Some Aspects of Thermal Modeling Theory and Analysis as Applied to Spacecraft Temperature Control 690199
A description of digital computer methods and numerical techniques which are used in evaluating temperature distributions in spacecraft structures is presented.
The theory and application of thermal modeling from the point of view of comparing the accuracy of simplified analytical models with zonal and nodal methods are discussed, and an example is given to illustrate the general theory.
Citation: Karam, R. and Eby, R., "Some Aspects of Thermal Modeling Theory and Analysis as Applied to Spacecraft Temperature Control," SAE Technical Paper 690199, 1969, https://doi.org/10.4271/690199. Download Citation
Author(s):
Robert D. Karam, Robert J. Eby
Affiliated:
Fairchild Hiller Space and Electronics Systems
Pages: 9
Event:
1969 International Automotive Engineering Congress and Exposition
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Spacecraft
Simulation and modeling
Logistics
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