Saturn S-II Gross Mass: 100,000 kg (220,000 lb). Empty Mass: 14,000 kg (30,000 lb). Thrust (vac): 3,557.313 kN (799,716 lbf). Isp: 420 sec. Burn time: 100 sec. Propellants: Lox/LH2. Isp(sl): 300 sec. Diameter: 6.60 m (21.60 ft). Span: 6.60 m (21.60 ft). Length: 22.56 m (74.01 ft). Country: USA. No Engines: 4. Engine: J-2. Status: Study 1960. Used on Launch Vehicles: Saturn C-2.                   Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2007 except where otherwise noted.

Encyclopedia Astronautica topic index 0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z Enter your search terms   Web www.astronautix.com Submit search form