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Nova MM S10R-2
Part of Nova
Nova Model S10R-2
Nova Model S10R-2
Nova Martin Marietta Model S10R-2
Credit: © Mark Wade
American heavy-lift orbital launch vehicle. Reusable single stage to orbit Nova using conical shape, 30 CD module engines in zero-length plug nozzle. Operational date would have been July 1978.

Status: Study 1963. Payload: 381,000 kg (839,000 lb). Thrust: 133,421.60 kN (29,994,369 lbf). Gross mass: 10,959,200 kg (24,160,900 lb). Height: 68.00 m (223.00 ft). Diameter: 21.30 m (69.80 ft). Apogee: 185 km (114 mi).

LEO Payload: 381,000 kg (839,000 lb) to a 185 km orbit.

Stage Data - Nova MM S10R-2



Family: heavy-lift, orbital launch vehicle. Country: USA. Engines: CD Module. Stages: Nova MM S10R-2 stage. Agency: Martin.

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