|Table of Contents|

esearch on plume flow of space thrusters(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2014年06期
Page:
46-50
Research Field:
研究与设计
Publishing date:

Info

Title:
esearch on plume flow of space thrusters
Author(s):
GUO Jing;  KONG Fan-chao;  HU Xu-kun
Beijing Institute of Aerospace Testing Technology, Beijing 100074, China
Keywords:
-
PACS:
V439-34
DOI:
-
Abstract:
The necessity of plume flow research of space thrusters is introduced. At the same time, plume test and numerical simulation methods which are the two valid ways to research space engine's plume characters are elaborated. Then the key technique and development of plume test are summarized. Afterwards, the compositions, vacuum pumping methods, main specifications and characteristics of representative plume test beds including J2-A chamber and CHAFF-IV facility of USA, CCG chamber and STG chamber of European, KM space simulators and PES chamber of China are summarized. Finally, development of the numerical simulation technology related to plume test on ground is introduced by overviewing numerical models of plume, focusing on DSMC method and its software, presenting plume computational methods of high density plume and electrical propulsion thruster plume. The technology of test and numerical simulation of space thruster plume is helpful to research the plume of space

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