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Saturn S-ID Sustainer-1
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Gross Mass: 2,627,600 kg (5,792,800 lb). Empty Mass: 84,400 kg (186,000 lb). Thrust (vac): 7,740.300 kN (1,740,089 lbf). Isp: 304 sec. Burn time: 371 sec. Propellants: Lox/Kerosene. Isp(sl): 265 sec. Diameter: 10.06 m (33.00 ft). Span: 19.01 m (62.36 ft). Length: 48.16 m (158.00 ft). Country: USA. No Engines: 1. Engine: F-1. Status: Study 1967. Boeing studies, 1967:'Stage and a half' S-1C with four outboard F-1's jettisoned and inboard F-1 functioning as sustainer as in Atlas; 20 foot stretch of sustainer stage. Booster stage burn 154 seconds in this configuration.
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