Nova MM R10R-2
Nova Model R10E/R10R
Nova Martin Marietta Model R10E-2 / R10R-2
Credit - © Mark Wade
Gross Mass: 8,647,000 kg (19,063,000 lb). Empty Mass: 1,361,000 kg (3,000,000 lb). Thrust (vac): 140,539.000 kN (31,594,424 lbf). Isp: 620 sec. Burn time: 310 sec. Propellants: Air/Lox/LH2. Isp(sl): 620 sec. Diameter: 21.30 m (69.80 ft). Span: 43.70 m (143.30 ft). Length: 49.30 m (161.70 ft). Country: USA. No Engines: 40. Engine: CD Module. Status: Study 1963.

Operational date would have been October 1980. Recoverable stage. Air-augmented plug nozzle.

Used on Launch Vehicles:  
 
 
 
 
 
 
 
 
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