Saturn S-ID Booster

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z

Saturn S-ID Booster

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 recoverable. Mass estimated based on double mass of four F-1's (based on Atlas example).

Status: Study 1968. Thrust: 30,962.50 kN (6,960,647 lbf). Gross mass: 67,100 kg (147,900 lb). Unfuelled mass: 67,100 kg (147,900 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 154 s. Height: 42.07 m (138.02 ft). Diameter: 10.06 m (33.00 ft). Span: 19.01 m (62.36 ft).

No Engines: 4.

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

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z