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Nova MM S10R-1 stage
Part of Nova 1 stage series
LOx/LH2 propellant rocket stage. Operational date would have been June 1978. SSTO; recoverable.
 AKA: Nova MM S10R-1.  Status: Study 1963. Thrust: 160,672.00 kN (36,120,502 lbf). Gross mass: 10,470,000 kg (23,080,000 lb). Unfuelled mass: 816,000 kg (1,798,000 lb). Specific impulse: 454 s. Specific impulse sea level: 377 s. Burn time: 263 s. Height: 69.50 m (228.00 ft). Diameter: 24.40 m (80.00 ft). Span: 32.20 m (105.60 ft). 
No Engines: 24. 
Country: 
USA. 
Engines: 
CD Module. 
Launch Vehicles: 
Nova MM S10R-1. 
Propellants: 
Lox/LH2. 
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