Nova MM 1C-2
Advanced Engines
Advanced Engines planned for uprated Saturn and Nova boosters
Credit - © Mark Wade
Gross Mass: 2,041,000 kg (4,499,000 lb). Empty Mass: 163,000 kg (359,000 lb). Thrust (vac): 20,015.000 kN (4,499,550 lbf). Isp: 428 sec. Burn time: 387 sec. Propellants: Lox/LH2. Diameter: 18.30 m (60.00 ft). Span: 18.30 m (60.00 ft). Length: 49.70 m (163.00 ft). Country: USA. No Engines: 3. Engine: M-1. Status: Study 1963.

Operational date would have been February 1973

Used on Launch Vehicles:  
 
 
 
 
 
 
 
 
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