Hypergolic Propellant Ignition Phenomenon Associated with Two-Phase Oxidizer Flow Injection
Author:
Affiliation:
1. Space Technologies Development Office, IHI Aerospace Company, Ltd., Tomioka, Gunma 370-2398, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B35203
Reference11 articles.
1. Soak-back heating response of thruster components for steady and pulsed firing
2. ZungL. B.WhiteJ. R. “Combustion Process of Impinging Hypergolic Propellants,” NASA CR-1704, 1971.
3. Handbook of Atomization and Sprays
4. Visualization and measurements of periodic boiling in silicon microchannels
5. Test experience, 490-N high-performance (321-s specific impulse) engine
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Investigation on Suppression of Hard Start Phenomena in Hypergolic Bipropellant Engine;AIAA SCITECH 2024 Forum;2024-01-04
2. Optical visualization of hypergolic burning spray structure using blue light spectrum;Acta Astronautica;2022-04
3. Visualization of Pulse Firing Mode in Hypergolic Bipropellant Thruster;Journal of Propulsion and Power;2020-09
4. Chemical Propulsion for Outer Planet Exploration;AIAA Propulsion and Energy 2019 Forum;2019-08-16
5. Atomization and hypergolic reactions of impinging streams of monomethylhydrazine and dinitrogen tetroxide;Combustion and Flame;2017-11
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