Design of a combined attitude and thermal control system for small satellites based on mechanically-pumped fluid loop

被引：0
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作者：
Geng, Yunhai [1 ]
Shan, Xiaowei [1 ]
Chen, Xueqin [1 ]
Zhang, Shijie [1 ]
机构：
[1] Research Center of Satellite Technology, Harbin Institute of Technology, Harbin 150001, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2012年 / 33卷 / 01期
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页码：147 / 155
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