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XV208, Lockheed C-130K Hercules W2, A400M Engine test, W2 XV208, Allison TP-400XV208, Lockheed C-130K Hercules W2, A400M Engine test, W2 XV208, Allison TP-400Hi bypass FanjetHi bypass Fanjet, jet engineGuiberson A/T-1020 Diesel Engine, radial, four strokeWright J65 Turbojet, axial-flow turbojet, jet, 1948, 1940sCurtiss OX-SCurtiss OX-SCurtiss OX-S
Wright J65 Turbojet, axial-flow turbojet, jet, 1948, 1940s
Code Number:
IAPD01_014
Title:
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:
Aerospace, industry, manufacturing, Powerplants, Aviation Power Plant, Engines, Propulsion, Thrust
Image by:
Wernher Krutein

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