This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Nova 59-4-3, Nova 59-4-4. Used on launch vehicles: Nova 4L. Propellants: Lox/LH2 Thrust(vac): 36,274 kgf. Thrust(vac): 355.70 kN. Isp: 425 sec. Isp (sea level): 306 sec. Burn time: 656 sec. Mass Engine: 1,438 kg. Chambers: 1. Chamber Pressure: 30.00 bar. Area Ratio: 28.00. Country: USA. Status: Study 1959.
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Last update 12 March 2001.
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© Mark Wade, 2001 .