Design and Development of a 100km Nitrous Oxide/Paraffin Hybrid Rocket Vehicle-Reference-Cited by-同舟云学术

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Design and Development of a 100km Nitrous Oxide/Paraffin Hybrid Rocket Vehicle

Published:2007-07-08 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Dyer Jonny,Doran Eric,Dunn Zach,Lohner Kevin,Bayart Cedric,Sadhwani Andy,Zilliac Greg,Cantwel Brian,Karabeyoglu Arif

Publisher

American Institute of Aeronautics and Astronautics

Reference4 articles.

1. Combustion of Liquefying Hybrid Propellants: Part 1, General Theory

2. 2Arves,J.,Gnau,M.,Joiner,K.,Kearney,D.,McNeal,C.,andMurbach,M."OVERVIEWOFTHEHYBRIDSOUNDING ROCKET (HYSR) PROJECT," Joint Propulsion Conference and Exhibit, July 2003.

3. 3Doran, E., Dyer, J., Lohner, K., and Dunn, Z. "Nitrous Oxide Hybrid Rocket Motor Fuel Regression Rate Characterization," Joint Propulsion Conference and Exhibit, July 2007.

4. 4Dunn, Z., Dyer, J., Lohner, K., Doran, E., Bayart, C., Sadhwani, A., Karabeyoglu, A., and Cantwell, B. "Test Facility Development for the 15,000 Ib Thrust Peregrine Hybrid Sounding Rocket," Joint Propulsion Conference and Exhibit, July 2007.

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