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Study of Cryogenic Effect on Hyperyelocity Impact of aluminum Alloy Whitpple Structure

机译:铝合金惠特普尔结构的超高温影响的低温效应研究

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Vast majority of space debris hypervelocity impact tests were performed at room temperature. However, the actual temperature of the environment suffering by spacecraft is very harsh. And the impact characteristic of spacecraft materials and protection structures at such a low temperature should differ from those obtained by conventional laboratory experiments.
机译:绝大多数空间碎片超高速冲击试验都是在室温下进行的。但是,航天器遭受的环境的实际温度非常苛刻。而且,在如此低的温度下,航天器材料和保护结构的冲击特性应不同于通过常规实验室实验获得的冲击特性。

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