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Saturn S-N V-25(S)U
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Gross Mass: 245,760 kg (541,800 lb). Empty Mass: 71,190 kg (156,940 lb). Thrust (vac): 889.325 kN (199,928 lbf). Isp: 825 sec. Burn time: 1,500 sec. Propellants: Nuclear/LH2. Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft). Length: 48.17 m (158.03 ft). Country: USA. No Engines: 1. Engine: Nerva. Status: Study 1968. Version of Nerva studied by Boeing for manned Mars expedition.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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