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- Code Number:
- IAPD01_014
- Title:
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Wright J65 Turbojet, axial-flow turbojet, jet, 1948, 1940s
- Major users: A-4 Skyhawk, Martin B-57 Canberra, Republic F-84F Thunderstreak
Developed from the Armstrong Siddeley Sapphire
Length: ~122in (~3098 mm) Diameter: 37.52in (953 mm) Dry weight: 2776lb (1259 kg) Compressor: 13-stage axial Combustors: annular Turbine: 2-stage axial Maximum thrust: 7239lbf (32.2KN) Overall pressure ratio: 7:1 Air mass flow: 119.05lb/s (54kg/s) Turbine inlet temperature: ~848C (1558F) Specific fuel consumption: ~0.916 lb/(lbf?h) (25.9 g/(kN?s)) Thrust-to-weight ratio: 2.61
- Keywords:
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Aerospace, industry, manufacturing, Powerplants, Aviation Power Plant, Engines, Propulsion, Thrust
- Image by:
- Wernher Krutein
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