) developed a system of camouflage patterns for US Army vehicles. These consisted of a set of standardized patterns for each vehicle, to be used with a set of twelve colours. The local terrain conditions and colours decided which of the paints were to be used, and on which parts of a vehicle. Then, if conditions altered, for example by a change in the weather, or by the unit moving into a new area of operations, the scheme could be quickly adjusted to suit them by replacing only one or two colours by different ones.

For example, if a vehicle was painted in the US & European winter scheme, which had a dark green and a medium brown as its predominant colours, and it started to snow, by overpainting either the green or the brown with white, one of the two snow schemes could be created. This gave a high degree of flexibility, though in practice it was hardly ever actually made use of—most vehicles were painted in one scheme and kept that.

I gave the M77 the “Winter Verdant” MERDC scheme, which was frequently used in Germany. It consists of Forest Green (FS 34079), Earth Red (FS 30117), Sand (FS 30277) and Black (FS 37038). The pattern itself was adapted from the standardized M60 MERDC scheme. Colors used were ModelMaster 1701 and 1710, plus Humbrol 238 and Revell 06. The seals on the turret and the searchlight cover were painted in a faded olive drab, the track segments with a mix of iron, dark grey and red brown.

 

After basic painting with brushes, the kit received a washing with thinned black and red brown acrylic paint. Decals (taken from the ESCI kit) came next, then the model received an overall dry brushing treatment with Humbrol 72 (Khaki Drill) and 168 (Hemp). Finally, everything was sealed with matt acrylic varnish from the rattle can and the lower hull areas were dusted with mineral pigments, simulating dust and mud.

  

Another relatively simple conversion, since only the (oscillating) turret was swapped. However, I was skeptical at first because the turret was originally intended for an M103 hull - but mounting it on a smaller M48 chassis worked well, just like in real life!

Texaco ad from the early Fifties.

Beer has food value but food has no beer value

A short drive from Wootton is Swingfield, which lies near the Folkestone to Canterbury road, the A260. In fact beside that road is St John's, a preceptory, that I will endeavour to see inside of during the summer months.

 

In fact, I thought St John was the sole ecclesiastical building in the parish, but in fact there is a grand church in the centre of the village, opposite what used to the village pub.

 

The church has a grand tower with an even grander staircase turret running up one side, and in the porch I could see the 'church open' board, all packed away, It did not look good.

 

But it was open, but the first thing that struck me was the fine porch, apparently 14thC.

 

The church is a large two cell construction, with simple box pews in the nave, with wooden pews in the chancel.

 

It's walls are plain with few memorials, considering its history with the Knights of St John.

 

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

 

This church is built in flint and rubble construction and the west tower has a remarkably wide stair turret. As one enters through the south porch one can see the remains of two mass dials made redundant by the construction of the porch itself. By the pulpit is a most unusual feature - the south-east window of the nave has had its sill cut away to provide space for a wooden ladder to give access to the rood loft. This window now contains a lovely stained glass representation of the Crucifixion with a charming little sun and moon at the top. At Swingfield the nineteenth-century north aisle detracts from the thirteenth-century nave; its scale, materials and lumpy effect do nothing to complement this charming church. It is currently (2005) under threat of conversion to a house.

 

www.kentchurches.info/church.asp?p=Swingfield

 

SWINGFIELD is within the ECCLESIASTICAL JURISDICTION of the diocese of Canterbury, and deanry of Dover.

 

¶The church, which is dedicated to St. Peter, consists of one isle and one chancel, having a square tower, with a beacon turret at the west end, in which is one bell. In the chancel are several memorials for the Pilchers, tenants of St. John's. In the isle are memorials for the Simmons's, of Smersall; arms, parted per fess and pale, three trefoils slipt. One of them, John Simmons, gent. obt. 1677, was great-grandfather of James Simmons, esq. alderman of Canterbury; memorials for the Pilchers; against the north wall is a monument for Mary, widow of Richard Pilcher, gent. of Barham, obt. 1775; arms, Pilcher, argent, on a fess dancette, gules, a fleur de lis, between three torteauxes. In the south-west window is this legend, Ora p aiabs Willi Smersolle & Margarete uxon is sue & paia Saundir Goldfiynch; above were formerly these arms, A cross impaling on a bend, cotized, a mullet between six martlets. Weever says, p. 274, there was an antient faire monument, whereon the portraiture of an armed knight, crosse legged, was to be seen, and only His jacet remaining of the inscription, and that there was this legend in a window: Orate p aia Willi Tonge & Johannis filii ejus qui banc fenestram fieri fecerunt; he died in 1478, and was buried here. And there was formerly in the windows, a figure of a knight of St. John's, habited in his furcoat of arms, a plain cross, and having his sword and spurs, and kneeling on a cushion, in a praying posture, and in one of the windows were these arms, Quarterly, first and fourth, Azure, a square castle, sable; second and third, Or, on a chevron, vert, three bawks heads erased, argent; on a chief, gules, a cross, argent; but there is nothing of these remaining now.

 

The rectory of this church was early appropriated to the hospital of St. John, which continued in the possessions of all the profits of it, till the dissolution of the hospital in the 32d year of king Henry VIII. After which it was granted, with the preceptory here, to Sir Anthony Aucher, who sold it to Sir Henry Palmer, in whose descendants it continued down to Sir Thomas Palmer, bart. after whose death in 1725 it passed, in manner as before-mentioned, to the Rev. Dr. Thomas Hey, of Wickham, who sold it, with St. John's, and the rectory as before-mentioned, to Mr. Brydges, of Denton, the present owner of it.

 

This church is now a perpetual curacy, of the yearly certified value of twenty pounds, which stipend is paid by the owner of the rectory, who has the nomination of the curate. In 1640 here were communicants one hundred and twenty-seven.

 

www.british-history.ac.uk/survey-kent/vol8/pp120-126

U.S. Air Force Fact Sheet THUNDERBIRDS

 

Mission

Officially, the Thunderbirds are known as the U.S. Air Force Air Demonstration Squadron.

The squadron’s mission is to plan and present precision aerial maneuvers to exhibit the capabilities of modern, high-performance aircraft and the high degree of professional skill required to operate those aircraft.

Within this broad mission, the team has five primary objectives: − Support Air Force recruiting and retention programs − Reinforce public confidence in the Air Force and to demonstrate to the public the professional competence of Air Force members − Strengthen morale and esprit de corps among Air Force members − Support Air Force community relations and people-to-people programs − Represent the United States and its armed forces to foreign nations and project international goodwill

 

The Team

The Thunderbirds squadron is an Air Combat Command unit composed of eight pilots (including six demonstration pilots), four support officers, four civilians and more than 100 enlisted personnel performing in almost 30 job specialties.

 

A Thunderbirds air demonstration is a mix of formation flying and solo routines. The four-jet diamond formation demonstrates the training and precision of Air Force pilots, while the lead and opposing solo aircraft highlight some of the maximum capabilities of the F-16 Fighting Falcon.

The pilots perform approximately 40 maneuvers in a demonstration. The entire show, including the ground show and air demonstration, lasts about 75 minutes. The season typically starts in March and ends in November, with the winter months used to train new members.

 

Officers serve a two-year assignment with the squadron, while enlisted personnel serve three to four.

The squadron performs no more than 80 air demonstrations each year and has never canceled a demonstration due to maintenance difficulty. More than 280 million people in all 50 states and 57 foreign countries have seen the red, white and blue Thunderbirds jets in more than 3,500 aerial demonstrations.

In addition to their responsibilities as the Air Force’s premier jet demonstration team, the Thunderbirds are part of our combat force. If required, the team's personnel and aircraft can be rapidly integrated into a fighter unit at Nellis Air Force Base, Nev. Since the aircraft are only slightly modified, they can be made combat-ready in less than 72 hours.

 

F-16 Fighting Falcon

The Lockheed Martin F-16 Fighting Falcon represents the full range of capabilities possessed by the Air Force's tactical fighters. This highly-maneuverable multi-role fighter has proved to be one of the world's best precision tactical bombers and air-to-air combat aircraft. The only modifications needed to prepare aircraft for air demonstrations are a smoke-generating system and painting in Thunderbird colors. Additional information about the F-16 can be found at www.af.mil/AboutUs/FactSheets/Display/tabid/224/Article/1....

  

History

The Thunderbirds were officially activated June 1, 1953, as the 3600th Air Demonstration Unit at Luke AFB, Ariz. The unit was nicknamed the “Stardusters.” Their first aircraft was the straight-winged F-84G Thunderjet, a combat fighter-bomber that had seen action in Korea. Early in 1955, the team transitioned to the swept-winged F-84F Thunderstreak.

 

In June 1956, the team moved to its current home at Nellis. At the same time the Thunderbirds traded the veteran F-84 for the world's first supersonic fighter, the F-100 Super Sabre -- an aerial platform that would serve the Thunderbirds for 13 years. More than 1,000 demonstrations were flown in the Super Sabre, thrilling spectators around the world. In 1964, the team changed briefly to the F-105B Thunderchief, but an in-flight mishap revealed a problem with that airframe’s design. So, after only six shows, the Thunderbirds returned to the F-100.

From 1969 to 1973, the Thunderbirds flew the Air Force's front-line fighter, the F-4E Phantom II. In 1974, the Thunderbirds converted to the T-38 Talon, the world's first supersonic trainer. The T-38 was more fuel-efficient and less costly to maintain, which made it an ideal choice during the oil crisis of the 1970s.

Early in 1983, the Thunderbirds reinstituted their traditional role of demonstrating the Air Force's front-line fighter capabilities. Transition to the F-16A allowed the team to retain manpower and fuel efficiency while demonstrating to spectators the latest in fighter technology.

 

For additional information on our team, visit www.afthunderbirds.com.

Point of Contact

USAF Thunderbirds, Public Affairs Office; 4445 Tyndall Ave.; Nellis AFB, NV 89191-6079; DSN 682-6776 or (702) 652-6776; e-mail: USAF.Thunderbirds@nellis.af.mil

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 Northrop Grumman-IAI F-24 is the latest reincarnation of the USAF "Lightweight Fighter Program" which dates back to the 1950ies and started with the development of Northrop's F-5 "Freedom Fighter".

 

The 1st generation F-5 became very successful in the export market and saw a long line of development, including the much more powerful F-5E "Tiger II" and the F-20 Tigershark (initially called F-5G). Northrop had high hopes for the F-20 in the international market; however, policy changes following Ronald Reagan's election meant the F-20 had to compete for sales against aircraft like the F-16, the USAF's latest fighter design (which was politically favored). The F-20 development program was eventually abandoned in 1986 after three prototypes had been built and a fourth partially completed.

 

But this was not the end for Northrop’s Lightweight Fighter. In the early 1980s, two X-29As experimental aircraft were built by Grumman from two existing Northrop F-5A Freedom Fighter airframes. The Grumman X-29 was a testbed for forward-swept wings, canard control surfaces, and other novel aircraft technologies. The aerodynamic instability of this arrangement increased agility but required the use of computerized fly-by-wire control. Composite materials were used to control the aeroelastic divergent twisting experienced by forward-swept wings, also reducing the weight. The NASA test program continued from 1984 to 1991 and the X-29s flew 242 times, gathering valuable data and breaking ground for new aerodynamic technologies of 4th and 5th generation fighters.

 

Even though no service aircraft directly evolved from the X-29, its innovative FBW system as well as the new material technologies also opened the door for an updated F-20 far beyond the 1990ies. It became clear that ever expensive and complex aircraft could not be the answer to modern, asymmetrical warfare in remote corners of the world, with exploding development costs and just a limited number of aircraft in service that could not generate true economies of scale, esp. when their state-of-the-art design would not permit any export.

Anyway, a global market for simpler fighter aircraft was there, as 1st generation F-16s as well as the worldwide, aging F-5E fleet and types of Soviet/Russian origin like the MiG-29 provided the need for a modern, yet light and economical jet fighter. Contemporary types like the Indian HAL Tejas, the Swedish Saab Gripen, the French Dassault Rafale and the Pakistani/Chinese FC-1/JF-17 ”Thunder” proved this trend among 4th - 4.5th generation fighter aircraft.

 

Northrop Grumman (Northrop bought Grumman in 1994) initiated studies and basic design work on a respective New Lightweight Fighter (NLF) as a private venture in 1995. Work on the NLF started at a slow pace, as the company was busy with re-structuring.

The idea of an updated lightweight fighter was fueled by another source, too: Israel. In 1998 IAI started looking in the USA for a development partner for a new, light fighter that would replace its obsolete Kfir fleet and partly relieve its F-16 and F-15 fleet from interception tasks. The domestic project for that role, the IAI Lavi, had been stillborn, but lots of its avionics and research were still at hand and waited for an airframe for completion.

The new aircraft for the IAF was to be superior to the MiG-29, at least on par with the F-16C/D, but easier to maintain, smaller and overall cheaper. Since the performance profiles appeared to be similar to what Northrop Grumman was developing under the NLF label, the US company eventually teamed up with IAI in 2000 and both started the mutual project "Namer" (=נמר, “Tiger” in Hebrew), which eventually lead to the F-24 I for the IAF which kept its project name for service and to the USAF’s F-24A “Tigershark”.

 

The F-24, as the NLF, was based on the F-20 airframe, but outwardly showed only little family heritage, onle the forward fuselage around the cockpit reminds of the original F-5 design . Many aerodynamic details, e. g. the air intakes and air ducts, were taken over from the X-29, though, as the experimental aircraft and its components had been developed for extreme maneuvers and extra high agility. Nevertheless, the X-29's forward-swept wing was considered to be too exotic and fragile for a true service aircraft, but the F-24 was to feature an Active Aeroelastic Wing (AAW) system.

 

AAW Technology integrates wing aerodynamics, controls, and structure to harness and control wing aeroelastic twist at high speeds and dynamic pressures. By using multiple leading and trailing edge controls like "aerodynamic tabs", subtle amounts of aeroelastic twist can be controlled to provide large amounts of wing control power, while minimizing maneuver air loads at high wing strain conditions or aerodynamic drag at low wing strain conditions. This system was initially tested on the X-29 and later on the X-53 research aircraft, a modified F-18, until 2006.

 

Both USAF and IAF versions feature this state-of-the-art aerodynamic technology, but it is uncertain if other customers will receive it. While details concerning the F-24's system have not been published yet, it is assumed that its AAW is so effective that canard foreplanes could be omitted without sacrificing lift and maneuverability, and that drag is effectively minimized as the wing profile can be adjusted according to the aircraft’s speed, altitude, payload and mission – much like a VG wing, but without its clumsy and heavy swiveling mechanism which has to bear high g forces. As a result, the F-24 is, compared to the F-20, which could carry an external payload of about 3.5 tons, rumored to be able to carry up to 5 tons of ordnance.

 

The delta wing shape proved to be a perfect choice for the required surface and flap actuators inside of the wings, and it would also offer a very good compromise between lift and drag for a wide range of performance. Anyway, there was one price to pay: in order to keep the wing profile thin and simple, the F-24’s landing gear retracts into the lower fuselage, leaving the aircraft with a relatively narrow track.

 

Another major design factor for the outstanding performance of this rather small aircraft was weight reduction and structural integrity – combined with simplicity, ruggedness and a modular construction which would allow later upgrades. Instead of “going big” and expensive, the new F-24 was to create its performance through dedicated loss of weight, which was in some part also a compensation for the AAW system in the wings and its periphery.

 

Weight was saved wherever possible, e .g. a newly developed, lightweight M199A1 gatling gun. This 20mm cannon is a three-barreled, heavily modified version of the already “stripped” M61A2 gun in the USAF’s current F-18E and F-22. One of the novel features is a pneumatic drive instead of the traditional electric mechanism, what not only saves weight but also improves trigger response. The new gun weighs only a mere 65kg (the six-barreled M61A2 weighs 92kg, the original M61A1 112 kg), but still reaches a burst rate of fire of 1.800 RPM (about 800 RPM under cyclic fire, standard practice is to fire the cannon in 30 to 50-round bursts, though) and a muzzle velocity of 1.050 metres per second (3,450 ft/s) with a PGU-28/B round.

 

While the F-16 was and is still made from 80% aluminum alloys and only from 3% composites, the F-24 makes major use of carbon fiber and other lightweight materials, which make up about 40% of the aircraft’s structure, plus an increased share of Titanium and Magnesium alloys. As a consequence and through many other weight-saving measures like keeping stealth capabilities to a minimum (even though RAM was deliberately used and many details designed to have a natural low radar signature, resulting in modest radar cross-section (RCS) reductions), a single, relatively small engine, a fuel-efficient F404-GE-402 turbofan, is enough to make the F-24 a fast and very agile aircraft, coupled with a good range. The F-24’s thrust/weight ratio is considerably higher than 1, and later versions with a vectored thrust nozzle (see below) will take this level of agility even further – with the pilot becoming the limiting factor for the aircraft’s performance.

 

USAF and IAF F-24s are outfitted with Northrop Grumman's AN/APG-80 Active Electronically Scanned Array (AESA) radar, also used in the F-16 Block 60 aircraft. Other customers might only receive the AN/APG-68, making the F-24 comparable to the F-16C/D.

 

The first prototype, the YF-24, flew on 8th of March 2008, followed by two more aircraft plus a static airframe until summer 2010. In early 2011 the USAF placed an initial order of 101 aircraft (probably also to stir export sales – the earlier lightweight fighters from Northrop suffered from the fact that the manufacturer’s country would not use the aircraft in its own forces). These initial aircraft will replace older F-16 in the interceptor role, or free them for fighter bomber tasks. The USN and USMC also showed interest in the aircraft for their aggressor squadrons, for dissimilar air combat training. A two-seater, called the F-24B, is supposed to follow soon, too, and a later version for 2020 onwards, tentatively designated F-24C, is to feature an even stronger F404 engine and a 3D vectoring nozzle.

 

Israel is going to produce its own version domestically from late 2014 on, which will exclusively be used by the IAF. These aircraft will be outfitted with different avionics, built by Elta in Israel, and cater to national requirements which focus more on multi-purpose service, while the USAF focusses with its F-24A on aerial combat and interception tasks.

 

International interest for the F-24A is already there: in late 2013 Grumman stated that initial talks have been made with various countries, and potential export candidates from 2015 on are Taiwan, Singapore, Thailand, Finland, Norway, Australia and Japan.

  

General F-24A characteristics:

Crew: 1 pilot

Length: 47 ft 4 in (14.4 m)

Wingspan: 27 ft 11.9 in / 8.53 m; with wingtip missiles (26 ft 8 in/ 8.13 m; without wingtip missiles)

Height: 13 ft 10 in (4.20 m)

Wing area: 36.55 m² (392 ft²)

Empty weight: 13.150 lb (5.090 kg)

Loaded weight: 15.480 lb (6.830 kg)

Max. take-off weight: 27.530 lb (12.500 kg)

 

Powerplant

1× General Electric F404-GE-402 turbofan with a dry thrust of 11,000 lbf (48.9 kN) and 17,750 lbf (79.2 kN) with afterburner

 

Performance

Maximum speed: Mach 2

Combat radius: 300 nmi (345 mi, 556 km); for hi-lo-hi mission with 2 × 330 US gal (1,250 L) drop tanks

Ferry range: 1,490 nmi (1715 mi, 2759 km); with 3 × 330 US gal (1,250 L) drop tanks

Service ceiling: 55,000 ft (16,800 m)

Rate of climb: 52,800 ft/min (255 m/s)

Wing loading: 70.0 lb/ft² (342 kg/m²)

Thrust/weight: 1.09 (1.35 with loaded weight & 50% fuel)

 

Armament

1× 20 mm (0.787 in) M199A1 3-barreled Gatling cannon in the lower fuselage with 400 RPG

Eleven external hardpoints (two wingtip tails, six underwing hardpoints, three underfuselage hardpoints) and a total capacity of 11.000 lb (4.994 kg) of missiles (incl. AIM 9 Sidewinder and AIM 120 AMRAAM), bombs, rockets, ECM pods and drop tanks for extended range.

  

The kit and its assembly:

A spontaneous project. This major kitbash was inspired by fellow user nighthunter at whatifmodelers.com, who came up with a profile of a mashed-up US fighter, created “out of boredom”. The original idea was called F-21C, and it was to be a domestic successor to the IAI Kfirs which had been used by the US as aggressor aircraft in USN and USMC service for a few years.

 

As a weird(?) coincidence I had many of the necessary ingredients for this fictional aircraft in store, even though some parts and details were later changed. This model here is an interpretation of the original design. The idea was spun further, and the available parts that finally went into the model also had some influence on design and background.

I thank nighthunter for sharing the early ideas, inviting me to take the design to the hardware stage (sort of…) and adapting my feedback into new design sketches, too, which, in return, inspired the model building process.

 

Well, what went into this thing? To cook up a F-24 à la Dizzyfugu you just need (all in 1:72):

● Fuselage from a Hasegawa X-29, including the cockpit and the landing gear

● Fin and nose cone from an Italeri F-16A

● Inner wings from a (vintage) Hasegawa MiG-21F

● Outer wings from a F-4 (probably a J, Hasegawa or Fujimi)

 

The wing construction deviates from nighthunter’s original idea. The favorite ingredients would have been F-16XL or simple Mirage III wings, but I found the composite wing to be more attractive and “different”. The big F-16XL wings, despite their benefit of a unique shape, might also have created scale/size problems with a F-20 style fuselage? So I built hybrid wings: The MiG-21 landing gear wells were filled with putty and the F-4 outer wings simply glued onto the MiG inner wing sections, which were simply cut down in span. It sounds like an unlikely combo, but these parts fit together almost perfectly! In order to hide the F-4 origins I modified them to carry wingtip launch rails, though, which were also part of nighthunter’s original design.

 

The AAW technology detail mentioned in the background came in handy as it explains the complicated wing shape and the fact that the landing gear retracts into the fuselage, not into the wings, which would have been more plausible… Anyway, there’s still room for a simpler export version, with Mirage III or Kfir C.2/7 wings, and maybe canards?

 

Using the X-29 as basis also made fitting the new wings onto the area-ruled fuselage pretty easy, as I could use the wing root parts from the X-29 to bridge the gap. The original, forward-swept wings were just cut away, and the remains used as consoles for the new hybrid delta wings. Took some SERIOUS putty work, but the result is IMHO fine.

 

The bigger/square X-29 air intakes were taken over, and they change the look of the aircraft, making it look less F-5-ish than a true F-20 fuselage. For the same reason I kept the large fairing at the fin base, combining it with a bigger F-16 tail, though, as a counter-balance to the new, bigger wings. Again, the F-16 fin was/is part of nighthunter’s idea, so the model stays true to the original concept.

 

For the same reason I omitted the original X-29 nose, which is rather pointy, sports vanes and a large sensor boom. The F-16 nose was a plausible choice, as the AN/APG-80 is also carried by late Fighting Falcons, and its shape fits well, too.

 

All around the hull, some small details like radar warning sensors, pitots and air scoops were added. Not really necessary, but such thing add IMHO to the overall impression of such a fictional aircraft beyond the prototype stage.

 

Cockpit and landing gear were taken OOB, I just added a pilot figure and slightly modified the seat.

 

The ordnance was puzzled together from the scrap box, the AIM-9Ls come from the same F-4 kit which donated its outer wings, the AIM-120s come from an Italeri NATO weapons kit. The drop tanks belong to an F-16.

  

Painting and markings:

At first I considered an F-24I in IAF markings, or even a Japanese aircraft, but then reverted to one of nighthunter’s initial, simple ideas: an USAF aircraft in the “Hill II” paint scheme (F-16 style), made up from three shades of gray (FS 36118, 36270 and 36375) with low-viz markings and stencils. Dutch/Turkish NF-5A/Bs in the “Hill II” scheme were used as design benchmarks, too. It’s a simple livery, but on this delta wing aircraft it looks pretty interesting. I used enamels, what I had at hand: Humbrol 127 and 126, and Modelmaster's 1723.

 

A light black ink wash was applied, in order to em,phasize the engraved panel lines, in contrast to that, panels were manually highlighted through dry-brushed, lighter shades of gray (Humbrol 27, 166 and 167).

 

“Hill II” also adds to a generic, realistic touch for this whif. Doing an exotic air force thing is rather easy, but creating a convincing whif for a huge military machinery like the USAF’s takes more subtlety, I think.

 

The cockpit was painted in medium Gray (Dark Gull Grey, FS 36231, Humbrol 140), as well as the radome. The landing gear and the air intakes were painted white. The radome was painted with Revell 47 and dry-brushed with Humbrol 140.

 

Decals were puzzled together from various USAF aircraft, including sheets from an Airfix F-117, an Italeri F-15E and even an Academy OV-10D.

  

Tadah: a hardware tribute to an idea, born from boredom - and the aircraft does not look even bad at all? What I wanted to achieve was to make the F-24 neither look like a F-20, nor a Saab Gripen clone, as the latter comes close in overall shape, size and design.

Series of 4 Posters on Food Facts.

one: i am american (born in cincinnati, ohio), but my ancestors hailed from poland, lithuania, and italy. they all came through ellis island at the turn of the 20th century. this explains my haphazard collection of features, no? :P

 

two: i grew up catholic. i'm now an atheist. ditto for the husband. funny how that happens...

 

three: i'd prefer to live in large cities. i'm allergic to suburbs. :P i did most of my growing up in the suburbs of orlando, florida, thus (i think!) partially explaining this preference and abhorrence.

 

four: i am naturally blonde. it's this really gross dishwater blonde, so i've been dying it some other "better" color since about 14. right now i am on a red kick. i have also sported various shades of blonde, pink, purple and orange, sometimes more than one of such at once.

 

five: i think my daughter is one of the best things i've ever created. i had an ectopic pregnancy in 2002, and i was convinced i'd never have children. having her, and feeding her from my own body has convinced me that a.) my body is capable of doing (very) good things and b.) has given me new purpose in life. i am so blessed to be here, to be alive and healthy, to have the chance to see her grow. she is the light of my life.

 

six: my current favorite color is orange. i really like ALL colors, though. but only really in their most saturated, vivid versions. i don't really like shades or pastels nearly as much.

 

seven: my favorite kind of cake is carrot cake, my favorite jelly belly flavor is juicy pear, and i like my chocolate dark, dark, dark. i like my whiskey single malt, and my beer belgian.

 

eight: if i wasn't so focused on the arts and design, i might consider a career in medicine. my friend jessica (who's studying nursing) told me i have a medical mind. i argue that i just have a scientific mind, mostly because i just enjoy the act of thinking critically and have a rather annoying penchant for asking too many questions about just about everything. for fun, i read non-fiction books about health and medicine.

 

nine: i am very interested in linguistics but speak no other language but english. i have a hard time choosing which one to learn! hopefully it's not too late!

 

ten: i have been on a mission to bring back clip-on earrings and acid wash since 2005. i feel i have been rather successful at the latter, much to my delight.

 

eleven: i prefer to write in lowercase, if i can help it. i have been doing so, as a rule, since 1997.

 

twelve: i have two degrees, after about 6+ years of schooling. i majored in history and art history as an undergrad, and got another degree in fashion. i graduated summa cum laude from both schools (highest honors).

 

thirteen: i'm actually rather shy and more than a little neurotic. i can also be very moody. i'm more introverted than extroverted. when i do talk, i'm usually pretty straightforward and honest, to a fault.

 

fourteen: my husband is my best friend. we met at a rave in orlando on new years eve 1996, turning 1997. i trust him more than anyone else on the face of the planet.

 

fifteen: i really don't like wearing socks. but have to, of course. as a result, most of my socks are fairly cringeworthy to look at. thankfully they are mostly hidden by my boots, which are my favorite type of footwear. also, my husband would like me to mention that i don't like wearing belts for function...only fashion. i.e., i'd rather let my pants fall down than wear a belt through the loops. yup, i'm quirky.

 

sixteen: i'm moving back to new york city..., very, VERY soon. :) goodbye san francisco!

F.A.C.T.S. 2017 ||

Gent, Belgien ||

 

Day 01 - 21.10.2017 ||

 

FACTS is the largest Comic Con show in the Benelux. Each year more than 40,000 visitors gather at FACTS for two days to switch from the real world to the one of Fantasy, Comics, Action Heroes, Games, Anime and Toys. ||

FACTS is for the European fantasy fans what King's Landing is for Westeros. ||

 

My Bog-Post : ||

mchenryarts.wordpress.com/2017/11/05/f-a-c-t-s-2017/ ||

 

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www.flickr.com/photos/mchenryarts ||

www.facebook.com/McHenryArts ||

 

People who are the main subject of the photo can use this for your personal use, for example, the use on Facebook, etc. The only requirement is a link to my Facebook or Flickr Page. ||

 

Nutzungsvereinbarung / Terms of Use :

mchenryarts.wordpress.com/tou/

+++ 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 Supermarine Spitfire is a British single-seat fighter aircraft that was used by the Royal Air Force and many other Allied countries during and after the Second World War. The Spitfire was built in many variants, using several wing configurations, and was produced in greater numbers than any other British aircraft.

 

The Spitfire was designed as a short-range, high-performance interceptor aircraft by R. J. Mitchell, chief designer at Supermarine Aviation Works (which operated as a subsidiary of Vickers-Armstrong from 1928). In accordance with its role as an interceptor, Mitchell designed the Spitfire's distinctive elliptical wing to have the thinnest possible cross-section; this thin wing enabled the Spitfire to have a higher top speed than several contemporary fighters, including the Hawker Hurricane.

 

It was the only British fighter to be in continuous production throughout World War II, and remained in service with several air forces around the world for several years. One of its post-war operators was the Lebanese Air Force, or Al Quwwat al-Jawwiya al-Lubnaniyya (لقوات الجوية اللبنانية‎).

The Lebanese Air Force was established in 1949 under the command of then-Lieutenant Colonel Emile Boustany who later became commander of the army. Soon after its establishment, a number of planes were donated by the British, French, and Italian governments, with additional planes donated by Britain and Italy later that same year.

 

Britain donated 4 Percival Prentices, 2 World War II-era Percival Proctors and seven trpocailized Supermarine Spitfires (six Mk. XVIe and one TR.8 two-seater), while Italy donated 4 Savoia-Marchetti SM.79 bombers which were mainly used for transportation.

 

The Mk XVI Spitfire was a WWII design, and the last variant powered by a Merlin engine and based on the original, sleek fuselage. It was basically the same as the Mk IX, except for the engine, a Merlin 266. The Merlin 266 was the Merlin 66 and was built under licence in the USA by the Packard Motor Company. The "2" was added as a prefix in order to avoid confusion with the engines, as they required different tooling.

 

All Mk XVI aircraft produced (a total of 1,054 Mk XVIs left Castle Bromwich) were of the Low-Altitude Fighter (LF) variety. This was not determined by the length of the wings (clipped wings were fitted to most LF Spitfires), but by the engine, which had been optimised for low-altitude operation. All production Mk XVIs had clipped wings for low altitude work and were fitted with the rear fuselage fuel tanks with a combined capacity of 75 gal. Many XVIs featured cut-down rear fuselages with bubble canopies. On these aircraft the rear fuselage tank capacity was limited to 66 gal.

 

Because of a slightly taller intercooler and rearranged accessories on the Packard Merlins a new, bulged upper cowling was introduced, a detail that also appeared on late production IXs. For the service in the Middel East region the Lebanese machines received dust filters which considerably changed the aircraft's silhouette.

 

Armament consisted of two 20 mm Hispano II cannons - each with 120 rpg - and two 0.50 calibre Browning machine guns - each with 250 rpg. 1 × 500 lb (227 kg) bomb could be carried underneath the centre rack, and 1 × 250 lb (114 kg) bomb could be slung under each wing. As a special feature, the wing hardpoints of the Lebanese Spitfires were "wet" so that slipper tanks with 24 gal. each could be carried, compensating for the reduces rear fuselage tank due to the bubble canopy's lowered dorsal spine.

 

The Lebanese Spitfires only saw a short service, since in 1953, jet fighters were introduced when 16 de Havilland Vampire jets were received, and the first Hawker Hunters arrived in 1959, which replaced the obsolete Spitfires. This initial Hunter batch was followed by more Hunters through 1977.

 

In 1968, 12 Mirage IIIELs were delivered from France but were grounded in the late 1970s due to lack of funds. In 2000, the grounded Mirages were sold to Pakistan, and four Hunters were even revived in 2008 and served until 2014.

  

General characteristics:

Crew: one pilot

Length: 29 ft 11 in (9.12 m)

Wingspan: 36 ft 10 in (11.23 m)

Height: 11 ft 5 in (3.86 m)

Wing area: 242.1 ft2 (22.48 m2)

Airfoil: NACA 2209.4(tip)

Empty weight: 5,065 lb (2,297 kg)

Loaded weight: 6,622 lb (3,000 kg)

Max. takeoff weight: 6,700 lb (3,039 kg)

 

Powerplant:

1× Rolls-Royce Merlin 60 supercharged V12 engine,

rated at 1.470 hp (1.096 kW) at 9.250 ft (2.820 m)

 

Performance:

Maximum speed: 370 mph, (322 kn, 595 km/h)

Combat radius: 410 nmi (470 mi, 760 km)

Ferry range: 991 nmi (1,135 mi, 1,827 km)

Service ceiling: 36,500 ft (11,125 m)

Rate of climb: 2,600 ft/min (13.2 m/s)

Wing loading: 27.35 lb/ft2 (133.5 kg/m²)

Power/mass: 0.22 hp/lb (0.36 kW/kg)

 

Armament:

2x 20mm Hispano Mk II cannon (120 RPG)

2x .5 in Browning machine guns (250 RPG)

Three hardpoints (1 ventral, 1 under each outer wing) for up to 1.000 lb (454 kg).

  

The kit and its assembly:

This whif is based on a simple idea: how did Lebanon's Air Force start? Small countries make a good whif playground, and I guess that nobody has the Lebanon on his/her list...?

Another factor was that I had some Austrian roundels left in store that could, with a green dot, easily be turned into Lebanese markings. So the theme was quickly settled, but the details take some preparation time, so the idea lingered for some time.

 

After some legwork I deemed a simple Spitfire with a dust filter worthy as an initial aircraft, and the respective Hobby Boss kit of a Spitfire Mk. VB in the stash came handy.

But somehow this was a bit dull, and at the inception of the Lebanon Air Force there were better option available than an early Mk. V. I still wanted a sleek, Merlin-powered Spitfire variant, though, and eventually settled for the Mk. XVI - with its clipped wings and the bubble canopy it has a very distinctive look.

 

When a "1 Week group Build" at whatifmodelers.com in the Easter Week 2015 was announced, I took this occassion to build the Lebanese Spitfire.

 

By that time I already had a basis kit at hand (Heller's Spitfire XVI) as well as some donation parts and decals.

Work was strightforward, the Heller kit was built almost OOB. It's a rather old model kit, with raised panel lines, but good detail. The material is thin, so the built item lacks some structural stability! On the other side, this makes some minor mods really easy: I lowered the flaps and moved the tail rudders slightly off of neutral position. I also opened the cockpit "door" on the left side for later static display, even though the cockpit itself was left OOB. It's a bit "flat", but for the kit's age it's pretty good, and the injected canopy is crystal clear and fits perfectly.

 

I had some major woes concerning the fit for the forward fuselage, and even more when I tried to mate wings and fuselage: there was a 1mm gap(!) on both sides that had to be bridged with putty, and the thin and flexible material did help much...

 

Other mods concern the propeller (added a styrene tube and a metal axis for free spin), the radiators (these are molded into the lower wings - sounds horrible, but is made very well and thin, I just added some foamed styrene inside as protective mesh because OOB there's just a blank "box" inside) and the kit received a dust filter - a resin piece taken from a Pavla conversion set for Hawker Hurricanes.

  

Painting and markings:

While a donated RAF Spitfire would certainly have carried a desert paint scheme in Dark Earth/Mid Stone/Azure Blue or a late WWII Dark Green/Ocean Grey/Light Sea Grey livery I settled for something more individual and effective for the rugged Levantine terrain.

In this case I went for the rarely used RAF 'Tropical Scheme' in Mid Stone/Dark Green from above and with Mediterrenean Blue undersides.

 

The pattern itself is standard RAF, the upper cammo taken down onto the dust filter's flanks was taken over from RAAF Spitfires during WWII (RAF aircraft would carry a higher waterline, with the filter painted completely in the lower surface's tone). Basic paints are RAF Dark Green from Modelmaster and Humbrol 84 (RAF Mid Stone) - rather authentic. But I used Humbrol 87 (Steel Grey) for the undersides - it's rather intense and has a greenish hue, and by far not as dark as the typical RAF Azure Blue or PRU Blue.

 

Interior surfaces were painted in RAF Cockpit Green (Modelmaster Authentic), while the landing gear and its wells were kept in Aluminum Dope (Humbrol 56).

 

Decals/markings were puzzled together and improvised. The Lebanese roundels are actually Austrian national markings into which a dark green dot has ben added manually... the fin flash and the roman/arabic codes come from an Xtradecal aftermarket sheet.

 

Beyond these basic markings I did not add anything flashy - in 1951 things were rather simple,

The kit received a light shading and some dry painting with light grey, plus a light black ink wash. Soot/exhaust stains were created with grinded graphite and around the engine some leaked oil was added with Tamiya's "Smoke", and everything was sealed under a coat of matt acrylic varnish.

  

I'll admit it's not a spectacular whif, and overall rather simple concerning build and painting. But a proud addition to whatifmodelers.com's "! Week Group Build", even though this was already finished in just three days from sprues to beauty pics...

 

THE CLIMATE CHANGE SCAM.

 

The facts:

CO2 is a trace gas, it makes up only 0.04% of the atmosphere.

Expressed as a fraction, that is: four hundredths of one percent!

 

Only 3% of the total CO2 in the atmosphere is due to human activity

That is: three percent of four hundredths of one percent of CO2 in the atmosphere is likely to be caused by humans!

 

97% of the total CO2 in the atmosphere is from from natural sources

 

The UK only produced slightly over 1.% (1.02%) of the world's 3% total of CO2 caused by human activity!

That is: the UK produced around one hundredth

of the three percent total CO2 caused by humans!

The UK’s CO2 emissions have fallen by around 42% since 1990

 

CO2 is highly beneficial and crucial for life and plant growth.

An increase of CO2 would improve plant growth and reforestation.

 

The UK produces slightly over one hundredth of the human caused total of 3 percent (three hundredths) of the total four hundredths of one percent of CO2 in the atmosphere.

If you think that is a tiny, insignificant amount, you are perfectly correct.

 

All life is based on carbon, it is an essential food for plants. Plants obtain carbon from CO2 (Carbon Dioxide).

They separate the carbon from the oxygen which they release into the atmosphere.

The oxygen they release is also essential for life.

The idea that CO2 is a poison, or something undesirable, is preposterous nonsense. it is not based on good science, but politics, ideology and vested interests.

The amount of carbon dioxide in the atmosphere is very small compared to other gases, such as nitrogen, but it is essential.

 

The amount that humans contribute to the total CO2 is negligible. The vastly overwhelming amount - 97% is produced naturally. The idea that the other 3 percent, caused by humans, will destroy the planet is ridiculous.

 

Records going back centuries show that natural temperature rises are followed a rise in CO2, not the other way round. As the sea gets warmer it releases more CO2, a purely natural process. The most likely cause of the increase in temperature is activity on the Sun. The records show that it is an increase in temperature that causes an increase in CO2. This is not necessarily bad. A generally warmer climate caused by the Sun, with the resulting increase in CO2 is ideal for plant growth and a greener planet.

 

So, is CO2 a cause of global warming or climate change? Extremely unlikely!

You may ask; what about the scientific consensus, the claim that 97% of scientists agree that CO2 is a cause of climate change?

 

a) If something is repeated often enough, many people end up believing it. That’s how propaganda works.

 

b) Most scientists are not climate scientists, they work in other fields. They tend to respect the findings/opinions of other scientists, because they trust the scientific integrity of their peers, above any vested interests.

 

c) A consensus in science is not proof of anything. Scientific truth is not a democratic decision, it is not decided by a consensus, however large. That is a political concept, not a scientific one.

In science, empirical evidence is king.

The idea that a consensus opinion makes something beyond doubt, or unable to be challenged is an anathema to genuine scientific endeavour.

Science doesn’t work like that.

To impose a straightjacket on science is a fanatical position, which has the hallmark of ideological fanaticism. It is anti-science and a deplorable situation.

 

The common, political currency seems to be that anyone who dares to challenge the present, climate change opinion is a science denier, a term of abuse which is intended to imply they are wilfully ignorant, evil or even criminal.

That is an appalling situation. And very damaging for freedom of expression and the future of science. Scientific practice is a search for truth, not an ideology, or a political football. No genuine scientist, who has any integrity, can ever support such a situation. Any scientist who claims that manmade climate change is an irrefutable fact, or that issue is settled and the debate is over, is a disgrace to science.

There is no such thing as a ‘climate change denier’. It is a meaningless insult, invented by fanatical ideologues. All honest scientists would agree that any scientific opinion or hypothesis is only as good as the latest bit of evidence.

 

Inconvenient facts, the science that Al Gore doesn't want you to know:

binged.it/2WJoiRX

 

Piers Corbyn (brother of Jeremy Corbyn) - manmade climate change does not exist.

youtu.be/UvHMhZ1T964

 

Patrick Moore (one of the founders of Greenpeace) A dearth of carbon?

Dr. Moore says we were literally running out of carbon before we started to pump it back into the atmosphere, “CO2 has been declining to where it is getting close to the end of plant life, and in another 1.8 million years, life would begin to die on planet Earth for lack of CO2.”

 

According to Moore it is life itself that has been consuming carbon and storing it in carbonaceous rocks. He goes on to say, “billions of tons of carbonaceous rock represent carbon dioxide pulled out of the atmosphere, and because the Earth has cooled over the millennia, nature is no longer putting CO2 into the atmosphere to offset this.”

youtu.be/sXxktLAsBPo

  

Princeton physics professor William Happer explains why he describes some climate change scientists as a ‘cult.’

youtu.be/vro-yn59uso

 

Who trusts the MSM?

Their lies are not just fake news, they deliberately set out to slander those who don’t agree with the liberal left, globalist elite. Their lies are positively evil. Everyone should watch this video and they will never trust the media again: banned.video/watch?id=5f00ca7c672706002f4026a9

  

New NASA satellite data prove carbon dioxide is GREENING the Earth and restoring forests.

www.afinalwarning.com/500086.html?fbclid=IwAR2SoywjkPYu8-...

 

The latest Vegetation Index data from NASA shows that the Earth is getting progressively "greener" and lusher over time. The planet is 10 percent greener today than it was in 2000, NASA says, which means better conditions for growing crops. Forests are also expanding while deserts are becoming more fertile and usable for agriculture. All in all, the global Vegetation Index rose from 0.0936 to 0.1029 between 2000 and 2021, a 9.94 percent increase. "10 percent greening in 20 years! We are incredibly fortunate!" announced Zoe Phin, a researcher who compiled the data into a chart for her blog. "I just wish everyone felt that way. But you know not everyone does. To the extent that humans enhance global greening is precisely what social parasites want to tax and regulate. No good deed goes unpunished." A separate German study found that the globe has been greening for at least the past three decades. Satellite imagery suggests that vegetation has been expanding at a growing rate, contracting the gloom-and-doom narrative being spread by the climate alarmists.

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