This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: Rolls Royce. Used on stages: L-1011. Used on launch vehicles: Pegasus, Pegasus XL. Propellants: Air/Kerosene Thrust(vac): 3,000 kgf. Thrust(vac): 29.40 kN. Isp: 9,900 sec. Burn time: 4,590 sec. Mass Engine: 4,180 kg. Chambers: 1. Country: UK. Status: In 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 .