Flexible Ablative Thermal Protection Sizing on Inflatable Aerodynamic Decelerator for Human Mars Entry Descent and Landing
Author:
Affiliation:
1. NASA Ames Research Center
2. ELORET Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-344
Reference11 articles.
1. 3Drake,B.G.,editor.HumanExplorationofMarsDesignReferenceArchitecture5.0.s.l.:NASA-SP-2009-566,July2009.
2. Dwyer-Cianciolo, A. M., etal, "Entry, Descent and Landing Systems Analysis Study: Phase 1 Report," NASA-TM-2010-216720, July2010.
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