航天推进技术研究院主办
[1]袁 磊,王 申,连仁志,等.一种推进剂剩余量在轨测量方法研究[J].火箭推进,2013,39(05):75-81.
YUAN Lei,WANG Shen,LIAN Ren-zhi,et al.On-board gauging method of remaining propellant[J].Journal of Rocket Propulsion,2013,39(05):75-81.
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YUAN Lei,WANG Shen,LIAN Ren-zhi,et al.On-board gauging method of remaining propellant[J].Journal of Rocket Propulsion,2013,39(05):75-81.
一种推进剂剩余量在轨测量方法研究
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
39
期数:
2013年05期
页码:
75-81
栏目:
工艺与材料
出版日期:
2013-10-31
- Title:
- On-board gauging method of remaining propellant
- 文章编号:
- 1672-9374(2013)05-0087-05
- 分类号:
- V423.4-34
- 文献标志码:
- A
- 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。
- Abstract:
- For a Chinese satellite, an on-board gauging method of remaining propellant was designed, 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%.
参考文献/References:
[1]达道安, 张天平． 在轨卫星液体推进剂测量技术评述[J]．推进技术, 1997, 18(4): 89-94.
[2]YENDLER B. Review of propellant gauging methods, AIAA 2006-939[R]. US: AIAA, 2006.
[3]AMBROSE J, YENDLER B, COLLICOTT S H. Modeling to evaluate a spacecraft propellant gauging system[J]. Journal of Spacecraft and Rockets, 2000, 37(6): 833-835.
[4]LAL A, RAGHUNANDAN B N. Uncertainty analysis of propellant gauging system for spacecraft[J]. Journal of Spacecraft and Rockets, 2005, 42(5): 943-946.
[5]HANSMAN R J, Jr. Fundamental limitations on low gravity fluid gauging technologies imposed by orbital mission requirements, AIAA 88-3402[R]. US: AIAA, 1988.
[6]CHOBOLOV M V, PUROHIT G P. Low gravity propellant gauging system for accurate prediction of spacecraft end-of-life[J]. Journal of Spacecraft and Rockets, 1993, 30(1): 92-101.
[7]达道安，张天平．一种适合我国在轨卫星液体推进剂剩余量测量的技术方案[J]． 推进技术, 1997, 18(6): 98-102.
[8]张天平, 达道安． 卫星液体推进剂剩余量测量的热力学模型及其应用[J]． 中国空间科学技术, 1998, 18(6): 52-57.
[9]张天平, 达道安, 李育红, 等． 卫星推进剂剩余量测量技术地面试验研究[J]． 上海航天, 2000 (4): 34-39.
[10]傅娟． 微重力条件下贮箱液体推进剂量自主检测方法研究[D]． 长沙: 国防科学技术大学, 2010.
[11]魏延明, 宋涛, 梁军强． 基于并联贮箱结构的卫星推进剂剩余量测量方法[J]． 空间控制技术与应用, 2010, 8(4): 25-30.
[12]宋涛, 马云华, 林长杰, 等． 环境对气体注入法测量剩余推进剂的影响分析[J]． 航天器工程, 2011, 7(4): 147-151.
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备注/Memo
收稿日期：2013-01-25；修回日期：2013-05-14
基金项目：中国航天科技集团公司支撑项目（2009JY02）
作者简介：袁磊（1977—），男，研究员，研究领域为空间推进系统工程
更新日期/Last Update:
1900-01-01