| タイトル | Thermal Design, Tvac Testing, and Lessons Learned for Critical GSE of ATLAS and the ICESat-2 Mission |
| 本文（外部サイト） | http://hdl.handle.net/2060/20160010083 |
| 著者（英） | Bradshaw, Heather |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 2016-08-01 |
| 言語 | eng |
| 内容記述 | This presentation describes the thermal design of the three main of optical components which comprise the Bench Checkout Equipment (BCE) for the Advanced Topographic Laser Altimeter System (ATLAS) instrument, which is flying on the ICESat-2 mission. Thermal vacuum testing of these components is also described in this presentation, as well as a few lessons learned. These BCE components serve as critical GSE for the mission; their purpose is to verify ATLAS is performing well. It has been said that, in one light, the BCE is the most important part of ATLAS, since, without it, ATLAS cannot be aligned properly or its performance verified before flight. Therefore, careful attention was paid to the BCEs thermal design, development, and component-level Tvac testing prior to its use in instrument-level and spacecraft-level Tvac tests with ATLAS. This presentation describes that thermal design, development, and testing, as well as a few lessons learned. |
| NASA分類 | Spacecraft Design, Testing and Performance |
| レポートNO | GSFC-E-DAA-TN34201 |
| 権利 | No Copyright |
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