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

Status: Study 1963. Thrust: 26,683.00 kN (5,998,577 lbf). Gross mass: 2,721,000 kg (5,998,000 lb). Unfuelled mass: 245,000 kg (540,000 lb). Specific impulse: 428 s. Burn time: 383 s. Height: 50.50 m (165.60 ft). Diameter: 18.30 m (60.00 ft). Span: 18.30 m (60.00 ft).

No Engines: 4.



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

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