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F-1A -

Credit: Boeing / Rocketdyne. 9,728 bytes. 160 x 235 pixels.

Manufacturer Name: F-1A. Designer: Rocketdyne. Developed in: 1967. Application: . Used on stages: Nova GD-B-1, Nova MM 1B-1, Nova MM 1C-1, Saturn MS-IC-1, Saturn MS-IC-25(S), Saturn MS-IC-3B. Used on launch vehicles: Nova GD-B, Nova MM 1B, Nova MM 1C, Saturn MLV-V-1, Saturn MLV-V-1/J-2T/200K, Saturn MLV-V-1/J-2T/250K, Saturn MLV-V-2, Saturn MLV-V-3, Saturn MLV-V-4(S)-B, Saturn V-24(L), Saturn V-25(S)B, Saturn V-25(S)U, Saturn V-3B, Saturn V-4X(U). Propellants: Lox/Kerosene Thrust(vac): 937,093 kgf. Thrust(vac): 9,189.60 kN. Isp: 310 sec. Isp (sea level): 270 sec. Burn time: 158 sec. Mass Engine: 8,098 kg. Diameter: 3.6 m. Length: 5.5 m. Chambers: 1. Chamber Pressure: 70.00 bar. Area Ratio: 16.00. Country: USA. Status: Study NASA 1966. Comments: Designed for booster applications. Gas generator, pump-fed.

Advanced EnginesAdvanced Engines - Advanced Engines planned for uprated Saturn and Nova boosters

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Last update 12 March 2001.
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