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  2. Staged combustion cycle - Wikipedia

    en.wikipedia.org/wiki/Staged_combustion_cycle

    The Russian RD-180 engine also employs a staged-combustion rocket engine cycle. Lockheed Martin began purchasing the RD-180 in circa 2000 for the Atlas III and later, the V , rockets. The purchase contract was subsequently taken over by United Launch Alliance (ULA—the Boeing/Lockheed-Martin joint venture) after 2006, and ULA continues to fly ...

  3. SpaceX Raptor - Wikipedia

    en.wikipedia.org/wiki/SpaceX_Raptor

    Raptor is a family of rocket engines developed and manufactured by SpaceX. It is the third rocket engine in history designed with a full-flow staged combustion (FFSC) fuel cycle, and the first such engine to power a vehicle in flight. [15] The engine is powered by cryogenic liquid methane and liquid oxygen, a combination known as methalox.

  4. Category : Rocket engines using full flow staged combustion cycle

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

    Pages in category "Rocket engines using full flow staged combustion cycle" The following 5 pages are in this category, out of 5 total. This list may not reflect recent changes .

  5. Stoke Space - Wikipedia

    en.wikipedia.org/wiki/Stoke_Space

    In 2023, Stoke Space had an interview with Tim Dodd (also known as The Everyday Astronaut), wherein the CEO Andy Lapsa revealed their plan to create a fully and rapidly reusable orbital rocket. [ 6 ] In the first months of 2023, Stoke Space finished the construction of Hopper1, a full-scale second stage prototype, intended to test fluid ...

  6. Category:Rocket engines by cycle - Wikipedia

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

    Category: Rocket engines by cycle. 3 languages. ... Rocket engines using full flow staged combustion cycle (5 P) G. Rocket engines using the gas-generator cycle (79 P) P.

  7. 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 ...

  8. BE-3 - Wikipedia

    en.wikipedia.org/wiki/BE-3

    The BE-3 (Blue Engine 3) is a liquid hydrogen/liquid oxygen rocket engine developed by Blue Origin. The engine began development in the early 2010s and completed acceptance testing in early 2015. The engine is being used on the New Shepard suborbital rocket, for which made its first test flight on 29 April 2015 and had its first crewed flight ...

  9. Comparison of orbital launch systems - Wikipedia

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

    The following chart shows the number of launch systems developed in each country, and broken down by operational status. Rocket variants are not distinguished; i.e., the Atlas V series is only counted once for all its configurations 401–431, 501–551, 552, and N22.