A new satellite hydrogen‐oxygen microthruster combustion chamber: An experimental and numerical study

Author:

Chen Qiumin1ORCID,Wang Xiang2,Gong Jingsong2,Xu Shengli2

Affiliation:

1. State Key Laboratory of Explosion Science and Technology Beijing Institute of Technology Beijing China

2. School of Aerospace Engineering Tsinghua University Beijing China

Publisher

Hindawi Limited

Subject

Energy Engineering and Power Technology,Fuel Technology,Nuclear Energy and Engineering,Renewable Energy, Sustainability and the Environment

Reference24 articles.

1. PlattD.A monopropellant Milli‐Newton thruster system for attitude control of Nanosatellites Paper presented at: Annual USU Conference on Small Satellites; 2002:5–9.

2. Cold gas propulsion microthruster for feed gas utilization in micro satellites

3. JamesK BodnarM FreedmanM.Hydros: high performance water‐electrolysis propulsion for cubesats and microsats. Paper presented at: AIAA/Usu Conference on Small Satellite 2018 North Logan Utah; 2018.

4. Microscale combustion: Technology development and fundamental research

5. Development and test of a miniature hydrogen peroxide monopropellant thruster;Scharlemann C;AIAA,2006

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3