Probabilistic Sizing Demonstration of a Flexible Thermal Protection System for a Hypersonic Inflatable Aerodynamic Decelerator
2015
36 pages
Report
No indication
English
Unmanned Spacecraft , Manned Spacecraft , Astronomy & Astrophysics , Extraterrestrial Exploration , Thermal protection , Inflatable structures , Aerodynamic brakes , Atmospheric entry , Monte carlo method , Probability theory , Sensitivity analysis , Mathematical models , Spacecraft design , Manned mars missions , Component reliability
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|Morphing Hypersonic Inflatable Aerodynamic Decelerator
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