This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Timberwind 45. Used on launch vehicles: Timberwind Centaur. Propellants: Nuclear/LH2 Thrust(vac): 45,000 kgf. Thrust(vac): 441.30 kN. Isp: 1,000 sec. Isp (sea level): 890 sec. Burn time: 449 sec. Mass Engine: 1,500 kg. Diameter: 4.3 m. Chambers: 1. Thrust to Weight Ratio: 30.00. Country: USA. Status: Developed -1990.
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Last update 12 March 2001.
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© Mark Wade, 2001 .