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Nova MM 1B-2
Part of Nova 2 stage series Family
LOx/LH2 propellant rocket stage. Operational date would have been February 1973.

Status: Study 1963. Thrust: 13,346.00 kN (3,000,300 lbf). Gross mass: 1,361,000 kg (3,000,000 lb). Unfuelled mass: 122,000 kg (268,000 lb). Specific impulse: 428 s. Burn time: 383 s. Height: 45.40 m (148.90 ft). Diameter: 20.00 m (65.00 ft). Span: 20.00 m (65.00 ft).

No Engines: 2.



Country: USA. Engines: M-1. Launch Vehicles: Nova MM 1B. Propellants: Lox/LH2.

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