Effects of propellant heat groove configuration on solar thermal propulsion performance

Jie Yang; Li Jun Yang

Effects of propellant heat groove configuration on solar thermal propulsion performance

Jie Yang^*
, Li Jun Yang

^*此作品的通讯作者

宇航学院

Beihang University

科研成果: 期刊稿件 › 文章 › 同行评审

4 引用（Scopus）

摘要

A detailed study of solar thermal propulsion (STP) performance was made using numerical simulation method by changing spiral groove parameter in this paper. The optimum design parameter was gotten according to analysis on STP's thrust, specific impulse and mass flow rate. Advantage and disadvantage of performances were also compared between single and double spiral groove STP. The conclusion provides a guidance to design of STP thrust chamber spiral groove.

源语言	英语
页（从-至）	1156-1162
页数	7
期刊	Hangkong Dongli Xuebao/Journal of Aerospace Power
卷	25
期	5
出版状态	已出版 - 5月 2010

其它文件与链接

链接到 Scopus 的出版物

引用此

@article{f29a1fd733fa42ab8ccc8d28c17b6d80,

title = "Effects of propellant heat groove configuration on solar thermal propulsion performance",

abstract = "A detailed study of solar thermal propulsion (STP) performance was made using numerical simulation method by changing spiral groove parameter in this paper. The optimum design parameter was gotten according to analysis on STP's thrust, specific impulse and mass flow rate. Advantage and disadvantage of performances were also compared between single and double spiral groove STP. The conclusion provides a guidance to design of STP thrust chamber spiral groove.",

keywords = "Convection heat transfer, Solar thermal propulsion(STP), Specific impulse, Thrust, Thruster room",

author = "Jie Yang and Yang, \{Li Jun\}",

year = "2010",

month = may,

language = "英语",

volume = "25",

pages = "1156--1162",

journal = "Hangkong Dongli Xuebao/Journal of Aerospace Power",

issn = "1000-8055",

publisher = "BUAA Press",

number = "5",

}

TY - JOUR

T1 - Effects of propellant heat groove configuration on solar thermal propulsion performance

AU - Yang, Jie

AU - Yang, Li Jun

PY - 2010/5

Y1 - 2010/5

N2 - A detailed study of solar thermal propulsion (STP) performance was made using numerical simulation method by changing spiral groove parameter in this paper. The optimum design parameter was gotten according to analysis on STP's thrust, specific impulse and mass flow rate. Advantage and disadvantage of performances were also compared between single and double spiral groove STP. The conclusion provides a guidance to design of STP thrust chamber spiral groove.

AB - A detailed study of solar thermal propulsion (STP) performance was made using numerical simulation method by changing spiral groove parameter in this paper. The optimum design parameter was gotten according to analysis on STP's thrust, specific impulse and mass flow rate. Advantage and disadvantage of performances were also compared between single and double spiral groove STP. The conclusion provides a guidance to design of STP thrust chamber spiral groove.

KW - Convection heat transfer

KW - Solar thermal propulsion(STP)

KW - Specific impulse

KW - Thrust

KW - Thruster room

UR - https://www.scopus.com/pages/publications/77953643532

M3 - 文章

AN - SCOPUS:77953643532

SN - 1000-8055

VL - 25

SP - 1156

EP - 1162

JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

JF - Hangkong Dongli Xuebao/Journal of Aerospace Power

IS - 5

ER -

Effects of propellant heat groove configuration on solar thermal propulsion performance

摘要

其它文件与链接

学术指纹

引用此