| 球锥贮箱微重力试验研究 |
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| 引用本文： | 张景芳.球锥贮箱微重力试验研究[J].强度与环境,1996(4):37-45. |
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| 作者姓名： | 张景芳 |
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| 作者单位： | 北京强度环境研究所!100076，北京9200信箱72分箱 |
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| 摘 要： | 用落塔试验和相似准则，在较宽邦德数（Ｂ０＝１３－１００）范围内给出球锥贮箱准静态试验结果；得同重力环境下的挤出效率；对上述贮箱，还取得了较标准的敢界面产筝形状及液体完成重要位全过程的图象和时间数据。可供自旋稳定卫星在微重力环境下，管理液体推进剂参考使用。
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| 关 键 词： | 自旋稳定 卫星 微重力试验 推进剂 储箱 |
Experimental investigation of ball-cone tank under microgravity condition |
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| Zhang JingfangBeijing Institute of structure and Environment engineering.Experimental investigation of ball-cone tank under microgravity condition[J].Structure & Environment Engineering,1996(4):37-45. |
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| Authors: | Zhang JingfangBeijing Institute of structure and Environment engineering |
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| Institution: | Zhang JingfangBeijing Institute of structure and Environment engineering |
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| Abstract: | Through Drop tower test and ixmensionless similar principle. This paper gave liquid test result of peculiar to staric state its field of Band number more widened (K0= 13~ 100):gave expulsion efficiency of peculiar to fIuid rate; gave worth liquid - gas surface static equilibrium shape; gave states and tipses of liquid that have finished all reorientation. These results will be used in the liquid propellant management of spinning stabilzation satellite under microgravity environment. |
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| Keywords: | Microgravity enviroment Microgravity test Fluid management Spin stabilized satellite Propellant tank |
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