摘要
用落塔试验和相似准则．在较宽邦德数（B。=13～100）范围内给出球锥贮箱准静态试验结果；得到该贮箱在微重力环境下的挤出效率；对上述贮箱，还取得了较标准的液气界面静平衡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。
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.
出处
《强度与环境》
北大核心
1996年第4期37-45,共9页
Structure & Environment Engineering
关键词
自旋稳定
卫星
微重力试验
推进剂
储箱
Microgravity enviroment, Microgravity test, Fluid management, Spin stabilized satellite, Propellant tank
