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astronautix.com Nova GD-J-2
Advanced Engines
Advanced Engines
Advanced Engines planned for uprated Saturn and Nova boosters

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Gross Mass: 1,270,000 kg. Empty Mass: 91,000 kg. Thrust (vac): 1,361,000 kgf. Isp: 428 sec. Burn time: 365 sec. Propellants: Lox/LH2 Diameter: 19.5 m. Span: 19.5 m. Length: 38.0 m. Country: USA. No Engines: 2. M-1 Status: Study General Dynamics 1963. Comments: Massed estimated based on tank volumes, total thrust, and first stage burnout conditions. .
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Last update 12 March 2001.
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© Mark Wade, 2001 .