Bristol 188

1962

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  RESEARCH AIRCRAFTVirtual Aircraft Museum / United Kingdom / Bristol  

Bristol 188

The Bristol 188, sometimes called the 'flaming pencil', was designed to research structures for sustained supersonic flight, particularly in support of the Avro 730 reconnaissance aircraft. This required the aircraft to 'soak' at Mach 2.6 for at least 30 minutes. To achieve the required strength the structure was largely stainless steel, which required new techniques and great expense to fabricate into an airframe.

Take-off speed was nearly 483km/h, but in all other respects the 188's speed was slower than desired, being able to achieve Mach 2.0 for only a couple of minutes. The whole project cost a huge GBP20 million and failed to achieve its objectives. It was wound down rather than develop the engines further. Test pilot Godfrey Auty was voted the 'man most likely to eject in the coming year' by his peers but thankfully never had to.

FACTS AND FIGURES

© A new type of stainless steel, joined by a new 'puddle' welding process was needed fot the 188. It took over two years to develop the steel before it could even be ordered for construction use.

© The PS.50 (modified Gyron Junior) engines had greater diameter than the fuselage but never developed enough thrust to push the 188 to the high speeds required.

© Fuel capacity was usually only enough for 20-25 minutes flight including a high-speed run. By airline standards the 188 was in a fuel emergency situation before take-off.

Bristol 188 on YOUTUBE

Bristol 188

Specification 
 MODELT.188
 CREW1
 ENGINE2 x 6350kg de Havilland Gyron Junior DGJ 10
 DIMENSIONS
  Wingspan10.69 m35 ft 1 in
  Length21.64 m71 ft 0 in
  Height4.06 m13 ft 4 in
  Wing area36.79 m2396.00 sq ft
 PERFORMANCE
  Max. speed1932 km/h1201 mph

3-View 
Bristol 188A three-view drawing (700 x 641)

Comments1-20 21-40
R Morris, e-mail, 26.01.2010 12:56

Never to be forgottten aircraft. Since i first saw it at as a child at farnborough with a view right up it tail as it climbeed out.

reply

Cliff, e-mail, 01.07.2009 13:56

I was the flying control mechanic responsible for installation on this a /c.

reply

L.DOWLING, e-mail, 11.11.2006 10:38

THE T.188 NEVER ACHIVED ITS ROLE OF EXPLORING THE 'HEAT BARRIER' KENETIC HEATING DUE TO AERODYNAMIC FRICTION.DUE TO ITS LIMETED ENDURANCE. BUT IT HAS LOTS OF 'WOW FACTOR' DUE TO ITS ADVANCED AERODYNAMICS.

reply

1-20 21-40

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