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气球落舱内试验平台的高微重力水平分析

ANALYSIS OF HIGH QUALITY MICROGRAVITY ABOUT BALLOON-RELEASED TEST PLATFORM

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【作者】 高云峰王麟华

【Author】 GAO Yunfeng, WANG Linghua (Department of Engineering Mechanics, Tsinghua University, Beijing 100084) (Center for Space Science and Applied Research, The Chinese Academy of Sciences, 100080)

【机构】 清华大学工程力学系!北京100084中国科学院空间科学与应用研究中心

【摘要】 研究了一种新型高微重力水平气球落舱内试验平台的动力特性,考虑了稀薄气体的影响,建立了落舱及平台的动力学方程.通过数值计算获得了平台微重力水平与落舱控制精度、平台与落舱的分离时刻、真空舱内真空度的关系.

【Abstract】 Some dynamic characters of a new balloon-released test platform in capsule with high quality microgravity are studied in this paper. The dynamics equations are obtained by considering the effect of the rarefied gas and the free molecular flow in vacuum chamber. The relationship between microgravity and control precision, detach time of platform from capsule, and pressure of the vacuum chamber are obtained by simulation.

【基金】 国家自然科学基金资助项目!(49784004)
  • 【文献出处】 空间科学学报 ,Chinese Journal of Space Science , 编辑部邮箱 ,2001年02期
  • 【分类号】P172
  • 【被引频次】1
  • 【下载频次】75
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