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Nova MM 24G
Part of Nova
Nova Model 24G
Nova Model 24G
Nova Martin Marietta Model 24G
Credit: © Mark Wade
American heavy-lift orbital launch vehicle. Nova design using new high pressure LH2/LOx engines; 18 in the first stage in a plug nozzle arrangement, 2 in the second. Operational date would have been December 1974.

Status: Study 1963. Payload: 447,000 kg (985,000 lb). Thrust: 80,053.70 kN (17,996,788 lbf). Gross mass: 6,619,400 kg (14,593,200 lb). Height: 94.00 m (308.00 ft). Diameter: 21.60 m (70.80 ft). Apogee: 185 km (114 mi).

LEO Payload: 447,000 kg (985,000 lb) to a 185 km orbit.

Stage Data - Nova MM 24G



Family: heavy-lift, orbital launch vehicle. Country: USA. Engines: HP-1. Stages: Nova MM 24G-2, Nova MM-1. Agency: Martin.
Photo Gallery

Nova 24G, 34, and 33Nova 24G, 34, and 33
Nova Martin Marietta designs 24G, 34, and 33
Credit: Lockheed Martin



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