航天推进技术研究院主办
[1]晋晓伟,童 飞,马 键,等.一种用于微纳卫星的丙烷微推进系统[J].火箭推进,2012,38(01):17-21.
JIN Xiao-wei,TONG Fei,MA Jian,et al.Propane micro propulsion system used in micro and nano satellite[J].Journal of Rocket Propulsion,2012,38(01):17-21.
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JIN Xiao-wei,TONG Fei,MA Jian,et al.Propane micro propulsion system used in micro and nano satellite[J].Journal of Rocket Propulsion,2012,38(01):17-21.
一种用于微纳卫星的丙烷微推进系统
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
38
期数:
2012年01期
页码:
17-21
栏目:
研究与设计
出版日期:
2012-02-15
- Title:
- Propane micro propulsion system used in micro and nano satellite
- 文章编号:
- 1672-9374(2012)01-0017-05
- Keywords:
- liquefied gas; micro propulsion; propane; micro and nano satellite
- 分类号:
- V439-34
- 文献标志码:
- A
- 摘要:
- 介绍了一种应用于某微纳卫星的丙烷微推进系统，该推进系统利用换热模块，在不额外消耗星上电能的情况下实现“液－气”的可靠转化，利用自身的稳压模块和控制模块，系统可实现50 mN推力的快速精确控制。通过轻量化设计技术，系统总重仅2.5 kg。
- Abstract:
- A propane micro propulsion system used in a micro and nano satellite is introduced. With this system, the“liquid-gas”transformation was achieved without any extra consumption of energy on satellite by a heat exchange module. The propulsion system can realize a fast and accurate control for the thrust of 50 mN by the aid of pressure-stabilizing module and control module in the micro propulsion system. The dry mass of the system based on the miniaturization technology is only 2.5 kg.
参考文献/References:
[1]GIBBON D, PAUL M. The use of liquefied gases in small satellite propulsion systems, AIAA 2001-3246[R]. USA: AIAA, 2001.
[2]GIBBON D, WARD J. The design, development and testing of a propulsion system for the SNAP-1 nanosatellite [R/OL]. [2009-11-04]. http://www.sst1.co.uk.
[3]魏青, 薛国宇. 微小卫星液化气推进技术[J]. 上海航天, 2003(5): 47.
[4]马彦峰, 边炳秀. 液化气体推进剂在微小卫星推进系统中的应用[J]. 空间控制技术与应用, 2008(2): 60-62.
[5]毛根旺, 唐金兰. 航天器推进系统及其应用[M]. 西安: 西北工业大学出版社, 2009.
[6]JEFFREY G Reichbach, RAYMOND J Sedwick, MANUEL Martinez Sanchez. Micropropulsion system selection for precision formation flying satellites, AIAA 2001-3646[R]. USA： AIAA, 2001.
[7]SURREY. Nanosatellite applications platform [EB/OL]. [2009-11-04]. http://www.sstl.co.uk.
[8]PETE Smith, ROLAND McLellan, DAVE Gibbon. Smallsat propulsion [EB/OL]. [2009-11-04]. http://www.sstl.co.uk.
[9]韩先伟，周军，唐周强, 等. 微型推进系统技术方案研究[J].火箭推进，2005, 31(1): 1-7.
[10]林来兴. 现代小卫星的微推进系统[J]. 航天器工程, 2010 (6): 13-14.
相似文献/References:
[1]韩先伟,周军,唐周强,等.微型推进系统技术方案研究[J].火箭推进,2005,31(01):1.
Han Xianwei,Zhou Jun,Tang Zhouqiang,et al.Study of micropropulsion system technical options[J].Journal of Rocket Propulsion,2005,31(01):1.
[2]禹天福.空间化学推进技术的发展[J].火箭推进,2005,31(06):23.
Yu Tianfu.Development of space chemical propulsion technology[J].Journal of Rocket Propulsion,2005,31(01):23.
备注/Memo
收稿日期：2011-11-07；修回日期：2011-12-06
基金项目：国家航天高技术项目（2007AA70540）
作者简介：晋晓伟（1982—），男，工程师，研究领域为液体推进系统
更新日期/Last Update:
1900-01-01