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液体氢仓库推进剂管理装置的性能绩效

Performance Gains of Propellant Management Devices for Liquid Hydrogen Depots

作者:Hartwig, J. W.; McQuillen, J. B.; Chato, D. J. 作者单位:National Aeronautics and Space Administration, Cleveland, OH. NASA John H. Glenn Research Center at Lewis Field. 加工时间:2015-08-30 信息来源:科技报告(NASA) 索取原文[24 页]
关键词:液态电池;电能利用;电能存储
摘 要:This paper presents background, experimental design, and preliminary experimental results for the liquid hydrogen bubble point tests conducted at the Cryogenic Components Cell 7 facility at the NASA Glenn Research Center in Cleveland, Ohio. The purpose of the test series was to investigate the parameters that affect liquid acquisition device (LAD) performance in a liquid hydrogen (LH2) propellant tank, to mitigate risk in the final design of the LAD for the Cryogenic Propellant Storage and Transfer Technology Demonstration Mission, and to provide insight into optimal LAD operation for future LH2 depots. Preliminary test results show an increase in performance and screen retention over the low reference LH2 bubble point value for a 325 2300 screen in three separate ways, thus improving fundamental LH2 LAD performance. By using a finer mesh screen, operating at a colder liquid temperature, and pressurizing with a noncondensible pressurant gas, a significant increase in margin is achieved in bubble point pressure for LH2 screen channel LADs.
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