This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: General Electric. Used on stages: XB-70. Propellants: Air/Kerosene Thrust(vac): 8,843 kgf. Thrust(vac): 86.70 kN. Isp: 2,084 sec. Burn time: 11,000 sec. Chambers: 1. Country: USA. Status: Out of Production. Comments: Thrust is maximum sea level thrust; specific impulse is sea level value at that thrust.
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Last update 12 March 2001.
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© Mark Wade, 2001 .