- Fighter
- Interception
- Ground Attack
- Reconnaissance (RECCE)
- X-Plane / Developmental
Length:
69.06 ft (21.05 m)
Width:
37.01 ft (11.28 m)
1 x de Havilland Gyron PS.26-6 OR PS.26-3 afterburning turbojet engine developing 17,400lb to 20,000lb (respectively) thrust (dry) and 23,800lb to 27,000lb (respectively) thrust with reheat.
Max Speed:
1,920 mph (3,090 kph; 1,668 kts)
Service Ceiling:
58,071 feet (17,700 m; 11 miles)
Max Range:
1,553 miles (2,500 km; 1,350 nm)
Rate-of-Climb:
40,000 ft/min (12,192 m/min)
(Showcased performance values pertain to the Hawker P.1121 production model; Compare this aircraft entry against any other in our database)
PROPOSED:
2 x 30mm ADEN automatic cannons installed internally.
2 x "Red Top" air-to-air missiles (AAMs) at underwing hardpoints (one missile per wing).
Also support for 50 x 2" RP aerial rockets, nuclear-tipped drop bombs, and underwing fuel drop tanks.
(Showcased armament details pertain to the Hawker P.1121 production model)
P.1121 - Base project designation; incomplete prototype.
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