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Accuracy of Extrapolation of Equilibrium Temperatures of Transient Fields of Temperature with Two Different Mathematical Approaches

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Eckert, K., author.
Conference Name:
International Conference on Environmental Systems (1995-07-10 : San Diego, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1995
Summary:
AbstractA key element of spacecraft thermal balance testing is the reliable determination of the final temperature values of the temperature equilibrium. At the end of a thermal balance test phase, temperature equilibrium is generally considered to be reached when nearly all thermocouples have fulfilled pre-defined temperature equilibrium criteria, e.g. in the form of a maximal allowed rate of temperature change.Test time can be reduced in the same manner as the equilibrium temperatures can be reliably extrapolated from the measured thermocouples temperatures, thus requiring only a less stringent equilibrium criterion to be fulfilled by the sensed temperatures.This paper concentrates on a mathematical theory for practical use in the extrapolation of equilibrium temperatures for spacecraft and units with essentially radiative couplings to their thermal environment
Notes:
Vendor supplied data
Publisher Number:
951696
Access Restriction:
Restricted for use by site license

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