Thermal Assessment of Landsat-7 ETM+ Radiative Cooler in Instrument and Spacecraft Thermal Vacuum Tests and in Flight

1999-01-2628

08/02/1999

Event
34th Intersociety Energy Conversion Engineering Conference
Authors Abstract
Content
During the radiative cooler cool-down phase of the Landsat-7 Enhanced Thematic Mapper Plus (ETM+) instrument thermal vacuum test #3, the coldest temperature that the cold focal plane array (CFPA) achieved was 89.5 K. The cold stage/CFPA temperature decreased from 315 K to 89.5 K in 80 hours. In the spacecraft and instrument integrated thermal vacuum test, the cold stage/ CFPA temperature decreased from 315 K to 86.9 K in 80 hours, and was still decreasing at a rate of 0.1 K/hr when the cool-down was terminated. The cool-down was faster, and a colder CFPA temperature was obtained. In flight, the cooler cool-down was even faster, and colder. The cold stage/CFPA temperature decreased from 315 K to 89.7 K in 33 hours, and was still decreasing at a rate of 1 K/hr when cool-down was terminated at 89.7 K. The factors that affected the ETM+ cooler cool-down are the radiation heat sink temperature for the cold stage and intermediate stage, parasitic radiation heat load to the cooler, parasitic conduction heat load to the cooler, and cooler outgas time preceding cooler cool-down.
Meta TagsDetails
DOI
https://doi.org/10.4271/1999-01-2628
Pages
9
Citation
Choi, M., "Thermal Assessment of Landsat-7 ETM+ Radiative Cooler in Instrument and Spacecraft Thermal Vacuum Tests and in Flight," SAE Technical Paper 1999-01-2628, 1999, https://doi.org/10.4271/1999-01-2628.
Additional Details
Publisher
Published
Aug 2, 1999
Product Code
1999-01-2628
Content Type
Technical Paper
Language
English