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USS Hopewell DD 681, Mesothelioma and Asbestos Exposure asbestos.com | JSSM- 2006, Vol.5, Issue 4, 672 - 681 jssm.org | Armstrong Therapeutic exercise, Back Exercise, Armstrong chiropractor, IA olesonchiropractic.com |
The Armstrong Whitworth AW.681, also known as the Whitworth Gloster 681 or Hawker Siddeley HS.681, was a projected British long-range STOL military transport aircraft design by Armstrong Whitworth Aircraft and was to be capable of development to VTOL performance. The AW.681 was designed to meet the NATO specification BMR-4.
[edit] Design and developmentTo meet Royal Air Force Operation Requirement 351 to specification C.241, Armstrong Whitworth's design was selected.[1] The aircraft featured a swept shoulder mounted wing and a high T-tail. The rear fuselage was upswept with loading doors and a ramp. Four Rolls-Royce RB.142 Medway engines with vectored thrust nozzles were to be mounted on pylons under the wings which were to feature boundary layer control with blown flaps, leading edges, and ailerons. The Medway engines would have given STOL performance only. The use of an additional 18 6,000 lbf (26.7 kN) RB.162-64 lift engines or replacement of the Medways with four Bristol Siddeley Pegasus ducted flow turbofans was proposed to obtain VTOL capability. The Pegasus 5-6 would have been rated at around 18,000 lbf (80 kN).[2] The project was under development for the Royal Air Force when it was cancelled in January 1965.[3] [edit] Specifications (proposed STOL)Data from Armstrong Whitworth Aircraft since 1913 [4] General characteristics
Performance
[edit] See alsoComparable aircraft [edit] References[edit] Notes
[edit] Bibliography
[edit] External links
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