Nova GD-J-2
Advanced Engines
Advanced Engines planned for uprated Saturn and Nova boosters
Credit - © Mark Wade
Gross Mass: 1,270,000 kg (2,790,000 lb). Empty Mass: 91,000 kg (200,000 lb). Thrust (vac): 13,346.000 kN (3,000,300 lbf). Isp: 428 sec. Burn time: 365 sec. Propellants: Lox/LH2. Diameter: 19.50 m (63.90 ft). Span: 19.50 m (63.90 ft). Length: 38.00 m (124.00 ft). Country: USA. No Engines: 2. Engine: M-1. Status: Study 1963.

Massed estimated based on tank volumes, total thrust, and first stage burnout conditions.

Used on Launch Vehicles:  
 
 
 
 
 
 
 
 
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