Nova GD-E-2
Advanced Engines
Advanced Engines planned for uprated Saturn and Nova boosters
Credit - © Mark Wade
Gross Mass: 4,535,000 kg (9,997,000 lb). Empty Mass: 363,000 kg (800,000 lb). Thrust (vac): 26,683.000 kN (5,998,577 lbf). Isp: 428 sec. Burn time: 646 sec. Propellants: Lox/LH2. Diameter: 20.60 m (67.50 ft). Span: 20.60 m (67.50 ft). Length: 47.90 m (157.10 ft). Country: USA. No Engines: 4. 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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