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The F-1 is a rocket engine developed by Rocketdyne. The engine uses a gas-generator cycle developed in the United States in the late 1950s and was used in the Saturn V rocket in the 1960s and early 1970s. Five F-1 engines were used in the S-IC first stage of each Saturn V, which served as the main launch vehicle of the Apollo program.
F-1 rocket engine used in the Saturn program, Rocketdyne former main production facility, Canoga Park, Los Angeles. After World War II, North American Aviation (NAA) was contracted by the Defense Department to study the German V-2 missile and adapt its engine to Society of Automotive Engineers (SAE) measurements and U.S. construction details.
The following is a list of Formula One engine manufacturers. In Formula One motor racing, engine or power unit manufacturers are people or corporate entities which are credited as the make of Formula One engines that have competed or are intended to compete in the FIA Formula One World Championship. A constructor of an engine owns the ...
F1 Engine may refer to: Rocketdyne F-1, a type of gas-generator cycle rocket engine; The engine of a Formula One racing car This page was last edited on 28 ...
Engine Origin Designer Vehicle Status Use Propellant Power cycle Specific impulse (s) [a] Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [b] Oxidiser: fuel ratio
The F-1 engine was five years into its development at the time and still experiencing combustion stability problems. Rocketdyne eventually solved the F-1 instability problems by adding copper dividers as baffles, [15] but the RD-270 still had unsolved instability problems when the N1 program was cancelled in 1974, long after the F-1 problems ...
It would be a near-impossible project, sure, but at the end your car would have a 20,000 RPM Cosworth F1 engine.
While tripropellant engines have been tested by Rocketdyne and NPO Energomash, no tripropellant rocket has been flown. There are two different kinds of tripropellant rockets. One is a rocket engine which mixes three separate streams of propellants, burning all three propellants simultaneously.