Armstrong Whitworth AW.681
| AW.681 / HS.681 | |
|---|---|
 |
|
| Manufacturer's model of the AW.681 | |
| Role | Projected VTOL Military transport |
| Manufacturer | Hawker Siddeley |
| Status | Project cancelled February 1965 |
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 of the early-1960s by Armstrong Whitworth Aircraft and was to be capable of development to VTOL performance. The AW.681 was designed to meet the NATO specification NBMR-4.
Contents
Design and development
Operational Requirement 351 was issued to meet a requirement for the Royal Air Force for a medium-range freighter to replace the Beverley and Hastings. There were proposals from British Aircraft Corporation and Hawker Siddeley, the former offering the BAC.222 based on the Lockheed Hercules and the BAC.208 with deflected thrust engines and lift fans.[1] Armstrong Whitworth's design was selected.[2]
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).[3]
In March 1962 the government announced the go-ahead for the HS.681 with a project study and a prototype to fly in 1966. With a load of 60 troops it was expected that 50 aircraft would be ordered. Some of the production work would be sub-contracted to Short Brothers in Belfast. In 1964 when a Labour Party formed a government it announced a review of military programmes. The project was cancelled in February 1965 when the government announced it would buy the American Lockheed Hercules instead.[4]
Armstrong Whitworth made a last-minute effort to promote a non-STOL version of the HS.681, designated the HS.802 which used the wings and engines from the HS.801 Nimrod.[5] As a consequence of the cancellation the Armstrong Whitworth factory in Coventry was closed with a loss of 5,000 jobs.[6]
Specifications (proposed STOL)
Data from Armstrong Whitworth Aircraft since 1913.[7]
General characteristics
- Payload: 35,000 lb (15,900 kg)
- Length: 104 ft 2 in (31.75)
- Wingspan: 134 ft (40.84)
- Height: 37 ft 10 in (11.53 m)
- Wing area: 2,250 sq ft (209 m²)
- Max. takeoff weight: 181,200 lb (82,360 kg)
- Powerplant: 4 × Rolls-Royce Medway turbofans with thrust deflection, 13,790 lb (61.3 kN) each
Performance
- Maximum speed: Mach 0.71
- Range: 4,801 mi (7,725 km)
- Service ceiling: 25,000 ft (7,620 m)
See also
- Aircraft of comparable role, configuration and era
- Related lists
References
Notes
- ↑ Lua error in package.lua at line 80: module 'strict' not found.
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- ↑ Pegasus engine variants
- ↑ Our Aeronautical Correspondent. "£300M. Saving In Ten Years On Aircraft." Times [London, England] 3 Feb. 1965: 10. The Times Digital Archive. Web. 27 Nov. 2012.
- ↑ [Our Correspondent-COVENTRY, FEB. 4. "Utility Version Of Transport At Half Cost Suggested." Times [London, England] 5 Feb. 1965: 12. The Times Digital Archive. Web. 27 Nov. 2012.]
- ↑ ["News in Brief." Times [London, England] 11 Feb. 1965: 6. The Times Digital Archive. Web. 27 Nov. 2012.]
- ↑ Tapper 1988, p.344.
Bibliography
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External links
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Wikimedia Commons has media related to Armstrong Whitworth AW.681. |
