pathology_doc said:Gridlock, would you be the sort of lunatic who'd also back the secret export of an Avro Arrow to the UK before the hammer came down, in such a manner that it's still hidden away somewhere? Having one surface in the UK and wind up parked next to the TSR.2 would be the ultimate monument to cancelled projects.
DamienB said:John Farley is a chap I have a great deal of respect for and has mentioned the TSR2's lack of wing area in a few discussions on the type; however the flaws he mentions (long take-off distance, long landing distance, lack of manouevrability) aren't the criticisms I'd make of the final design. The revised (relaxed) spec still had STOL capability of sorts - getting it in and out of a 1,000 meter poor quality runway with a useful war load wasn't to be sniffed at (if BAC coudl have managed it - as their own predictions were nearer 1200m). Manouevring to avoid missiles - well, the idea was never to get shot at, not to be doing fancy flying if you were. Look-down/shoot-down radars in fighters came much, much later and no fighter of the time would have been able to keep up with a fleeing TSR2 at low level in turbulence.
Loren said:It is not in Texas - I saw it in Nevada the last time I went to Groom Lake - with the flying saucers.
DamienB said:Oh dear, oh dear... Aeroplane Monthly's February 2012 has the TSR2 as the subject of one of their 'Database' articles.
Unfortunately, the article is littered with errors (and spelling mistakes):
Apparently the TSR2 was powered by the Olympus 302 (!); Freddie Page was appointed project leader by the government rather than BAC themselves; TSR designation is noted as being made in 1960 rather than 1959 wrongly explains the '2'; claims Vickers wanted to use Brooklands for first flight (never on the cards - Wisley was their choice) and perpetuates a wholly inaccurate account of the arguments about first flight location; reheat system was 'complex' (by far the simplest part of the engine); ejector seats capable up to mach 2 (not even close!); terrain following radar was apparently Blue Parrot (that's the Buccaneer radar, not a TFR); what on earth is the lateral oblique radar?; the C in ECM apparently now means 'communications' rather than 'counter'; pic on p80 miscaptioned as being flight 5 is flight 7; pic at top of p82 miscaptioned as pre-flight attention (but she's tied down!); "all engine problems cured" in January 1965 (not so!); flight 7 saw successful undercarriage retraction (no it didn't, it went wrong - flight 10 was the first successful retraction); one landing was on foam (actually four did); flight 16 had 'several' rolls (pretty sure it was just one, which was foolhardy enough on its own); undercarriage tie struts 'eliminated' vibration problems (not entirely); TSR2 was cancelled 'without prior warning or consultation' (what, apart from the three months worth of consultations and discussions with BAC about getting the price down?). There's more but I've had enough...
It finally dissolves into this: "Documents which may, or may not, give the exact reasons for the cancellation are still hidden away in the archives, and remain untouched because of heavy-handed embargoes." Said documents are available quite freely in various archives and spell out the reasons over and over again. Cost.
Sadly the whole article perpetuates the 'wonder jet' myth, inflating capabilities, ignoring items that were cancelled during development, and brings nothing new to the table at all. A real wasted opportunity and very odd considering the new reference material available in print from myself and others in the last year or so.
sealordlawrence said:I have never seen these numbers anywhere else and i was curious as to whether you had come across them during the course of your obviously extensive research. Also, whilst you lay out the planned distribution of aircraft between bases in your book I interested as to how many squadrons the 158 would have become?
sealordlawrence said:DamienB,
To try and get this thread back to its original subject I was wondering if you could comment on a couple of numbers that I have seen for considered/suggested/planned TSR-2 procurement:
320: In BSP Jet Bombers Tony Buttler states that: 'there were suggestions for 320'
200: Saki Dockrill states in 'Britain's retreat from east of Suez' that: 'The initial number requested by the RAF in 1959 had been 200 which the Conservative Government had reduced to 158'
I have never seen these numbers anywhere else and i was curious as to whether you had come across them during the course of your obviously extensive research. Also, whilst you lay out the planned distribution of aircraft between bases in your book I interested as to how many squadrons the 158 would have become?
How on earth could someone get their hands on an olympus engine and expect to sell it online. I think it should be in a museum.BAC TSR2 Olympus 320 Jet Engine
-This is engine number ONE !
-This example is the only privately owned Olympus 320 engine in the world. Other later examples are preserved in large accredited / registered charity museums in the UK but they are unlikely to ever go on sale.
-There are no known TSR2 Olympus 320 engines outside the UK.
This engine was found tucked away on a farm in Southern England and is quite possibly the aviation Barn Find of the decade. It was originally bought for scrap but it’s owner had the foresight to keep and preserve it for generations to come. The engine has just undergone an 18 month restoration and is now ready to display as the ultimate museum exhibit Jet Engine.
J.A.W. said:Surely - if the TSR-2 was that good, there would be a close Soviet analogue/clone built too?
Along the lines of the MiG 25 amalgam of NAA XF-108/RA -5 ideas?
donaldson1 said:It carried four on-board digital computers to process radar information.
Bruno Anthony said:A good documentary shat all over itself with the weakly supported argument that the USA(those evil Americans again) knee capped the TSR-2 to protect its F-111.
Hot Breath said:Excuse me, my understanding was that it carried analogue computers. These must have been remarkably primitive digital ones, considering the design and construction period.
JFC Fuller said:Hot Breath said:Excuse me, my understanding was that it carried analogue computers. These must have been remarkably primitive digital ones, considering the design and construction period.
The nav-attack system used the NAA Autonetics VERDAN computer which I understand to have been digital. It was actually a major cause of the programmes problems, the computer not really being up to what the RAF requirements needed it to do.
GEC and the RAE had been working on digital computer technology since the mid-late 1950s.
donaldson1 said:Despite this, unique film material did escape destruction and has remained hidden in vaults - until now.
http://youtu.be/o53u0X0Ik0w
J.A.W. said:Curiously too, the BAC brochure produced for the TSR 2 - also has a decidedly G & S Anderson look..
F-14D said:Just came across the excellent documentary. Had video I had never seen. I don't think anyone else has posted this URL here before.
According to Barrie Hygate, British Experimental Jet Aircraft, Argus (1990), page 248, "to improve lateral stability, the tips were given a marked downwards angle." Lateral stability is stability in roll, the resistance to dropping a wingtip. I find this odd, as "improve" usually means "increase", while the stability of such high-mounted swept or sort-of-delta wings is usually excessive and they are given downwards anhedral to reduce it. In the light of other replies, I wonder whether Hygate means to "improve" by reducing excessive stability.PMN1 said:What did the downward turned wingtips do for the aircraft?