Thermal Cycling for Development of Hybrid Fuel for a Notional Mars Ascent Vehicle-Reference-Cited by-同舟云学术

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Thermal Cycling for Development of Hybrid Fuel for a Notional Mars Ascent Vehicle

Published:2016-07-22 Issue: Volume: Page:
ISSN:
Container-title:52nd AIAA/SAE/ASEE Joint Propulsion Conference
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Author:

Farias Edgardo,Redmond Matthew,Karp Ashley C.,Shotwell Robert,Mechentel Flora S.,Story George T.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4563

Reference12 articles.

1. 3Ashley A. Chandler, (2012). An investigation of liquefying hybrid rocket fuels with applications to solar system exploration (Doctoral dissertation).Retrievedfrom https://purl.stanford.edu/bm524fh7508.

Cited by 3 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. State of Art and Current Challenges of the Paraffin-Based Hybrid Rocket Technology;AIAA Propulsion and Energy 2019 Forum;2019-08-16

2. Tubular Equivalent Regression Rate in Hybrid Rockets with Complex Geometries;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2019

3. A Hybrid Mars Ascent Vehicle Concept for Low Temperature Storage and Operation;52nd AIAA/SAE/ASEE Joint Propulsion Conference;2016-07-22

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