| タイトル | Mars Sample Return: Mars Ascent Vehicle Mission and Technology Requirements |
| 本文（外部サイト） | http://hdl.handle.net/2060/20140011316 |
| 著者（英） | Hawke, Veronica M.; Jiang, Xun J.; Bowles, Jeffrey V.; Huynh, Loc C. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 2013-11-01 |
| 言語 | eng |
| 内容記述 | A Mars Sample Return mission is the highest priority science mission for the next decade recommended by the recent Decadal Survey of Planetary Science, the key community input process that guides NASAs science missions. A feasibility study was conducted of a potentially simple and low cost approach to Mars Sample Return mission enabled by the use of developing commercial capabilities. Previous studies of MSR have shown that landing an all up sample return mission with a high mass capacity lander is a cost effective approach. The approach proposed is the use of an emerging commercially available capsule to land the launch vehicle system that would return samples to Earth. This paper describes the mission and technology requirements impact on the launch vehicle system design, referred to as the Mars Ascent Vehicle (MAV). |
| NASA分類 | Astrodynamics; Spacecraft Design, Testing and Performance |
| レポートNO | NASA/TM-2013-216620
ARC-E-DAA-TN12232 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
