F-1A

F-1A
Credit - Boeing / Rocketdyne

Manufacturer Name: F-1A. Designer: Rocketdyne. Developed in: 1967. Propellants: Lox/Kerosene. Thrust(vac): 9,189.600 kN (2,065,904 lbf). Thrust(sl): 8,003.800 kN (1,799,326 lbf). Isp: 310 sec. Isp (sea level): 270 sec. Burn time: 158 sec. Mass Engine: 8,098 kg (17,853 lb). Diameter: 3.61 m (11.84 ft). Length: 5.48 m (17.97 ft). Chambers: 1. Chamber Pressure: 70.00 bar. Area Ratio: 16.00. Thrust to Weight Ratio: 115.71. Country: USA. Status: Study 1968.

Designed for booster applications. Gas generator, pump-fed.

F-1A used on Rocket Stages

Used on stage: Nova GD-B-1. on launch vehicle: Nova GD-B.

Used on stage: Nova MM 1B-1. on launch vehicle: Nova MM 1B.

Used on stage: Nova MM 1C-1. on launch vehicle: Nova MM 1C.

Used on stage: Saturn MS-IC-1. on launch vehicle: Saturn MLV-V-1.

Used on stage: Saturn MS-IC-1. on launch vehicle: Saturn MLV-V-1/J-2T/200K.

Used on stage: Saturn MS-IC-1. on launch vehicle: Saturn MLV-V-1/J-2T/250K.

Used on stage: Saturn MS-IC-1. on launch vehicle: Saturn MLV-V-2.

Used on stage: Saturn MS-IC-1. on launch vehicle: Saturn MLV-V-3.

Used on stage: Saturn MS-IC-1. on launch vehicle: Saturn MLV-V-4(S)-B.

Used on stage: Saturn MS-IC-1. on launch vehicle: Saturn V-24(L).

Used on stage: Saturn MS-IC-25(S). on launch vehicle: Saturn V-25(S)B.

Used on stage: Saturn MS-IC-25(S). on launch vehicle: Saturn V-25(S)U.

Used on stage: Saturn MS-IC-25(S). on launch vehicle: Saturn V-4X(U).

Used on stage: Saturn MS-IC-3B. on launch vehicle: Saturn V-3B.

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