Q8045871: Difference between revisions

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Q8045871
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{{Page|YF-73|Classes|Chinese cryogenic rocket engine}}
{{Page|YF-73|Classes|Chinese cryogenic rocket engine|}}

Latest revision as of 16:05, 17 February 2025




The YF-73 was China's first successful cryogenic liquid hydrogen fuel and liquid oxygen oxidizer gimballed engine. It was used on the Long March 3 H8 third stage, running on the simple gas generator cycle and with a thrust of 44.15 kilonewtons (9,930 lbf). It had four hinge mounted nozzles that gimbaled each on one axis to supply thrust vector control and was restart capable. It used cavitating flow venturis to regulate propellant flows. The gas generator also incorporated dual heat exchangers that heated hydrogen gas, and supplied helium from separate systems to pressurize the hydrogen and oxygen tanks. The engine was relatively underpowered for its task and the start up and restart procedures were unreliable. Thus, it was quickly replaced by the YF-75.

YF-73 3YF-73 3
YF-73 1YF-73 1
YF-73 2YF-73 2
    TypeSubtypeDateDescriptionNotesSource
    commonsimageYF-73 3 Commons
    commonsimageYF-73 1 Commons
    commonsimageYF-73 2 Commons