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

Xia Siqi; Sun Peijie; Li Peng; Wang Changhuan; Wang Lei; Li Yanzhong

doi:10.3969/j.issn.0253-4339.2019.03.109

您当前的位置：

首页 >

文章列表页 >

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

更新时间：2024-07-18

- Simulation Research on Pressure Control Performance of Thermodynamic Venting System of Rocket Propellant Tank
- Journal of Refrigeration Vol. 40, Issue 3, (2019)
- 作者机构：
  
  1. 西安交通大学制冷与低温工程系
  2. 上海宇航系统工程研究所
- 作者简介：
- 基金信息：
- DOI：10.3969/j.issn.0253-4339.2019.03.109
  CLC：
- Published：2019
- 稿件说明：
移动端阅览
Xia Siqi, Sun Peijie, Li Peng, et al. Simulation Research on Pressure Control Performance of Thermodynamic Venting System of Rocket Propellant Tank[J]. Journal of refrigeration, 2019, 40(3).
DOI：

Xia Siqi, Sun Peijie, Li Peng, et al. Simulation Research on Pressure Control Performance of Thermodynamic Venting System of Rocket Propellant Tank[J]. Journal of refrigeration, 2019, 40(3). DOI： 10.3969/j.issn.0253-4339.2019.03.109.

摘要

本文介绍了低温推进剂在轨管理中热力学排气系统（thermodynamic venting system，TVS）的构成及工作原理。基于VOF模型，编写用户自定义程序考虑箱内存在的热质传递现象，采用CFD模拟贮箱内部的压力变化和温度场分布。构建的CFD模型能够较好地模拟TVS的工作特性，证明CFD研究的有效性。针对不同液体初始充灌率、节流条件等影响因素进行变工况模拟，揭示TVS的工作规律。计算TVS在微重力下的控压性能，验证其在微重力下的可行性并获得运行规律。

Abstract

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 phenomena inside the tank

and computational fluid dynamics (CFD) was applied to simulate the pressure evolution and temperature field distribution in the tank during the TVS operation. A comparison study showed that the CFD model could well simulate the characteristics of the TVS

which might verify the effectiveness of the CFD approach in analyzing TVS performance. Moreover

the variable conditions of different initial liquid filling rate

throttling ratios

and other influencing factors were simulated to reveal the working rules of the TVS. The pressure control performance of the TVS under microgravity was also calculated. The feasibility of the TVS under microgravity was verified

and its operational rules were obtained.

关键词

Keywords

references

Views

2194

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Simulation Study on Outflow Characteristics of Cryogenic Propellant during Rocket Ascent

Gravity-dependence Analysis of Cryogenic Fluid Management Techniques in Space and Experimental Scheme Suggestions

Related Author

Huang Xiaoning

Wang Lei

Mao Hongwei

Xue Liangjiang

Li Yanzhong

Wang Lei

Jia Zhouxia

Qu Miao

Related Institution

Department of Refrigeration and Cryogenic Engineering, Xi'an Jiaotong University

State Key Laboratory of Space Cryogenic Propellant Technology

Institute of Refrigeration and Cryogenic Engineering, Xi'an Jiaotong University

Science and Technology on Reliability and Environment Engineering Laboratory, Beijing Institute of Structure and Environment Engineering

Address：10/F, Yindu Mansion, 67 Fucheng Road, Haidian Dist, Beijing, China Postal code：100142
Tel：010-68711412 Email：editor@car.org.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09064830号-19 京公网安备11010802024621
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰