真空羽流逆流污染的理论计算

推进技术 ›› 2000, Vol. 21 ›› Issue (1): 8-11.

真空羽流逆流污染的理论计算

蔡国飙,杜军,王慧玉,朱小兰

北京航空航天大学宇航学院!北京100083;北京航空航天大学宇航学院!北京100083;北京航空航天大学宇航学院!北京100083;兰州物理研究所!甘肃兰州730000

发布日期:2021-08-15
基金资助:
国防“九五”重点预研资助项目

Theoretical computation on the contamination of vacuum plume in the backflow region

School of Astronautics, Beijing Univ of Aeronautics and Astronautics, Beijing 100083, China;School of Astronautics, Beijing Univ of Aeronautics and Astronautics, Beijing 100083, China;School of Astronautics, Beijing Univ of Aeronautics and Astronautics, Beijing 100083, China;Lanzhou Inst of Physics, Lanzhou 730000, China

Published:2021-08-15

摘要/Abstract

摘要： 针对普遍关注的羽流逆流污染问题,讨论了喷管出口背部位置受到的回流分子撞击热污染和分子沉积问题,从分子运动论和统计力学出发编制了计算程序,对不同的算例进行了计算,得到符合规律的结果,为火箭发动机设计和科学试验提供了理论依据。

关键词: 姿控火箭发动机;喷管气流;高空环境;羽流;航天器污染

Abstract: The plume contamination has several patterns with respect to different contaminational surfaces The prediction of thermal contamination and deposition due to the impingement of the molecular of the back flow region of the nozzle were discussed The program based on the theory of molecule movements and statistical mechanics was composed with analytical methods and was applied to several different conditions, with computational results in conformity with analysis in theory The purpose of this research is to provide a good foundation for the rocket engine design and scientific experiments

Key words: Attitude control rocket engine;Nozzle flow;High altitude environment;Plume;Spacecraft contamination

蔡国飙,杜军,王慧玉,朱小兰. 真空羽流逆流污染的理论计算[J]. 推进技术, 2000, 21(1): 8-11.