| タイトル | Hypersonic and Supersonic Static Aerodynamics of Mars Science Laboratory Entry Vehicle |
| 本文（外部サイト） | http://hdl.handle.net/2060/20120011936 |
| 著者（英） | Dyakonov, Artem A.; Vannorman, John W.; Schoenenberger, Mark |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2012-06-25 |
| 言語 | eng |
| 内容記述 | This paper describes the analysis of continuum static aerodynamics of Mars Science Laboratory (MSL) entry vehicle (EV). The method is derived from earlier work for Mars Exploration Rover (MER) and Mars Path Finder (MPF) and the appropriate additions are made in the areas where physics are different from what the prior entry systems would encounter. These additions include the considerations for the high angle of attack of MSL EV, ablation of the heatshield during entry, turbulent boundary layer, and other aspects relevant to the flight performance of MSL. Details of the work, the supporting data and conclusions of the investigation are presented. |
| NASA分類 | Aerodynamics |
| レポートNO | NF1676L-14276 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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