Author:
Chandler Ashley,Cantwell Brian,Hubbard G.
Publisher
American Institute of Aeronautics and Astronautics
Reference20 articles.
1. Chandler,A.A.,Cantwell,B.J.,Hubbard,G.S.&Karabeyoglu,A.ATwo-Stage,SinglePortHybridPropulsionSystemfora Mars Ascent Vehicle, AIAA 2010-6635, 46th Joint Propulsion Conference, Nashville, July 2010.
2. Karabeyoglu, A. Mixtures of Nitrous Oxide, Carbon Dioxide and Oxygen as Oxidizers for Mars Applications. AIAA 2010-6712. 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Nashville, TN. July 2010.
3. Hybrid rocket engines: The benefits and prospects
4. Morley,T.,Budnik,F.,MacKenzie,R.,andFaehling,N.MarsExpressNavigationforBeagle2SeparationandMarsOrbit Insertion. Proceedings of the 18th International Symposium on Space Flight Dynamics (ESA SP-548). October 2004, Munich, Germany, p.189-194.
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