Specifications (proposed STOL)
Data from Armstrong Whitworth Aircraft since 1913
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)
Read more about this topic: Armstrong Whitworth AW.681