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  2. Rocketdyne F-1 - Wikipedia

    en.wikipedia.org/wiki/Rocketdyne_F-1

    How NASA brought the monstrous F-1 “moon rocketengine back to life; New F-1B rocket engine upgrades Apollo-era design with 1.8M lbs of thrust; MSFC History office F-1 Fact sheet; Anthony Young Collection, The University of Alabama in Huntsville Archives and Special Collections Research material on the development of the F-1 engine. U.S ...

  3. Liquid rocket booster - Wikipedia

    en.wikipedia.org/wiki/Liquid_rocket_booster

    In 2013, it was reported that in comparison to the F-1 engine, the F-1B engine was to have improved efficiency, be more cost effective and have fewer engine parts. [4] Each F-1B was to produce 1,800,000 lbf (8.0 MN) of thrust at sea level, an increase over the 1,550,000 lbf (6.9 MN) of thrust of the initial F-1 engine.

  4. P160C - Wikipedia

    en.wikipedia.org/wiki/P160C

    The P160C is a solid-fuel rocket engine designed for use as the first stage of the Vega-E and as the boosters of the Ariane 6 Block 2 launch vehicles. The solid rocket motors were developed by Europropulsion, a joint venture of Avio and ArianeGroup, for the European Space Agency. The "C" in the name signifies its "Common" use across these ...

  5. Northrop Grumman taps Firefly Aerospace to upgrade its ... - AOL

    www.aol.com/news/northrop-grumman-taps-firefly...

    Chalk one up for the American broomsticks. Due to the continuing war in Ukraine, Russia halted all sales of its rocket engines to the United States in March this year. "Through our collaboration ...

  6. 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

  7. Fastrac (rocket engine) - Wikipedia

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

    NASA started full-engine, hot-fire testing in March, 1999, with a 20 second test to demonstrate the complete engine system. [12] The engine was tested at full power for 155 seconds on July 1, 1999. [13] A total of 85 tests were scheduled for the rest of 1999. As of 2000, 48 tests had been conducted on three engines using three test stands. [8]

  8. 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.

  9. 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).

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