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

^*Corresponding author for this work

School of Astronautics

Beihang University

Research output: Contribution to journal › Article › peer-review

4 Scopus citations

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.

Original language	English
Pages (from-to)	1156-1162
Number of pages	7
Journal	Hangkong Dongli Xuebao/Journal of Aerospace Power
Volume	25
Issue number	5
State	Published - May 2010

Keywords

Convection heat transfer
Solar thermal propulsion(STP)
Specific impulse
Thrust
Thruster room

Cite this

@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",

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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

Abstract

Keywords

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