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  2. Rocketdyne F-1 - Wikipedia

    en.wikipedia.org/wiki/Rocketdyne_F-1

    The F-1 engine is the most powerful single-nozzle liquid-fueled rocket engine ever flown. The M-1 rocket engine was designed to have more thrust, but it was only tested at the component level. The later developed RD-170 is much more stable, technologically more advanced , more efficient and produces more thrust, but uses four nozzles fed by a ...

  3. Comparison of orbital rocket engines - Wikipedia

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

    1 Current, Upcoming, and In-Development rocket engines. 2 Retired and canceled rocket engines. 3 See also. 4 Notes. 5 References. Toggle the table of contents.

  4. Future Launchers Preparatory Programme - Wikipedia

    en.wikipedia.org/wiki/Future_Launchers...

    The Future Launchers Preparatory Programme (FLPP) is a technology development and maturation programme of the European Space Agency (ESA). It develops technologies for the application in future European launch vehicles (launchers) and in upgrades to existing launch vehicles.

  5. SpaceX Merlin - Wikipedia

    en.wikipedia.org/wiki/SpaceX_Merlin

    The Merlin 1B rocket engine was an upgraded version of the Merlin 1A engine. The turbopump upgrades were handled by Barber-Nichols, Inc. for SpaceX. [ 10 ] It was intended for Falcon 1 launch vehicles, capable of producing 380 kN (85,000 lbf) of thrust at sea level and 420 kN (95,000 lbf) in vacuum, and performing with a specific impulse of 261 ...

  6. 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 ...

  7. Team Rocket F1 Rocket - Wikipedia

    en.wikipedia.org/wiki/Team_Rocket_F1_Rocket

    The F1 Rocket is a tandem two-seat low-wing cantilever monoplane built mainly in aluminum. [1] The Rocket has a titanium fixed conventional landing gear with a tailwheel. . Designed to be built with a range of nose-mounted engines between 235 and 350 hp (175 and 224 kW) the prototype has a Lycoming IO-540 with a three-bladed propelle

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    mail.aol.com

    Get AOL Mail for FREE! Manage your email like never before with travel, photo & document views. Personalize your inbox with themes & tabs. You've Got Mail!

  9. LauncherOne - Wikipedia

    en.wikipedia.org/wiki/LauncherOne

    LauncherOne is a two-stage air-launched vehicle using Newton engines, RP-1/LOX liquid rocket engines. The second stage was to be powered by NewtonOne, a 211 kN (47,000 lb f ) thrust engine. It was originally intended that the first stage will be powered by a scaled-up design of the same basic technology as NewtonOne, called NewtonTwo, with 211. ...