An Optimization Design Method for Thermal Control of Satellite Propulsion Subsystem-Reference-Cited by-同舟云学术

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An Optimization Design Method for Thermal Control of Satellite Propulsion Subsystem

Published:2017 Issue:6 Volume:37 Page:748
ISSN:0254-6124
Container-title:Chinese Journal of Space Science
language:
Short-container-title:kjkxxb

Author:

ZHOU Yangeng,ZHOU Xiujuan,ZHANG Yu,ZHAO Jizhe,WU Zishuai,GUI Lijia,HU Xiaokang

Publisher

National Space Science Center, Chinese Academy of Sciences

Subject

General Medicine

Reference10 articles.

1. MA Wei, XUAN Yimin, HAN Yuge. Thermal design and infrared characteristics of the satellite[J]. Spacecr. Eng., 2009, 18(2):48-54

2. MIN Guirong. Satellite Thermal Control Technology[M]. Beijing:China Astronautics Publishing House, 1991

3. CHEN Jianxin, LIU Weiqiang. Research on thermal analysis for some remote sensing satellite[J]. Aerosp. Shanghai, 2011, 28(3):46-49

4. HOU Zengqi, HU Jin'gang. Spacecraft Thermal Control Techniques——Principles and Application[M]. Beijing:China Science and Technology Press, 2007

5. LI Guoqiang. Discuss about system and robust design of spacecraft thermal control[J]. Spacecr. Eng., 2013, 22(5):52-55

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