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Boulton Paul P.92

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 inline 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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