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astronautix.com Nova MM 14A-2
Advanced Engines
Advanced Engines
Advanced Engines planned for uprated Saturn and Nova boosters

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Gross Mass: 3,401,000 kg. Empty Mass: 295,000 kg. Thrust (vac): 3,401,000 kgf. Isp: 428 sec. Burn time: 385 sec. Propellants: Lox/LH2 Diameter: 18.3 m. Span: 18.3 m. Length: 28.8 m. Country: USA. No Engines: 5. M-1 Status: Study 1963. Comments: Operational date would have been April 1973 .
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Last update 12 March 2001.
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© Mark Wade, 2001 .