MVP Archive History | Apollo Archive Special 06 : F-1 ENGINE

Basic Information
Name: F-1 Rocket Engine
Manufacturer: Rocketdyne
Operational Period: 1967 – 1973
Application: Saturn V First Stage (S-IC)
Fuel: RP-1 (Kerosene)
Oxidizer: Liquid Oxygen (LOX)
Thrust: Approx. 680 tons
What is the F-1 Engine?
The F-1 engine is a liquid-fuel rocket engine that was mounted on the first stage of the Saturn V rocket used in the Apollo program.
Even today, it possesses one of the highest thrusts of any single-combustion chamber liquid-fuel rocket engine that has actually flown.
It was the driving force that sent humanity from Earth into space during the Apollo program.
Structure
The F-1 engine was composed of a massive combustion chamber, a nozzle, and a high-output turbopump.
It generates thrust by burning the fuel, RP-1, and liquid oxygen, and ejecting ultra-high-temperature, ultra-high-pressure gas from the nozzle.
While its structure may appear simple, it was a collection of extremely advanced technology for its time.
Relationship with Saturn V
Five F-1 engines were mounted on the first stage of the Saturn V.
At liftoff, all five were ignited simultaneously, reaching a total thrust of approximately 3,400 tons.
This immense thrust allowed the Saturn V, which exceeded 110 meters in total length, to leave Earth.
Performance
Thrust
Approx. 1.5 Million lbf (Approx. 680 tons)
Height
Approx. 5.8 m
Diameter
Approx. 3.7 m
Weight
Approx. 8.4 t
Burn Time
Approx. 150 seconds
Number of units
5 per Saturn V
What was achieved
The F-1 engine supported manned lunar exploration missions from Apollo 8 through Apollo 17.
It was also used for the launch of the Skylab space station.
Both humanity's first moon landing and the return of Apollo 13 began with a launch powered by F-1 engines.
Technical significance
The F-1 engine is not merely a large engine.
It was required to generate extremely high thrust while maintaining high reliability and stability.
The success of the Apollo program could not have been realized without the completion of this engine.
For this reason, it is still discussed today as one of the representative technical achievements in rocket engineering.
Afterward
After the Apollo program ended, the operation of the F-1 engine also concluded.
However, its design philosophy and development experience have been passed on to subsequent large rocket developments.
The actual hardware can still be seen in museums today, preserved as an engineering legacy that symbolizes the Apollo era.
