The Armstrong Whitworth A.W.23 was a prototype bomber and transport aircraft built by Armstrong Whitworth Aircraft to Air Ministry Specification C.26/31, which asked for a dual-purpose machine for the Royal Air Force with the emphasis on the transport role. Designer John Lloyd made it a low-wing twin-engine monoplane powered by two Armstrong Siddeley Tiger engines, with a fabric-covered steel fuselage holding a large cabin and bomb racks under the floor. Its wing used a patented light-alloy box spar braced with steel tubes, strong but thick and draggy, and the structure was reused on the Whitley bomber. It was the company's first aircraft with a retractable undercarriage. The prototype flew on 4 June 1935 but unreliable engines delayed testing and the Bristol Bombay won. It later served Flight Refuelling Ltd and was destroyed in a German raid in 1940.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) EngineArmstrong Siddeley Tiger VI 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Armstrong Whitworth A.W.23 (Wikipedia)
Of Make
Source Armstrong Whitworth A.W.23 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Armstrong Whitworth A.W.23 (Wikipedia)Lead, builderQuote, Lead, builder
was a prototype bomber/transport aircraft produced to specification C.26/31 for the British Air Ministry by Armstrong Whitworth Aircraft
Originated In
Also in Geography Atlas: where this subject originated.
Source Armstrong Whitworth A.W.23 (Wikipedia)Lead, originQuote, Lead, origin
was a prototype bomber/transport aircraft produced to specification C.26/31 for the British Air Ministry by Armstrong Whitworth Aircraft
Sources
1. Armstrong Whitworth A.W.23 (Wikipedia)
Lead, builder
was a prototype bomber/transport aircraft produced to specification C.26/31 for the British Air Ministry by Armstrong Whitworth Aircraft
Lead, origin
was a prototype bomber/transport aircraft produced to specification C.26/31 for the British Air Ministry by Armstrong Whitworth Aircraft
Design and development, first flight
first flying on 4 June 1935
Design and development, fate
It was destroyed in a German bombing raid on Ford airfield in June 1940.
Lead, type
was a prototype bomber/transport aircraft
Specifications, powerplant
Powerplant: 2 × Armstrong Siddeley Tiger VI 14-cylinder radial engines, 810 hp (600 kW)
Specifications, engine type
Powerplant: 2 × Armstrong Siddeley Tiger VI 14-cylinder radial engines, 810 hp (600 kW)
Specifications, gross weight
Gross weight: 24,100 lb (10,932 kg)
Design and development, number built
A prototype, K3585, was built first flying on 4 June 1935.
Of Make: Armstrong Whitworth Aircraft, Lead, maker
was a prototype bomber/transport aircraft produced to specification C.26/31 for the British Air Ministry by Armstrong Whitworth Aircraft
Exemplifies: Aviation, Lead, aircraft type
was a prototype bomber/transport aircraft produced to specification C.26/31 for the British Air Ministry by Armstrong Whitworth Aircraft
In Group: Military Transport Aircraft, Lead, role
was a prototype bomber/transport aircraft produced to specification C.26/31 for the British Air Ministry by Armstrong Whitworth Aircraft
View the Source2. Aviastar: Armstrong Whitworth A.W.23
AviastarSpecification, performanceQuote, Specification, performance
Max. speed 282 km/h 175 mph
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