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

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Gross Mass: 1,633,000 kg. Empty Mass: 113,000 kg. Thrust (vac): 1,361,000 kgf. Isp: 426 sec. Burn time: 468 sec. Propellants: Lox/LH2 Diameter: 21.3 m. Span: 21.3 m. Length: 21.3 m. Country: USA. No Engines: 4. M-1 Status: Study 1963. Comments: Operational date would have been July 1977. Recoverable stage. .
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Last update 12 March 2001.
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© Mark Wade, 2001 .