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The Armstrong Whitworth AW.171 was a British project of the 1950s to develop a supersonic VTOL flying wing aircraft. Work was cancelled in 1957 before a prototype was completed.
[edit] Specification
- Length : 21.59m
- Wing Span: 5.36m
- Main Engine : Bristol Orpheus (2,200Kg) X 2
- Lift Engine : Rolls-Royce RB108 (953Kg) X 10
- All-Up Weight : 7,398Kg
- Max Speed : 2,387Km/h (Mach 2)
- Crew : 1
[edit] External link
[1]
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