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

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Gross Mass: 2,268,000 kg. Empty Mass: 143,000 kg. Thrust (vac): 2,721,000 kgf. Isp: 426 sec. Burn time: 327 sec. Propellants: Lox/LH2 Diameter: 21.3 m. Span: 21.3 m. Length: 27.4 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 .