Degradation behaviour of a composite material for thermal protection systems. Part II Process simulation
Journal of Materials Science, ISSN: 0022-2461, Vol: 33, Issue: 12, Page: 3145-3149
1998
- 77Citations
- 28Captures
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Example: if you select the 1-year option for an article published in 2019 and a metric category shows 90%, that means that the article or review is performing better than 90% of the other articles/reviews published in that journal in 2019. If you select the 3-year option for the same article published in 2019 and the metric category shows 90%, that means that the article or review is performing better than 90% of the other articles/reviews published in that journal in 2019, 2018 and 2017.
Citation Benchmarking is provided by Scopus and SciVal and is different from the metrics context provided by PlumX Metrics.
Article Description
Mass and energy balance equations have been solved in order to simulate the behavior of a silicon-based ablative composite used as a thermal protection shield for a non-animated space capsule. A method to calculate some of the parameters in the energy balance equation, is proposed, taking advantage of combined thermal analysis techniques. Furthermore, degradation kinetics in the hypothesis of constant volume is used to solve the mass balance. The results of the computer simulation are compared with the experimental data, obtained using plasma arc testing. The model can be used for both material selection and thickness calculation for thermal protection shields. © 1998 Kluwer Academic Publishers.
Bibliographic Details
http://www.scopus.com/inward/record.url?partnerID=HzOxMe3b&scp=0343806598&origin=inward; http://dx.doi.org/10.1023/a:1004352007961; http://link.springer.com/10.1023/A:1004352007961; http://dx.doi.org/10.1023/a%3A1004352007961; https://dx.doi.org/10.1023/a%3A1004352007961; https://link.springer.com/article/10.1023/A:1004352007961
Springer Nature
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