Vickers Type 253
| Type 253 | |
|---|---|
 |
|
| Role | Multi-role military |
| National origin | United Kingdom |
| Manufacturer | Vickers-Armstrongs Ltd |
| Designer | R.K.Pierson & Barnes Wallis |
| Retired | 16 August 1934 |
| Number built | 1 |
The Vickers Type 253 was a single-engined two-seat biplane general-purpose military machine built to a 1930 government specification. It won a production contract, but this was transferred to the same company's monoplane equivalent, the Wellesley. Only one Type 253 was built.
In April 1932 the Air Ministry awarded a contract to Vickers for a single prototype aircraft under Air Ministry specification G.4/31 for a Westland Wapiti replacement, a multi-role aircraft capable of carrying out level bombing, army co-operation, dive bombing, reconnaissance, casualty evacuation and torpedo bombing. Vickers' entrant to this competition was the Type 253, though often known by the specification as the Vickers G.4/31. The Ministry had also ordered prototypes of other designs and some manufacturers had offered private ventures (aircraft built with their own money). The Type 253 was in competition with the Handley Page HP.47. Fairey G.4/31, Westland PV.7, Armstrong Whitworth A.W.19, Blackburn B-7, Hawker P.V.4 and the Parnall G.4/31. The Ministry preferred an air-cooled engine, and Vickers' choice was the radial Bristol Pegasus.
The Vickers Type 253 used a Pegasus IIM3 engine, enclosed by a drag-reducing Townend ring, to power a two-bay, unstaggered biplane, with a lower wing smaller in span and chord. Both wings were of constant chord, but the centre sections were mildly forward-swept and the lower centre section carried anhedral out to the inner interplane struts. Both sets of interplane struts leaned outwards, the outer ones more so. Both wings carried ailerons and the upper planes had leading edge slats. The wings joined the fuselage top and bottom with no gap, the pilot sitting just ahead of the leading edge in an open cockpit and the observer sitting well behind the trailing edge. A conventional tail carried balanced rudder and elevators. The split-axle fixed undercarriage was neatly mounted, the main legs fixed to the front spar under the inner interplane struts and braced rearwards to the wing roots.
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