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Nova MM 33-1
Part of Nova 1 stage series Family
LOx/LH2 propellant rocket stage. Operational date would have been April 1975. SSTO - payload 1,042,000 lbs.

Status: Study 1963. Thrust: 156,876.00 kN (35,267,127 lbf). Gross mass: 10,489,000 kg (23,124,000 lb). Unfuelled mass: 626,000 kg (1,380,000 lb). Specific impulse: 443 s. Specific impulse sea level: 379 s. Burn time: 268 s. Height: 75.90 m (249.00 ft). Diameter: 24.40 m (80.00 ft). Span: 26.20 m (85.90 ft).

No Engines: 24.



Country: USA. Engines: HP-1. Launch Vehicles: Nova MM 33. Propellants: Lox/LH2.

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