Simulation Study on Outflow Characteristics of Cryogenic Propellant during Rocket Ascent

Simulation Study on Outflow Characteristics of Cryogenic Propellant during Rocket Ascent

At the rocket launching stage, it is very important to supply sufficient and vapor-free liquid propellant to maintain the functioning of the main engine. Considering the working characteristics and design requirements of the outflow device of the cryogenic propellant tank, a computational fluid dyna...

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Bibliographic Details
Main Authors: Huang Xiaoning, Wang Lei, Mao Hongwei, Xue Liangjiang, Li Yanzhong
Format: Article
Language:zho
Published: Journal of Refrigeration Magazines Agency Co., Ltd. 2020-01-01
Series:Zhileng xuebao
Subjects:
rocket launch
cryogenic propellant
outflow device
surface collapse
CFD simulation
Online Access:http://www.zhilengxuebao.com/thesisDetails#10.3969/j.issn.0253-4339.2020.04.136

Internet

http://www.zhilengxuebao.com/thesisDetails#10.3969/j.issn.0253-4339.2020.04.136

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