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Aero-structural assessment of an inflatable aerodynamic decelerator
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Liever, Peter A. Habchi, Sami D. Sheta, Essam F. Tan, X. G. Venugopalan, Vinod |
| Copyright Year | 2010 |
| Description | 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. |
| File Size | 9387843 |
| Page Count | 143 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20100031172 |
| Archival Resource Key | ark:/13960/t1fj7fn43 |
| Language | English |
| Publisher Date | 2010-08-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Simulation Mars Planet Systems Analysis Inflatable Structures Landing Aids Aerodynamic Brakes Atmospheric Entry Descent Toroids Payloads Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
