This page no longer updated from 31 October 2001. Latest version can be found at LR-87+

Used on stages: Astrorocket-1, Astrorocket-2. Used on launch vehicles: Martin Astrorocket. Propellants: N2O4/Aerozine-50 Thrust(vac): 166,666 kgf. Thrust(vac): 1,634.40 kN. Isp: 293 sec. Isp (sea level): 258 sec. Burn time: 164 sec. Chambers: 1. Country: USA. Status: Study 1965.
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Last update 12 March 2001.
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© Mark Wade, 2001 .