Simulation Research on Pressure Control Performance of Thermodynamic Venting System of Rocket Propellant Tank

Simulation Research on Pressure Control Performance of Thermodynamic Venting System of Rocket Propellant Tank

This article described the composition and working principle of the thermodynamic venting system (TVS) for the in-orbit management of cryogenic propellants. Based on the volume of fluid (VOF) multiphase model, a user-defined function (UDF) was compiled to consider the heat and mass transfer phenomen...

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Bibliographic Details
Main Authors: Xia Siqi, Sun Peijie, Li Peng, Wang Changhuan, Wang Lei, Li Yanzhong
Format: Article
Language:zho
Published: Journal of Refrigeration Magazines Agency Co., Ltd. 2019-01-01
Series:Zhileng xuebao
Subjects:
cryogenic propellant
pressure control
CFD simulation
microgravity
Online Access:http://www.zhilengxuebao.com/thesisDetails#10.3969/j.issn.0253-4339.2019.03.109
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