| タイトル | Techport Input for Propulsive Descent Technologies (PDT) Project |
| 本文（外部サイト） | http://hdl.handle.net/2060/20140011140 |
| 著者（英） | Campbell, Charles H. |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 2013-09-01 |
| 言語 | eng |
| 内容記述 | The PDT project will investigate the use of retro propulsion during the supersonic phase of atmospheric entry for Mars missions. The project technical approach involves a combination of procurement and evaluation of commercially provided flight data, development of candidate vehicle configurations, and engineering calibration of computational fluid dynamics models to the available flight data. |
| NASA分類 | Lunar and Planetary Science and Exploration; Spacecraft Propulsion and Power |
| レポートNO | JSC-CN-31466 |
| 権利 | No Copyright |
