| タイトル | The Earth Observing System AM Spacecraft - Thermal Control Subsystem |
| 著者（英） | Scott, C.; Chalmers, D.; Fredley, J. |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 1993-07-01 |
| 言語 | eng |
| 内容記述 | Mission requirements for the EOS-AM Spacecraft intended to monitor global changes of the entire earth system are considered. The spacecraft is based on an instrument set containing the Advanced Spaceborne Thermal Emission and Reflection radiometer (ASTER), Clouds and Earth's Radiant Energy System (CERES), Multiangle Imaging Spectro-Radiometer (MISR), Moderate-Resolution Imaging Spectrometer (MODIS), and Measurements of Pollution in the Troposphere (MOPITT). Emphasis is placed on the design, analysis, development, and verification plans for the unique EOS-AM Thermal Control Subsystem (TCS) aimed at providing the required environments for all the onboard equipment in a densely packed layout. The TCS design maximizes the use of proven thermal design techniques and materials, in conjunction with a capillary pumped two-phase heat transport system for instrument thermal control. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 93A46581
AIAA PAPER 93-2845 |
| 権利 | Copyright |
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