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Nova MM 1B
Part of Nova
Nova Model 1B
Nova Model 1B
Nova Martin Marietta Model 1B
Credit: © Mark Wade
American heavy-lift orbital launch vehicle. Nova design using existing engines; 14 F-1A in the first stage, 2 M-1 in the second. Operational date would have been December 1972

Status: Study 1963. Payload: 330,000 kg (720,000 lb). Thrust: 112,117.60 kN (25,205,039 lbf). Gross mass: 9,187,000 kg (20,253,000 lb). Height: 110.00 m (360.00 ft). Diameter: 20.00 m (65.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 330,000 kg (720,000 lb) to a 185 km orbit.

Stage Data - Nova MM 1B



Family: heavy-lift, orbital launch vehicle. Country: USA. Engines: F-1A, M-1. Stages: Nova MM 1B-1, Nova MM 1B-2. Agency: Martin.

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