| タイトル | Trajectory Design for the Phobos and Deimos & Mars Environment Spacecraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/20160012392 |
| 著者（英） | Loucks, Michel E.; Lee, Pascal; Yang, Fan Yang; Genova, Anthony L.; Korsmeyer, David J. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 2016-09-13 |
| 言語 | eng |
| 内容記述 | The presented trajectory design and analysis was performed for the Phobos and Deimos & Mars Environment (PADME) mission concept as part of a NASA proposal submission managed by NASA Ames Research Center in the 2014-2015 timeframe. The PADME spacecraft would be a derivative of the successfully flown Lunar Atmosphere & Dust Environment Explorer (LADEE) spacecraft. While LADEE was designed to enter low-lunar orbit, the PADME spacecraft would instead enter an elliptical Mars orbit of 2-week period. This Mars orbit would pass by Phobos near periapsis on successive orbits and then raise periapsis to yield close approaches of Deimos every orbit thereafter. |
| NASA分類 | Astrodynamics; Lunar and Planetary Science and Exploration |
| レポートNO | ARC-E-DAA-TN36102 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
