超高速
航天飞机
航空航天工程
门
射弹
航天飞机热防护系统
航程(航空)
材料科学
环境科学
核工程
结构工程
热保护
复合材料
工程类
物理
冶金
热力学
摘要
Studies of the acoustic signals originating from impact damage on Space Shuttle components were undertaken. Sprayed on foam insulation and small aluminum spheres were used as impactors. Shuttle reinforced carbon‐carbon panels, panels with Shuttle thermal protection tiles, and Shuttle main landing gear doors with tiles were targets. Ballistic speed and hypervelocity impacts over a wide range of impactor sizes, energies, and angles were tested. Additional tests were conducted to correlate the acoustic response of the test articles to actual Shuttle structures.
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