| 一种推进剂剩余量在轨测量方法研究 |
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| 引用本文： | 袁磊,王申,连仁志,刘涛.一种推进剂剩余量在轨测量方法研究[J].火箭推进,2013(5):87-91. |
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| 作者姓名： | 袁磊 王申 连仁志 刘涛 |
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| 作者单位： | 上海空间推进研究所,上海201112 |
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| 基金项目： | 基金项目：中国航天科技集团公司支撑项目（2009JY02） |
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| 摘 要： | 对我国某卫星平台气体注入压力激励推进剂剩余量测量方法进行了研究,建立了剩余量计算模型,开发了计算软件,开展了地面试验,结果表明,测量误差在-0.68%~0.66%范围内,达到了较高的测量精度。
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| 关 键 词： | 推进系统 剩余推进剂 推进剂在轨测量 |
On-board gauging method of remaining propellant |
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| YUAN Lei,WANG Shen,LIAN Ren-zhi,LIU Tao.On-board gauging method of remaining propellant[J].Journal of Rocket Propulsion,2013(5):87-91. |
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| Authors: | YUAN Lei WANG Shen LIAN Ren-zhi LIU Tao |
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| Institution: | ( Shanghai Institute of Space Propulsion, Shanghai 201112, China) |
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| Abstract: | For a Chinese satellite, an on-board gauging method of remaining propellant was de- signed, the mathematical model was established, the software for calculating remaining propellant was developed, and some ground tests were carried out. The test results show that the designed on-board gauging method of remaining propellant has adequate accuracy for engineering application and its error is within the ＇range of-0.68%~0.66%. |
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| Keywords: | propulsion system remaining propellant on-board propellant gauging |
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