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Large Deployable Reflector (LDR) thermal characteristicsThe thermal support group, which is part of the lightweight composite reflector panel program, developed thermal test and analysis evaluation tools necessary to support the integrated interdisciplinary analysis (IIDA) capability. A detailed thermal mathematical model and a simplified spacecraft thermal math model were written. These models determine the orbital temperature level and variation, and the thermally induced gradients through and across a panel, for inclusion in the IIDA.
Document ID
19900004144
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Miyake, R. N. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Wu, Y. C. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
August 15, 1988
Publication Information
Publication: Report of the Asilomar 3 LDR Workshop
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
90N13460
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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