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Emissivity measurements on carbon–carbon composites at high temperature under high vacuum

✍ Scribed by M. Balat-Pichelin; J.F. Robert; J.L. Sans


Book ID
104002118
Publisher
Elsevier Science
Year
2006
Tongue
English
Weight
1021 KB
Volume
253
Category
Article
ISSN
0169-4332

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✦ Synopsis


Carbon-carbon composites are candidate materials for the conception of the thermal shield of the ''Solar Probe'' space mission. To understand their behavior under solar aggressions and know the possible interactions with the shipped-in instruments, these materials were tested in a facility that allows to partially simulate the solar environment and to carry out in situ measurements. In this paper, we present the experimental results obtained for the a/e ratio, i.e. the ratio of the solar absorptivity a to the total hemisherical emissivity e that controls the thermal equilibrium of the thermal shield. The objective is to find the lower ratio a/e in order to have the lowest temperature on the shield at 4 solar radii.


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