This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Mustard 1, Mustard 2. Used on launch vehicles: Mustard. Propellants: Lox/LH2 Thrust(vac): 220,000 kgf. Thrust(vac): 2,157.40 kN. Isp: 405 sec. Isp (sea level): 300 sec. Burn time: 215 sec. Chambers: 1. Country: UK. Status: Study 1967.
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Last update 12 March 2001.
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© Mark Wade, 2001 .