Numerical Investigation of Hybrid Rocket Combustion Chamber Transient Behavior-Reference-Cited by-同舟云学术

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Numerical Investigation of Hybrid Rocket Combustion Chamber Transient Behavior

Published:2013-07-12 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
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Author:

Barato Francesco¹,Faenza Martina¹,Pavarin Daniele¹,Bettella Alberto¹,Bellomo Nicolas¹

Affiliation:

1. University of Padua

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-3897

Reference26 articles.

1. J. Arves, M. Gnau, K. Joiner, D.Kearney, C. McNeal, M. Murbach, "Overviewof The Hybrid SoundingRocket (HYSR) Project", AIAA2003-5199.

2. D. A. Kearney, K. F. Joiner,M.P. Gnau, M. A. Casemore, "Improvement to theMarketabilityofHybrid Propulsion Technologies", inProceedingsoftheAIAASpaceConference, pp.1674-1688,September 2007, AIAAPaper2007-6144.

Cited by 1 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. CFD Simulations of Self-pressurized Nitrous Oxide Hybrid Rocket Motors;2018 Joint Propulsion Conference;2018-07-08

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