Ignition transient model for large aspect ratio solid rocket motors-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Ignition transient model for large aspect ratio solid rocket motors

Published:1996-07-01 Issue: Volume: Page:
ISSN:
Container-title:32nd Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Luke G.¹,Eagar M.²,Dwyer H.³

Affiliation:

1. Aerojet Propulsion, Sacramento, CA

2. United Technologies Corp., Chemical Systems Div., San Jose, CA

3. California, Univ., Davis

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-3273

Reference23 articles.

1. Starting Transient of Solid-Propellant ocket Motors with High Internal Gas Velocities

2. Caveny,L.H. "ExtensionstoAnalysisofIgnition TransientsofSegmentedRocketMotors,"NASA ContractorReport:NASA CR-150632,January 1978.

Cited by 15 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. Experimental Investigations of a Pyrotechnic Igniter;AIAA SCITECH 2022 Forum;2022-01-03

2. Study on maximum pressure rise with igniter mass in tubular grain rocket motor;SCI TECHNOL ENERG MA;2021

3. Investigation of a novel pyrogenic pulser in a laboratory motor;Chinese Journal of Aeronautics;2020-01

4. A Model for Igniter Mass Flow Rate History Evaluation for Solid Rocket Motors;International Journal of Aerospace Engineering;2019-12-31

5. Parametric Study on Solid Rocket Motor Ignition Transient and Pressure Oscillations Onset;Journal of Propulsion and Power;2015-07

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