Armstrong Whitworth AW.681

Airplanes

Length

31.6992 m

Flat Wing Span

40.8432 m

Height

11.2776 m

Flat Wing Area

209.0318 m²

Max Mach

0.71 Mach

Number of Engines

Aircraft Engine

Maximum Range

7724.851 km

Pictures

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Aircraft	Maximum Range (km)
Armstrong Whitworth AW.681	7724.851

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Short S.26	Bristol Hercules	30.7848	40.8432	38	Compare
Nakajima G5N Shinzan	Mitsubishi Kasei	31.02	42.12		Compare
Lockheed C-130 Hercules	Allison T56	29.5656	40.2336		Compare
Lockheed EC-130		29.5656	40.2336		Compare
Breda-Zappata BZ.308	Bristol Centaurus	33.52	42.1	54	Compare
Lockheed XB-30	Wright R-3350 Duplex-Cyclone	31.91	37.5		Compare

All data (16 fields)

Name: Armstrong Whitworth AW.681
Manufacturer: Armstrong Whitworth
Description: 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.
Designer: Armstrong Whitworth
Length (m): 31.6992
Height (m): 11.2776
Capacity Description: 35000 lb
Max Mach (Mach): 0.71
Powerplant Description: 4 × Rolls-Royce Medway turbofans with thrust deflection
Primary Users: Royal Air Force (intended)
Status: Project cancelled in February 1965
Wikipedia Article (URL): en.wikipedia.org/wiki/Armstrong_Whitworth_AW.681
Flat Wing Span (m): 40.8432
Flat Wing Area (m²): 209.0318
Aircraft Engine: Rolls-Royce Medway
Number of Engines: 4