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Composite panel development at JPLParametric computer studies can be use in a cost effective manner to determine optimized composite mirror panel designs. An InterDisciplinary computer Model (IDM) was created to aid in the development of high precision reflector panels for LDR. The materials properties, thermal responses, structural geometries, and radio/optical precision are synergistically analyzed for specific panel designs. Promising panels designs are fabricated and tested so that comparison with panel test results can be used to verify performance prediction models and accommodate design refinement. The iterative approach of computer design and model refinement with performance testing and materials optimization has shown good results for LDR panels.
Document ID
19900004142
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mcelroy, Paul
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Helms, Rich
(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
90N13458
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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