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Thermoelectric temperature control system for the pushbroom microwave radiometer (PBMR)A closed loop thermoelectric temperature control system is developed for stabilizing sensitive RF integrated circuits within a microwave radiometer to an accuracy of + or - 0.1 C over a range of ambient conditions from -20 C to +45 C. The dual mode (heating and cooling) control concept utilizes partial thermal isolation of the RF units from an instrument deck which is thermally controlled by thermoelectric coolers and thin film heaters. The temperature control concept is simulated with a thermal analyzer program (MITAS) which consists of 37 nodes and 61 conductors. A full scale thermal mockup is tested in the laboratory at temperatures of 0 C, 21 C, and 45 C to confirm the validity of the control concept. A flight radiometer and temperature control system is successfully flight tested on the NASA Skyvan aircraft.
Document ID
19840019931
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dillon-Townes, L. A.
(NASA Langley Research Center Hampton, VA, United States)
Averill, R. D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1984
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.15:85824
NASA-TM-85824
Report Number: NAS 1.15:85824
Report Number: NASA-TM-85824
Accession Number
84N28000
Funding Number(s)
PROJECT: RTOP 506-62-63-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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