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This is a big boy. Built by Rocketdyne for the mighty F-1 engines of the Apollo Saturn V.

From NASA and Apollo 11 Space: “The gas generator is one of the first parts designed on a new engine because it is a crucial part of determining a rocket engine’s size. It’s like a “rocket motor” inside a rocket motor. It’s an internal combustion engine that drives the whole F-1 engine. The Saturn V’s F-1 is a gas generator-cycle rocket engine produced in the United States by Rocketdyne in the late 1950s and was used in the 1960s and early 1970s.

The F-1 engine continues to be the most powerful single combustion chamber liquid-propellant rocket engine ever developed. The most striking aspect is the sheer power when the gas generator ignites and creates approximately 31,000 pounds of force, continuously. When the original F-1 engine lit up, the gas generator powered the giant turbomachinery that pumped about three tons of propellant each second into the thrust chamber and accelerated through the nozzle, producing the incredible 1.5 million pounds of thrust. The Saturn V’s gas generator was used to drive a turbine, which drove separate fuel and oxygen pumps, each feeding the thrust chamber assembly.

The turbopump is required to resist temperatures ranging from input gas at 1,500 °F (820 °C) to liquid oxygen at −300 °F (−184 °C). So, fuel was used to lubricate and cool the turbine bearings. This large amount of fuel keeps the gas generator a little bit cooler, so it doesn’t melt. It keeps it about 800 degrees Celsius.”

Here is a video of just the gas generator firing in a 2013 revival by NASA.

This unit tags, both rated 1200 PSI
• Dual Ball Valve, Part: EO R62819
• Gas Gen Assy, Part: EWR 285763

An artifact in the Future Ventures’ 🚀 Space Collection.

4 responses to “Saturn V F-1 Engine Gas Generator Assembly”

  1. For comp: a high power rifle bullet creates chamber pressure of ~60,000 PSI (413+ MPa) on detonation for a very small fraction of a second, so this gas generator creates about 1/2 that continuously during main engine burn…should probably be called a "controlled explosion generator." Gimbals and combustion chambers are cool, but the turbo pumps are IMO the most amazing components of liquid fuel rocket design… Very amazing addition to the collection!

  2. ps: from wikipedia > "In mid-1935 Wernher von Braun initiated a fuel pump project at the southwest German firm Klein, Schanzlin & Becker that was experienced in building large fire-fighting pumps. The V-2 rocket design used hydrogen peroxide decomposed through a Walter steam generator to power the uncontrolled turbopump produced at the Heinkel plant at Jenbach, so V-2 turbopumps and combustion chamber were tested and matched to prevent the pump from overpressurizing the chamber…. Turbopumps have a reputation for being extremely hard to design to get optimal performance. Whereas a well engineered and debugged pump can manage 70–90% efficiency, figures less than half that are not uncommon. Low efficiency may be acceptable in some applications, but in rocketry this is a severe problem. Turbopumps in rockets are important and problematic enough that launch vehicles using one have been caustically described as a "turbopump with a rocket attached"–up to 55% of the total cost has been ascribed to this area."

  3. [https://www.flickr.com/photos/stephenbove] very interesting. 55%! it is the marvelous part of the RL-10, using the phase change from the heat from combustion to power the fuel and oxidizer pumps.
    Expander_rocket_cycle

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