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  2. YF-23 (rocket engine) - Wikipedia

    en.wikipedia.org/wiki/YF-23_(rocket_engine)

    The YF-23 is a liquid rocket vernier engine, burning N 2 O 4 and UDMH. [5] It is used in along the YF-22 to form the YF-24 and YF-25 propulsion modules. [ 3 ] [ 6 ] [ 7 ] [ 8 ]

  3. 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

  4. YF-20 - Wikipedia

    en.wikipedia.org/wiki/YF-20

    The YF-20 is a Chinese liquid-fuel rocket engine burning N 2 O 4 and UDMH in a gas generator cycle. It is a basic engine which when mounted in a four engine module forms the YF-21 . The high altitude variation is known as the YF-22 is normally paired with the YF-23 vernier to form the YF-24 propulsion module for second stages.

  5. YF-215 - Wikipedia

    en.wikipedia.org/wiki/YF-215

    The YF-215 engine has been designed to power the first stage of the Long March 9 rocket, with 26 of these engines in the first stage. [1] A successful ignition test of the pre-combustion chamber and gas generator of the engine was conducted on 12 May 2023.

  6. Northrop YF-23 - Wikipedia

    en.wikipedia.org/wiki/Northrop_YF-23

    The two YF-23s flew 50 times for a total of 65.2 hours. [69] The tests demonstrated Northrop's predicted performance values for the YF-23. [57] Both designs met or exceeded all performance requirements; the YF-23 was stealthier and faster, but the YF-22 was more agile. [70] [64] A YF-22 in the foreground with a YF-23 in the background

  7. General Electric YF120 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_YF120

    The YF120 had different nozzle designs for the YF-22 and YF-23 technology demonstrator prototypes tailored to the specific airframe. The YF120 on the YF-22, registration number N22YF, was equipped with thrust vectoring nozzles. The engine for the YF-22 featured a two-dimensional thrust vectoring nozzle that could vector in the pitch direction ...

  8. YF-75 - Wikipedia

    en.wikipedia.org/wiki/YF-75

    The YF-75 is a liquid cryogenic rocket engine burning liquid hydrogen and liquid oxygen in a gas generator cycle. It is China's second generation of cryogenic propellant engine, after the YF-73 , which it replaced.

  9. YF-90 - Wikipedia

    en.wikipedia.org/wiki/YF-90

    The YF-90 is a liquid cryogenic rocket engine burning liquid hydrogen and liquid oxygen in a staged combustion cycle. It is China's first hydrogen-oxygen engine to use the staged combustion cycle and is expected to be used for the second stage of the Long March 9, which is a three-stage rocket with boosters.