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| 气体注入压力激励法测量卫星液体推进剂剩余量的热力学模型 | |
| 引用本文： | 达道安,张天平,姜万顺,张志远,孟庆平,朱小兰,陈珍,霍红庆. 气体注入压力激励法测量卫星液体推进剂剩余量的热力学模型[J]. 航天器环境工程, 1998, 0(2) |
| 作者姓名： | 达道安 张天平 姜万顺 张志远 孟庆平 朱小兰 陈珍 霍红庆 |
| 作者单位： | 兰州物理研究所，兰州物理研究所，兰州物理研究所，兰州物理研究所，兰州物理研究所，兰州物理研究所，兰州物理研究所，兰州物理研究所 |
| 摘 要： | 通过对气体注入压力激励法测量卫星液体推进剂剩余量系统的详细热力学过程分析,建立了能满足实际测量需求的等温和绝热两种热力学模型,对具体测量模型的选用及相关问题进行了分析。 |
| 关 键 词： | 热力学模型 气体注入压力激励方法 液体推进剂 卫星 |
THE THERMODYNAMIC MODELS OF PSGL FOR LIQIUD PROPELLANT REMAINING MEASUREMENT ON SATELLITE |
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| Da daoan Zhang Tianping Jiang Wanshun Zhang Zhiyuan Meng Qingping Chen Zhon Zhu Xiaolan Hue Hongqing. THE THERMODYNAMIC MODELS OF PSGL FOR LIQIUD PROPELLANT REMAINING MEASUREMENT ON SATELLITE[J]. Spacecraft Environment Engineering, 1998, 0(2) | |
| Authors: | Da daoan Zhang Tianping Jiang Wanshun Zhang Zhiyuan Meng Qingping Chen Zhon Zhu Xiaolan Hue Hongqing |
| Abstract: | This paper is our theortical studies about the method of the pressure stimulated by gas injecting (PSG1),which was desiganted as the most suitable candidate applicable to the Chinese communication satellie for measuring liquid propellants remainings.Two main thermodynamical models,the isothermal model and the adiabatic model,were set up and the dominant equations corresponding to the models were derived for practical measurement usage. Some problems associated with practical operations were discussed. |
| Keywords: | PSGI Thermodynamic Model Liquid Propellant Satellite |
| 本文献已被 CNKI 等数据库收录！ | |