中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Performance evaluation and flow visualization of a MEMS based vaporizing liquid micro-thruster

文献类型:期刊论文

作者Cen, J. W.2; Xu, J. L.1
刊名acta astronautica
出版日期2010-08-01
卷号67期号:3-4页码:468-482
关键词Micro-satellite Vaporized liquid micro-thruster MEMS Flow pattern Instability
ISSN号0094-5765
产权排序[xu, j. l.] n china elect power univ, beijing key lab new & renewable energy, beijing 102206, peoples r china; [cen, j. w.] chinese acad sci, guangzhou inst energy convers, micro energy syst lab, guangzhou 510640, guangdong, peoples r china
通讯作者xujl@ms.giec.ac.cn
中文摘要mems micro-thruster is promising for future applications in precision formation flying missions. this paper presents performance evaluation and two-phase flow pattern visualization of a vaporized liquid micro-thruster (vlm). micro-thrust force of several milli-newtons was measured by a test rig with a lever. flow patterns in the micro-thruster chip were visualized by a high speed camera bonded with a microscope. we found that flow patterns influenced its specific impulse and there were several types of flow boiling patterns in the thruster chip. thrust instability was discussed as well. the results are helpful to understand flow characteristics of a vlm and improve its performance.
英文摘要mems micro-thruster is promising for future applications in precision formation flying missions. this paper presents performance evaluation and two-phase flow pattern visualization of a vaporized liquid micro-thruster (vlm). micro-thrust force of several milli-newtons was measured by a test rig with a lever. flow patterns in the micro-thruster chip were visualized by a high speed camera bonded with a microscope. we found that flow patterns influenced its specific impulse and there were several types of flow boiling patterns in the thruster chip. thrust instability was discussed as well. the results are helpful to understand flow characteristics of a vlm and improve its performance. (c) 2010 elsevier ltd. all rights reserved.
WOS标题词science & technology ; technology
学科主题engineering
类目[WOS]engineering, aerospace
研究领域[WOS]engineering
关键词[WOS]parallel microchannels ; heat-transfer ; microthruster ; design ; micropropulsion ; fabrication ; nozzles ; array
收录类别SCI
资助信息national fund for distinguished yong scholars [50825603]; national natural science foundation of china [50906092]
原文出处https://dx.doi.org/10.1016/j.actaastro.2010.04.009
语种英语
WOS记录号WOS:000279276700019
公开日期2014-12-24
源URL[http://ir.giec.ac.cn/handle/344007/8491]  
专题中国科学院广州能源研究所
作者单位1.N China Elect Power Univ, Beijing Key Lab New & Renewable Energy, Beijing 102206, Peoples R China
2.Chinese Acad Sci, Guangzhou Inst Energy Convers, Micro Energy Syst Lab, Guangzhou 510640, Guangdong, Peoples R China
推荐引用方式
GB/T 7714
Cen, J. W.,Xu, J. L.. Performance evaluation and flow visualization of a MEMS based vaporizing liquid micro-thruster[J]. acta astronautica,2010,67(3-4):468-482.
APA Cen, J. W.,&Xu, J. L..(2010).Performance evaluation and flow visualization of a MEMS based vaporizing liquid micro-thruster.acta astronautica,67(3-4),468-482.
MLA Cen, J. W.,et al."Performance evaluation and flow visualization of a MEMS based vaporizing liquid micro-thruster".acta astronautica 67.3-4(2010):468-482.

入库方式: OAI收割

来源:广州能源研究所

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