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Saturn II-INT-17
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Gross Mass: 495,000 kg (1,091,000 lb). Empty Mass: 48,000 kg (105,000 lb). Thrust (vac): 9,713.400 kN (2,183,659 lbf). Isp: 450 sec. Burn time: 200 sec. Propellants: Lox/LH2. Isp(sl): 275 sec. Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft). Length: 24.84 m (81.49 ft). Country: USA. No Engines: 7. Engine: HG-3-SL. Status: Study 1966. Saturn II modifed with reduced expansion ratio HG-3 high pressure engines for use a first stage (sea level launch).
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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