2021
DOI: 10.1016/j.actaastro.2021.01.046
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An experimental study on the spray characteristics of splash platelet injector

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Cited by 3 publications
(1 citation statement)
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“…For example, when the rocket engine is fired, it can ensure that the propellant flow in the pipeline rapidly changes from the gas phase to the liquid phase [3]. The chilling determines the spray characteristics of the engine injector and directly affects the engine starting process [4]. During the chill-down process, the temperature of the pipeline system drops sharply to obtain the chilling, and the cryogenic propellant completes the filling of the pipeline and establishes steady flow.…”
Section: Introductionmentioning
confidence: 99%
“…For example, when the rocket engine is fired, it can ensure that the propellant flow in the pipeline rapidly changes from the gas phase to the liquid phase [3]. The chilling determines the spray characteristics of the engine injector and directly affects the engine starting process [4]. During the chill-down process, the temperature of the pipeline system drops sharply to obtain the chilling, and the cryogenic propellant completes the filling of the pipeline and establishes steady flow.…”
Section: Introductionmentioning
confidence: 99%