| タイトル | TIRS Cryocooler: Spacecraft Integration and Test and Early Flight Data |
| 本文（外部サイト） | http://hdl.handle.net/2060/20160010591 |
| 著者（英） | Marquardt, E.; Boyle, R. |
| 発行日 | 2013-06-17 |
| 言語 | eng |
| 内容記述 | The Thermal Infrared Sensor (TIRS) is an instrument on Landsat 8, launched in February 2013. The focal plane is cooled by a two-stage Ball Aerospace Stirling cycle cryocooler, with a coldfinger operating at 40K. This paper describes events during the spacecraft integration and test program, and results from early orbit operation of the cryocooler. |
| NASA分類 | Spacecraft Instrumentation and Astrionics |
| レポートNO | LEGNEW-OLDGSFC-PubID14945 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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