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Nova MM S10R-2
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 | Nova Model S10R-2 Nova Martin Marietta Model S10R-2 Credit - © Mark Wade
| 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. Propellants: Lox/LH2. 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). Country: USA. No Engines: 30. Engine: CD Module. Status: Study 1963. Operational date would have been July 1978. SSTO; recoverable; payload 842,000 lbs. Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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