Saturn S-ID Sustainer-1

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Saturn S-ID Sustainer-1

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; 20 foot stretch of sustainer stage. Booster stage burn 154 seconds in this configuration.

Status: Study 1967. Thrust: 7,740.30 kN (1,740,089 lbf). Gross mass: 2,627,600 kg (5,792,800 lb). Unfuelled mass: 84,400 kg (186,000 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 371 s. Height: 48.16 m (158.00 ft). Diameter: 10.06 m (33.00 ft). Span: 19.01 m (62.36 ft).

Country: USA. Engines: F-1. Propellants: Lox/Kerosene.

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