Nova MM S10R-2
Launch vehicle · USA
Original archive entry. The text, images and links below are kept as they were written.
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.
LEO Payload: 381,000 kg (839,000 lb) to a 185 km orbit.
Stage Data - Nova MM S10R-2
- Stage 1. 1 x Nova MM S10R-2. Gross Mass: 10,502,000 kg (23,152,000 lb). Empty Mass: 839,000 kg (1,849,000 lb). Thrust (vac): 160,672.000 kN (36,120,502 lbf). Isp: 454 sec. Burn time: 263 sec. Isp(sl): 377 sec. Diameter: 21.30 m (69.80 ft). Span: 40.90 m (134.10 ft). Length: 56.60 m (185.60 ft). Propellants: Lox/LH2. No Engines: 30. Engine: CD Module. Status: Study 1963. Comments: Operational date would have been July 1978. SSTO; recoverable; payload 842,000 lbs.
Related
- Family
- heavy-lift, orbital launch vehicle
- Country
- USA
- Engines
- CD Module
- Stages
- Nova MM S10R-2 stage
- Agency
- Martin