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Saturn S-ID Sustainer
Part of Saturn IC
LOx/Kerosene propellant rocket stage. 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. Booster half stage burns 124 seconds in this configuration.

Status: Study 1968. Thrust: 7,740.30 kN (1,740,089 lbf). Gross mass: 2,219,100 kg (4,892,200 lb). Unfuelled mass: 68,100 kg (150,100 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 315 s. Height: 42.07 m (138.02 ft). Diameter: 10.06 m (33.00 ft). Span: 19.01 m (62.36 ft).



Country: USA. Engines: F-1. Launch Vehicles: Saturn V-B, Saturn V-C, Saturn V-D. Propellants: Lox/Kerosene.

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