Boulton Paul P.92

 

1st Flight 1941

The Boulton Paul P.92 was a British design for a two-seat, turret-armed, twin-engine heavy fighter and ground attack aircraft to meet Air Ministry Specification F.11/37.

Only a half scale prototype – the P.92/2 – was built and tested on its aerodynamics before the project was cancelled in 1940.

Specifications

Crew: 1

Length: 27 ft 6 in (8.38 m)

Wingspan: 33 ft (10 m)

Height: 7.6 ft (2.3 m)

Gross weight: 2,778 lb (1,260 kg)

Powerplant: 2 × de Havilland Gipsy Major II 4-cylinder inverted in-line air-cooled piston engine, 130 hp (97 kW) each

Performance

Maximum speed: 152 mph (245 km/h, 132 kn) at sea level

Cruise speed: 84 mph (135 km/h, 73 kn).

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