Measurement and calculation research of infrared radiation for solid rocket motor plume

Ding Qiang Zhu; Xiao Ying Zhang; Hong Jun Xiang; Guo Biao Cai; Zhen Peng Zhang; An Hua Shi; Jie Huang

Measurement and calculation research of infrared radiation for solid rocket motor plume

Ding Qiang Zhu^*
, Xiao Ying Zhang
, Hong Jun Xiang
, Guo Biao Cai
, Zhen Peng Zhang
, An Hua Shi
, Jie Huang

^*Corresponding author for this work

School of Astronautics

South China University of Technology
Beihang University
China Aerodynamics Research and Development Center

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

7 Scopus citations

Abstract

The measurement scheme, instruments, analysis and result of infrared radiation from scaled rocket motor plume are introduced in this paper. Also plume flow-field and infrared of non-aluminiferous propellant are calculated. Pressure of combustion chamber, infrared radiation intensity and flow filed of plume are measured in tests, conditions cover two environments where pressure is 90 kPa and 5 kPa, three infrared radiation measurement directions at 60°, 90° and 120° with plume. In this paper, pressure of combustion chamber, the images of plumes, infrared radiation intensities of plume at 2.7μm band 4.3μm band are given. Also the calculated result of plume flow field and infrared radiation are given. The experiment results certify the property of calculation method.

Original language	English
Pages (from-to)	255-259
Number of pages	5
Journal	Yuhang Xuebao/Journal of Astronautics
Volume	29
Issue number	1
State	Published - Jan 2008

Keywords

Flow filed
Infrared radiation
Measurement
Numerical calculation
Plume
Scaled rocket motor

Cite this

@article{f927ccc4e3354a7d8842f8e5c66b7a68,

title = "Measurement and calculation research of infrared radiation for solid rocket motor plume",

abstract = "The measurement scheme, instruments, analysis and result of infrared radiation from scaled rocket motor plume are introduced in this paper. Also plume flow-field and infrared of non-aluminiferous propellant are calculated. Pressure of combustion chamber, infrared radiation intensity and flow filed of plume are measured in tests, conditions cover two environments where pressure is 90 kPa and 5 kPa, three infrared radiation measurement directions at 60°, 90° and 120° with plume. In this paper, pressure of combustion chamber, the images of plumes, infrared radiation intensities of plume at 2.7μm band 4.3μm band are given. Also the calculated result of plume flow field and infrared radiation are given. The experiment results certify the property of calculation method.",

keywords = "Flow filed, Infrared radiation, Measurement, Numerical calculation, Plume, Scaled rocket motor",

author = "Zhu, \{Ding Qiang\} and Zhang, \{Xiao Ying\} and Xiang, \{Hong Jun\} and Cai, \{Guo Biao\} and Zhang, \{Zhen Peng\} and Shi, \{An Hua\} and Jie Huang",

year = "2008",

month = jan,

language = "英语",

volume = "29",

pages = "255--259",

journal = "Yuhang Xuebao/Journal of Astronautics",

issn = "1000-1328",

publisher = "Chinese Society of Astronautics",

number = "1",

}

TY - JOUR

T1 - Measurement and calculation research of infrared radiation for solid rocket motor plume

AU - Zhu, Ding Qiang

AU - Zhang, Xiao Ying

AU - Xiang, Hong Jun

AU - Cai, Guo Biao

AU - Zhang, Zhen Peng

AU - Shi, An Hua

AU - Huang, Jie

PY - 2008/1

Y1 - 2008/1

N2 - The measurement scheme, instruments, analysis and result of infrared radiation from scaled rocket motor plume are introduced in this paper. Also plume flow-field and infrared of non-aluminiferous propellant are calculated. Pressure of combustion chamber, infrared radiation intensity and flow filed of plume are measured in tests, conditions cover two environments where pressure is 90 kPa and 5 kPa, three infrared radiation measurement directions at 60°, 90° and 120° with plume. In this paper, pressure of combustion chamber, the images of plumes, infrared radiation intensities of plume at 2.7μm band 4.3μm band are given. Also the calculated result of plume flow field and infrared radiation are given. The experiment results certify the property of calculation method.

AB - The measurement scheme, instruments, analysis and result of infrared radiation from scaled rocket motor plume are introduced in this paper. Also plume flow-field and infrared of non-aluminiferous propellant are calculated. Pressure of combustion chamber, infrared radiation intensity and flow filed of plume are measured in tests, conditions cover two environments where pressure is 90 kPa and 5 kPa, three infrared radiation measurement directions at 60°, 90° and 120° with plume. In this paper, pressure of combustion chamber, the images of plumes, infrared radiation intensities of plume at 2.7μm band 4.3μm band are given. Also the calculated result of plume flow field and infrared radiation are given. The experiment results certify the property of calculation method.

KW - Flow filed

KW - Infrared radiation

KW - Measurement

KW - Numerical calculation

KW - Plume

KW - Scaled rocket motor

UR - https://www.scopus.com/pages/publications/56849087889

M3 - 文章

AN - SCOPUS:56849087889

SN - 1000-1328

VL - 29

SP - 255

EP - 259

JO - Yuhang Xuebao/Journal of Astronautics

JF - Yuhang Xuebao/Journal of Astronautics

IS - 1

ER -

Measurement and calculation research of infrared radiation for solid rocket motor plume

Abstract

Keywords

Other files and links

Fingerprint

Cite this