Effects of swirling oxidizer flow on fuel regression rate of hybrid rockets-Reference-Cited by-同舟云学术

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Effects of swirling oxidizer flow on fuel regression rate of hybrid rockets

Published:1999-06-20 Issue: Volume: Page:
ISSN:
Container-title:35th Joint Propulsion Conference and Exhibit
language:
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Author:

Takashi Tamura¹,Yuasa Saburo¹,Yamamoto Kengo¹

Affiliation:

1. Tokyo Metropolitan Inst. of Technology, Japan

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-2323

Reference2 articles.

1. [l] Sutton, G. P. "Rocket Propulsion Elements," JohnWiley & Sons,New York,1996,pp.261-271.

2. Yuasa,S.etal."A Techniquefor Improvingthe Performanceof Hybrid RocketEngines,"AIAA Paper99-2322,1999

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