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Nova MM 14A-2
Part of Nova 2 stage series Family
LOx/LH2 propellant rocket stage. Operational date would have been April 1973.

Status: Study 1963. Thrust: 33,352.00 kN (7,497,827 lbf). Gross mass: 3,401,000 kg (7,497,000 lb). Unfuelled mass: 295,000 kg (650,000 lb). Specific impulse: 428 s. Burn time: 385 s. Height: 28.80 m (94.40 ft). Diameter: 18.30 m (60.00 ft). Span: 18.30 m (60.00 ft).

No Engines: 5.



Country: USA. Engines: M-1. Launch Vehicles: Nova MM 14A. Propellants: Lox/LH2.

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