The Vickers Type 253 was a single-engined two-seat biplane general-purpose military aircraft built to a 1930 government specification, often known as the Vickers G.4/31. It won a production contract, but this was transferred to the company's monoplane equivalent, the Wellesley, and only one Type 253 was built. In April 1932 the Air Ministry awarded Vickers a contract for a single prototype under Specification G.4/31 for a Westland Wapiti replacement able to carry out level bombing, army cooperation, dive bombing, reconnaissance, casualty evacuation and torpedo bombing. It competed with the Handley Page HP.47, Fairey, Westland, Armstrong Whitworth, Blackburn, Hawker and Parnall entrants. It used a Pegasus IIM3 radial with a Townend ring in a two-bay unstaggered biplane. Its fuselage frame, designed by chief structural engineer Barnes Wallis, was a step toward his geodetic frames, with four light-alloy longerons joined by oppositely handed helical channel members.
Facts
Engine Class Top Speed (km/h) EngineOne Bristol Pegasus IIM3 nine-cylinder radial engine, 635 hp 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Vickers Type 253 (Wikipedia)
Of Make
Source Vickers Type 253 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Vickers Type 253 (Wikipedia)DevelopmentQuote, Development
In April 1932, the Air Ministry awarded a contract to Vickers for a single prototype aircraft
Originated In
Also in Geography Atlas: where this subject originated.
Source Vickers Type 253 (Wikipedia)Development, country of originQuote, Development, country of origin
In April 1932, the Air Ministry awarded a contract to Vickers for a single prototype aircraft under Air Ministry specification G.4/31
Sources
1. Vickers Type 253 (Wikipedia)
Lead, one built
Only one Type 253 was built.
Lead
was a single-engined two-seat biplane general-purpose military machine
Specifications, powerplant
1 × Bristol Pegasus IIM3 nine-cylinder radial engine, 635 hp (474 kW)
Specifications, empty weight
Empty weight: 4,500 lb (2,041 kg)
Specifications, maximum speed
Maximum speed: 161 mph (259 km/h, 140 kn) at 4,500 ft (1,400 m)
Development
In April 1932, the Air Ministry awarded a contract to Vickers for a single prototype aircraft
Development, country of origin
In April 1932, the Air Ministry awarded a contract to Vickers for a single prototype aircraft under Air Ministry specification G.4/31
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