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Thermal control of the Lidar In-Space Technology ExperimentThe Lidar In-Space Technology Experiment (LITE) will employ lidar techniques to study the atmosphere from space. The LITE instrument will be flown in the Space Shuttle Payload Bay with an earth directed orientation. The experiment thermal control incorporates both active and passive techniques. The Laser Transmitter Module (LTM) and the system electronics will be actively cooled through the Shuttle pallet coolant loop. The receiver system and experiment platform will be passsively controlled through the use of insulation and component surface properties. This paper explains the thermal control techniques used and the analysis results, with primary focus on the receiver system.
Document ID
19880033878
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Carlson, Ann B.
(NASA Langley Research Center Hampton, VA, United States)
Roettker, William A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
July 1, 1987
Subject Category
Spacecraft Instrumentation
Report/Patent Number
SAE PAPER 871443
Accession Number
88A21105
Distribution Limits
Public
Copyright
Other

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