The Vickers Type 151 Jockey was an experimental low-wing monoplane interceptor fighter powered by a radial engine, later modified into the Type 171 Jockey II with a more powerful engine and detail improvements. Only one was built. In the late 1920s the idea of the interceptor fighter was forming, and the Air Ministry sought under specification F.20/27 manufacturers to build biplanes and both low- and high-wing monoplanes; Vickers was asked for a low-wing prototype. It was a compact, angular cantilever monoplane built by the Wibault-Vickers corrugated skin all-metal method used on the Vireo, with a 480 hp Bristol Mercury IIA, later a 530 hp supercharged Jupiter VIIF. It was taken to Martlesham Heath for its first flight in April 1930. A rear fuselage vibration was cured after Barnes Wallis redesigned the internal bracing. The sole Jockey was lost in a flat spin on 5 July 1932, crashing at Woodbridge in Suffolk, but its lessons led to the Venom.
Facts
Engine Class Top Speed (km/h) EngineOne Bristol Jupiter VIIF nine-cylinder air-cooled radial engine, 530 hp 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Vickers Jockey (Wikipedia)
Of Make
Source Vickers Jockey (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Vickers Jockey (Wikipedia)DevelopmentQuote, Development
Vickers were asked for a prototype low-wing fighter
Originated In
Also in Geography Atlas: where this subject originated.
Source Vickers Jockey (Wikipedia)Development, country of originQuote, Development, country of origin
sought, under Air Ministry specification F.20/27, manufacturers to build biplanes and both low- and high-wing monoplanes
Sources
1. Vickers Jockey (Wikipedia)
Development, first flight
The Jockey was taken to RAF Martlesham Heath for its first flight in April 1930
Development, loss of the prototype
the sole Jockey was lost in a flat spin on 5 July 1932
Lead, one built
Only one was built
Lead
The Vickers Type 151 Jockey was an experimental low-wing monoplane interceptor fighter
Specifications, powerplant
Bristol Jupiter VIIF nine-cylinder air-cooled radial engine, 530 hp (400 kW)
Specifications, empty weight
Empty weight: 2,260 lb (1,025 kg)
Specifications, maximum speed
Maximum speed: 218 mph (351 km/h, 189 kn) at 10,000 ft (3,000 m)
Development
Vickers were asked for a prototype low-wing fighter
Development, country of origin
sought, under Air Ministry specification F.20/27, manufacturers to build biplanes and both low- and high-wing monoplanes
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