| タイトル | Entry Descent and Landing Workshop Proceedings |
| 本文（外部サイト） | http://hdl.handle.net/2060/20170002212 |
| 著者（英） | Little, Alan; Munk, Michelle M.; Kuhl, Chris; Santos, Jose; Bose, Deepak |
| 著者所属（英） | NASA Armstrong Flight Research Center |
| 発行日 | 2013-02-12 |
| 言語 | eng |
| 内容記述 | Objectives: Measure Pressure: a) Confirm spacecraft aerodynamics. b) Independently measure attitude. c) Determine density profile. d) Determine wind component. Measure Temperature: a) Verify heating levels on spacecraft surface. b) Determine recession amount and rate. c) Validate material response at Mars conditions. The better we understand the Mars entry environment, the better we can design the next spacecraft. |
| NASA分類 | Spacecraft Instrumentation and Astrionics |
| レポートNO | DFRC-E-DAA-TN28396-2 |
| 権利 | No Copyright |
