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Thermal Analysis of a Finite Element Model in a Radiation Dominated EnvironmentThis paper presents a brief overview of thermal analysis, evaluating the University of Arizona mirror design, for the Next Generation Space Telescope (NGST) Pre-Phase A vehicle concept. Model building begins using Thermal Desktop(Tm), by Cullimore and Ring Technologies, to import a NASTRAN bulk data file from the structural model of the mirror assembly. Using AutoCAD(R) capabilities, additional surfaces are added to simulate the thermal aspects of the problem which, for due reason, are not part of the structural model. Surfaces are then available to accept thermophysical and thermo-optical properties. Thermal Desktop(Tm) calculates radiation conductors using Monte Carlo simulations. Then Thermal Desktop(Tm) generates the SINDA/Fluint input file having a one-to-one correspondence with the NASTRAN node and element definitions. A model is now available to evaluate the mirror design in the radiation dominated environment conduct parametric trade studies of the thermal design, and provide temperatures to the finite element structural model.
Document ID
19990105701
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Page, Arhur T.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1999
Subject Category
Optics
Meeting Information
Meeting: Thermal and Fluids Analysis
Location: Huntsville, AL
Country: United States
Start Date: September 13, 1999
End Date: September 17, 1999
Funding Number(s)
PROJECT: RTOP 839-06-70-00-ED
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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