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Nova 60-8-2
Part of Nova 2 stage series Family

Advanced Engines

Advanced Engines
Advanced Engines planned for uprated Saturn and Nova boosters
Credit: © Mark Wade

LOx/LH2 propellant rocket stage. Mass estimated based on total LV weight. J-2-powered version of this stage also proposed.

Status: Study 1960. Thrust: 10,669.00 kN (2,398,486 lbf). Gross mass: 680,000 kg (1,490,000 lb). Unfuelled mass: 54,000 kg (119,000 lb). Specific impulse: 428 s. Specific impulse sea level: 310 s. Burn time: 242 s. Height: 35.10 m (115.10 ft). Diameter: 11.60 m (38.00 ft). Span: 11.60 m (38.00 ft).

No Engines: 2.



Country: USA. Engines: M-1. Launch Vehicles: Nova 4S, Nova 7S, Nova 8L. Propellants: Lox/LH2.

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