Nova MM 14A-2
Advanced Engines
Advanced Engines planned for uprated Saturn and Nova boosters
Credit - © Mark Wade
Gross Mass: 3,401,000 kg (7,497,000 lb). Empty Mass: 295,000 kg (650,000 lb). Thrust (vac): 33,352.000 kN (7,497,827 lbf). Isp: 428 sec. Burn time: 385 sec. Propellants: Lox/LH2. Diameter: 18.30 m (60.00 ft). Span: 18.30 m (60.00 ft). Length: 28.80 m (94.40 ft). Country: USA. No Engines: 5. Engine: M-1. Status: Study 1963.

Operational date would have been April 1973

Used on Launch Vehicles:  
 
 
 
 
 
 
 
 
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