Feasibility of a single port Hybrid Propulsion system for a Mars Ascent Vehicle

Author:

Chandler Ashley A.,Cantwell Brian J.,Scott Hubbard G.,Karabeyoglu Arif

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference11 articles.

1. Committee on the Planetary Science Decadal Survey, National Research Council, Vision and Voyages for Planetary Science in the Decade 2013–2022, The National Academies Press, Washington DC, 2011.

2. S. Hayati, Technology Planning for Next Decade Missions, MEPAG, Brown University Providence, 2009.

3. D. Stephenson, Mars ascent vehicle: concept development, in: Proceedings of the 38th Joint Propulsion Conference, Indianapolis Indiana, 7–10 July 2002, AIAA 2002-4318.

4. A.A. Chandler, J. Cantwell, G.S. Hubbard, Karabeyoglu, A two-stage, single port hybrid propulsion system for a Mars ascent vehicle, in: Proceedings of the 46th Joint Propulsion Conference, Nashville, TN, July 2010, AIAA 2010-6635.

5. B. Cantwell, A. Karabeyoglu, D. Altman, Recent advances in hybrid propulsion, in: Proceedings of the Eigth ISICP, Cape Town, South Africa, November 2–6, 2009.

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