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Nova MM 34-1
Part of Nova 1 stage series Family
LOx/LH2 propellant rocket stage. Operational date would have been June 1976. Sustainer stage (required 4-engine booster stage).

Status: Study 1963. Thrust: 30,685.00 kN (6,898,262 lbf). Gross mass: 10,126,000 kg (22,324,000 lb). Unfuelled mass: 544,000 kg (1,199,000 lb). Specific impulse: 439 s. Specific impulse sea level: 382 s. Burn time: 388 s. Height: 84.80 m (278.20 ft). Diameter: 24.40 m (80.00 ft). Span: 24.40 m (80.00 ft).



Country: USA. Engines: L6H. Launch Vehicles: Nova MM 34. Propellants: Lox/LH2.

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