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Hybrid ablative thermal protection systems and associated methods
Hybrid ablative thermal protection systems and associated methods
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机译:混合烧蚀热保护系统及相关方法
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摘要
A method of forming a thermal protection system for high speed aircraft is described. The method includes mechanically working an uncured ablator material into a first surface of a felt layer such that the ablator material penetrates a distance into a thickness of the felt layer thereby forming an region that has a mixture of felt and ablator material, adding additional uncured ablator material to the worked ablator material, and curing the combined ablator material.
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