A Comparison of Preliminary Design Concepts for Liquid, Solid and Hybrid Propelled Mars Ascent Vehicles Using In-Situ Propellants

Details A Comparison of Preliminary Design Concepts for Liquid, Solid and Hybrid Propelled Mars Ascent Vehicles Using In-Situ Propellants A Comparison of Preliminary Design Concepts for Liquid, Solid and Hybrid Propelled Mars Ascent Vehicles Using In-Situ Propellants

Jan 2000

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2000heds.conf..169c&link_type=article

Third Annual HEDS-UP Forum, Human Exploration and Development of Space-University Partners (HEDS-UP). Proceedings of the confere

Physics

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