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J57-8
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Designer: Pratt and Whitney. Propellants: Air/Kerosene. Thrust(vac): 45.400 kN (10,206 lbf). Thrust(sl): 41.200 kN (9,262 lbf). Isp: 1,414 sec. Burn time: 3,000 sec. Chambers: 1. Country: USA. Status: Out of production. First Flight: 1960. Last Flight: 1962. Flown: 7.00. Thrust is maximum sea level thrust; specific impulse is sea level value at that thrust.
J57-8 used on Rocket Stages - Used on stage: F-6. on launch vehicle: Caleb.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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