Saturn MS-IC-25(S)
Advanced Engines
Advanced Engines planned for uprated Saturn and Nova boosters
Credit - © Mark Wade
Gross Mass: 3,223,800 kg (7,107,200 lb). Empty Mass: 211,900 kg (467,100 lb). Thrust (vac): 45,925.500 kN (10,324,463 lbf). Isp: 304 sec. Burn time: 192 sec. Propellants: Lox/Kerosene. Isp(sl): 265 sec. Diameter: 10.06 m (33.00 ft). Span: 19.00 m (62.00 ft). Length: 54.70 m (179.40 ft). Country: USA. No Engines: 5. Engine: F-1A. Status: Study 1968.

S-IC with 41.5 foot stretch, 6,640,0000 lbs propellant, uprated F-1 engines.

Used on Launch Vehicles:  
 
 
 
 
 
 
 
 
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