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Large deployable reflector thermal characteristics in low earth orbitsPreliminary results are presented from the development of a thermal analytical tool capable of analyzing the orbital thermal characteristics of a Large Deployable Reflector (LDR) spaceborne astronomical instrument for observations in the 30-micron to 1-mm range. This LDR thermal analytical tool is a 9X6-node reflector thermal model to be used in conjunction with the thermal analyzer program SINDA, as well as the orbital heat flux program TRASYS for the computation of solar and IR radiation and orbit-related input data.
Document ID
19880035120
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wu, Y. C. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Miyake, R. N. (California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 88-0471
Report Number: AIAA PAPER 88-0471
Accession Number
88A22347
Distribution Limits
Public
Copyright
Other

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