高密度碳酚醛冷浸后的烧蚀性能

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN Pub Date : 1900-01-01 DOI:10.2322/TASTJ.17.333

K. Hirai, Akiko Nakazato, H. Yano, Kenichi Kawazone, J. Koyanagi, Kazuhiko Yamada

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引用次数: 2

摘要

研究了高密度碳酚醛(HD-CFRP)的烧蚀性能，通过暴露在-160摄氏度的极冷温度下，然后在5.5至12.1 MW/ m2的快速加热条件下进行JAXA/ISAS电弧喷射试验，以确定该材料的热完整性，作为要求苛刻的系统要求的未来返回舱隔热材料。

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Ablative Performance of High Density Carbon Phenolic after Cold Soak Exposure

Ablative performance of High-density carbon phenolic (HD-CFRP) is investigated by exposing to an extremely cold temperature of -160 degree Celsius, followed by rapid heating conditions ranging from 5.5 to 12.1 MW/m 2 of JAXA/ISAS arc jet tests to identify the thermal integrity of the material as a future re-entry capsule heat shield material with demanding system requirements, In this paper, we introduce our activities and the outcomes by the investigation.

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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN

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