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The thermal system for an environmental chamberThe design of a cooling and heating system for obtaining temperatures in the range of -60 C to +120 C on a thermal shroud is described. The proposed temperature control uses mechanical refrigeration with Freon-22 as the primary refrigerant, methanol as the secondary coolant for low temperatures, and electrically heated ethylene glycol for high temperatures. The system is designed to give the following time-temperature characteristics: lowering the temperature from +30 C to -60 C in 1.5 hours; maintaining the temperature at -60 C for a period of 6 hours; heating from -60 C to +120 C in 3 hours; maintaining the temperature at +120 C for a period of 6 hours; and cooling from +120 C in 1.5 hours. A description of the system and its operation are given.
Document ID
19760004063
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Srinivasan, K.
(Space Science and Technology Centre Trivandrum, India)
Narayana, K. B.
(Indian Inst. of Tech.)
Murthy, S. S.
(Indian Inst. of Tech.)
Murthy, M. V. K.
(Indian Inst. of Tech.)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: NASA. Goddard Space Flight Center 8th Conf. on Space Simulation
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
PAPER-39
Accession Number
76N11151
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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