Development of a small sounding hybrid rocket with a swirling-oxidizer-type engine-Reference-Cited by-同舟云学术

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Development of a small sounding hybrid rocket with a swirling-oxidizer-type engine

Published:2001-07-08 Issue: Volume: Page:
ISSN:
Container-title:37th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Yuasa Saburo¹,Yamamoto Kengo¹,Hachiya Hitoshi¹,Kitagawa Koki¹,Oowada Youichi²

Affiliation:

1. Tokyo Metropolitan Inst. of Technology, Japan

2. National Space Development Agency, Kakuda Propulsion Center, Japan

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-3537

Reference9 articles.

1. [5]Sutton, G. P. "Rocket Propulsion Elements," 6th Edition,John Wiley & Sons, 1992,pp.502-522.

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