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Nova MM 34-0
Part of Nova 0 stage series Family
LOx/LH2 propellant rocket stage. Operational date would have been June 1976. Booster stage (engines only).

Status: Study 1963. Thrust: 122,749.00 kN (27,595,072 lbf). Gross mass: 227,000 kg (500,000 lb). Unfuelled mass: 227,000 kg (500,000 lb). Specific impulse: 439 s. Specific impulse sea level: 382 s. Burn time: 190 s. Height: 18.20 m (59.70 ft). Diameter: 27.40 m (89.80 ft). Span: 33.00 m (108.00 ft).



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

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