The use of carbon-carbon composites as reentry vehicle nose tips has increased due to their unique thermochemical and thermostructural properties. One performance criterion of particular importance to the aerospace community is the ablation behavior. Since a large number of candidate composites is available, a preliminary screening test was sought which could select the most promising fibers and composites Therofore, the objective of this program was to irradiate various carbon/graphite filaments, bulk pitch matrices, carbon-carbon composites and pyrolytic graphite to characterize mass loss and structural changes. The laser irradiation experiments have provided an insight into the microstructural mechanisms of ablation. They have shwon that correlations exist between mass loss and material properties, tjat differences exist in mass loss characteristics between composite constituents, and that ablation testing results in similar correlations. It was concluded theat laser irradiation of reentry nose tip materials can be used to investigate the behavior of carbonaceous materials in an ablation environment. (Buehn)
Laser irradation of carbon fibers and composites
Die Laserbestrahlung von Carbonfasern und faserverstaerkten Verbundwerkstoffen
US Government Research Reports ; Jan ; 1-81
1979
81 Seiten
Report
Englisch
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