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  2. Archimedes (rocket engine) - Wikipedia

    en.wikipedia.org/wiki/Archimedes_(rocket_engine)

    Archimedes is presented as a highly reusable liquid-propellant engine using methane and liquid oxygen in an oxidizer-rich staged combustion cycle. [1] [2] There are both sea-level and vacuum variants. The engine is mostly 3D printed, [7] with some of the biggest 3D printers in the world. The rationale for the cycle change from the original gas ...

  3. YF-215 - Wikipedia

    en.wikipedia.org/wiki/YF-215

    The YF-215 is a liquid cryogenic rocket engine burning liquid methane and liquid oxygen in a full-flow staged combustion cycle. The engine is currently under development and is designed to power the super-heavy launch vehicle Long March 9.

  4. Category:Rocket engines using methane propellant - Wikipedia

    en.wikipedia.org/wiki/Category:Rocket_engines...

    Pages in category "Rocket engines using methane propellant" The following 22 pages are in this category, out of 22 total. This list may not reflect recent changes. A.

  5. SpaceX Merlin - Wikipedia

    en.wikipedia.org/wiki/SpaceX_Merlin

    Merlin is a family of rocket engines developed by SpaceX. They are currently a part of the Falcon 9 and Falcon Heavy launch vehicles, and were formerly used on the Falcon 1. Merlin engines use RP-1 and liquid oxygen as rocket propellants in a gas-generator power cycle. The Merlin engine was originally designed for sea recovery and reuse, but ...

  6. Lingyun (rocket engine) - Wikipedia

    en.wikipedia.org/wiki/Lingyun_(rocket_engine)

    Soaring above the clouds) is a gas-generator cycle rocket engine burning liquid methane and liquid oxygen under development by Jiuzhou Yunjian. History [ edit ]

  7. Orbital propellant depot - Wikipedia

    en.wikipedia.org/wiki/Orbital_propellant_depot

    For rockets and space vehicles, propellants usually take up 2/3 or more of their total mass. Large upper-stage rocket engines generally use a cryogenic fuel like liquid hydrogen and liquid oxygen (LOX) as an oxidizer because of the large specific impulse possible, but must carefully consider a problem called "boil off," or the evaporation of the cryogenic propellant.

  8. Liquid oxygen - Wikipedia

    en.wikipedia.org/wiki/Liquid_oxygen

    Liquid oxygen is the most common cryogenic liquid oxidizer propellant for spacecraft rocket applications, usually in combination with liquid hydrogen, kerosene or methane. [11] [12] Liquid oxygen was used in the first liquid fueled rocket. The World War II V-2 missile also used liquid oxygen under the name A-Stoff and Sauerstoff.

  9. RD-0169 - Wikipedia

    en.wikipedia.org/wiki/RD-0169

    'Rocket Engine 0169') is a Russian oxygen-methane fueled rocket engine being developed by KBKhA. Liquefied natural gas ( methane ) is used as fuel, while liquid oxygen is used as an oxidizer. Designed for use in reusable launch vehicles (like Soyuz-7 ).

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