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  2. Rocketdyne F-1 - Wikipedia

    en.wikipedia.org/wiki/Rocketdyne_F-1

    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.

  3. Rocketdyne - Wikipedia

    en.wikipedia.org/wiki/Rocketdyne

    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.

  4. F1 engine - Wikipedia

    en.wikipedia.org/wiki/F1_engine

    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 ...

  5. RS-68 - Wikipedia

    en.wikipedia.org/wiki/RS-68

    The RS-68 (Rocket System-68) was a liquid-fuel rocket engine that used liquid hydrogen (LH 2) and liquid oxygen (LOX) as propellants in a gas-generator cycle. It was the largest hydrogen-fueled rocket engine ever flown. [3] Designed and manufactured in the United States by Rocketdyne (later Pratt & Whitney Rocketdyne and Aerojet Rocketdyne).

  6. LR105 - Wikipedia

    en.wikipedia.org/wiki/LR105

    An LR105 Atlas sustainer engine on display at the Air Zoo.. The LR105 is a liquid-fuel rocket engine that served as the sustainer engine for the Atlas rocket family. [1] [2] [3] Developed by Rocketdyne in 1957 as the S-4, [4] [5] [6] it is called a sustainer engine because it continues firing after the LR89 booster engines have been jettisoned, providing thrust during the ascent phase.

  7. Comparison of orbital rocket engines - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_orbital...

    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

  8. Formula One engines - Wikipedia

    en.wikipedia.org/wiki/Formula_One_engines

    A Cosworth DFV 3-litre V8 Formula One engine Renault 1.5 litre turbo engine. In 1966, with sports cars capable of outrunning Formula One cars thanks to much larger and more powerful engines, the FIA increased engine capacity to 3.0 L atmospheric and 1.5 L compressed engines. [27]

  9. F1 Q&A: Are there problems between drivers and the FIA? - AOL

    www.aol.com/f1-q-problems-between-drivers...

    BBC F1 correspondent Andrew Benson answers your questions following the Singapore Grand Prix.