Experimental Evaluation of Copper Braid Thermal Conductance for IRS-1C Spacecraft

941471

6/1/1994

Authors
Abstract
Content
“Tinned Copper Braid” is planned to be used in IRS-1C spacecraft for the thermal control of the detector of the “Middle Infra Red” (MIR) band of LISS III Camera. The thermal conductance of the braid was evaluated experimentally in the temperature range of -65°C to +35°C by employing the calorimetric technique. The measured thermal conductance of the 215mm long copper braid varies from 0.051 to 0.056 W/°C at different temperatures in the specified range. An error estimation has been performed which shows a maximum uncertainty of better than ± 5% on the conductance value measured.
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DOI
https://doi.org/10.4271/941471
Pages
7
Citation
Ramasamy, A., Ramakrishnan, V., Srinivas, D., Gupta, P. et al., "Experimental Evaluation of Copper Braid Thermal Conductance for IRS-1C Spacecraft," SAE Technical Paper 941471, 1994, https://doi.org/10.4271/941471.
Additional Details
Publisher
Published
6/1/1994
Product Code
941471
Content Type
Technical Paper
Language
English