The Armstrong Whitworth AW.681, also designated the Hawker Siddeley HS.681, was a projected British long-range military transport of the early 1960s, meant to take off and land in very short distances and, in a later form, vertically. Armstrong Whitworth, by then part of Hawker Siddeley Aviation, drew it up to meet Operational Requirement 351, which sought a replacement for the Blackburn Beverley and Handley Page Hastings. Four Rolls-Royce Medway turbofans with vectored thrust nozzles and blown flaps would have given it its short field performance. The government authorised a detailed study and a prototype in March 1962, with a first flight expected around 1966, but announced the cancellation of the programme in February 1965 and bought the American Lockheed Hercules instead. A cheaper non-STOL proposal, the HS.802, found no buyer, and the Armstrong Whitworth factory at Coventry closed.
Facts
Engine Class Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Armstrong Whitworth AW.681 (Wikipedia)
Of Make
Source Armstrong Whitworth AW.681 (Wikipedia)
Sources
1. Armstrong Whitworth AW.681 (Wikipedia)
Lead
was a projected British long-range STOL military transport aircraft design of the early 1960s
Design, powerplant
The AW.681 was to have been powered by an arrangement of four Rolls-Royce RB.142 Medway turbofan engines
Development, termination
During February 1965, the cancellation of the HS.681 programme was announced by the government
Development, background
Armstrong Whitworth, which was by then a constituent of Hawker Siddeley Aviation, submitted a design, the AW.681.
View the SourceReader Challenges (0)
No disputes yet. Spotted an error or a better source? Open the first one.
Sign in to dispute this or suggest a correction.