NASA is conducting an Entry, Descent and Landing Systems Analysis (EDL-SA) Study to determine the key technology development projects that should be undertaken for enabling the landing of large payloads on Mars for both human and robotic missions. Inflatable Aerodynamic Decelerators (IADs) are one of the candidate technologies. A variety of EDL architectures are under consideration. The current effort is conducted for development and simulations of computational framework for inflatable structures.
Aero-Structural Assessment of an Inflatable Aerodynamic Decelerator
2010
143 pages
Report
Keine Angabe
Englisch
Morphing Hypersonic Inflatable Aerodynamic Decelerator
AIAA | 2013
|Morphing Hypersonic Inflatable Aerodynamic Decelerator
British Library Conference Proceedings | 2013
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