| タイトル | Earth Entry Requirements for Mars, Europa and Enceladus Sample Return Missions: A Thermal Protection System Perspective |
| 本文（外部サイト） | http://hdl.handle.net/2060/20160012765 |
| 著者（英） | Gage, Peter; Young, Zion; Venkatapathy, Ethiraj; Peterson, Keith; Stackpoole, Mairead; Mahzari, Milad; Ellerby, Don |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 2016-06-13 |
| 言語 | eng |
| 内容記述 | This oral presentation will be given at the 13th International Planetary Probe Workshop on June 14th, 2016 and will cover the drivers for reliability and the challenges faced in selecting and designing the thermal protection system (TPS). In addition, an assessment is made on new emerging TPS related technologies that could help with designs to meet the planetary protection requirements to prevent backward (Earth) contamination by biohazardous samples. |
| NASA分類 | Exobiology; Space Transportation and Safety; Spacecraft Design, Testing and Performance |
| レポートNO | ARC-E-DAA-TN32733 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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