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Nova MM S10R-1
Part of Nova
Nova Model S10R-1
Nova Model S10R-1
Nova Martin Marietta Model S10R-1
Credit: © Mark Wade
American heavy-lift orbital launch vehicle. Reusable single stage to orbit Nova using cylindrical shape, 24 CD module engines in zero-length plug nozzle. Operational date would have been June 1978.

Status: Study 1963. Payload: 414,000 kg (912,000 lb). Thrust: 133,421.60 kN (29,994,369 lbf). Gross mass: 10,966,800 kg (24,177,600 lb). Height: 83.00 m (272.00 ft). Diameter: 24.40 m (80.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 414,000 kg (912,000 lb) to a 185 km orbit.

Stage Data - Nova MM S10R-1



Family: heavy-lift, orbital launch vehicle. Country: USA. Engines: CD Module. Stages: Nova MM S10R-1 stage. Agency: Martin.

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