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微小卫星贮箱内两相流界面变形定位及控制管理
Alternative TitleINVESTIGATION OF TWO-PHASE FLOW INTERFACE DEFORMATION AND PROPELLANT MANAGEMENT IN TANK OF MICROSATELLITE
李章国; 刘秋生; 侯辉; 魏青; 郭尚群
Source Publication工程热物理学报
2010-04-15
Volume31Issue:4Pages:606-608
ISSN0253-231X
Abstract液化气推进技术是微小伴随卫星在轨飞行采用的一种新型推进技术. 微小伴星空间调姿、变轨过程需精确的推力控制, 因此必须了解卫星推进系统中推进剂的形位分布. 本文理论分析了空间微重力环境下液化气推进剂气/液界面的形位分布及变化, 并通过落塔实验验证了微重力环境下有效控制液体推进剂的管理方法.
Keyword气/液两相界面 液化气推进 微小伴随卫星 数值模拟 落塔实验
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Indexed ByEI ; CSCD
Language中文
Funding Organization国家重大自然科学基金资助项目(No.50890182) ; 国家自然科学基金资助项目(No.10772185)
CSCD IDCSCD:3911437
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Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/44064
Collection国家微重力实验室
Corresponding Author李章国
Recommended Citation
GB/T 7714
李章国,刘秋生,侯辉,等. 微小卫星贮箱内两相流界面变形定位及控制管理[J]. 工程热物理学报,2010,31(4):606-608.
APA 李章国,刘秋生,侯辉,魏青,&郭尚群.(2010).微小卫星贮箱内两相流界面变形定位及控制管理.工程热物理学报,31(4),606-608.
MLA 李章国,et al."微小卫星贮箱内两相流界面变形定位及控制管理".工程热物理学报 31.4(2010):606-608.
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