多孔脆性火山岩弹丸高速撞击航天器典型防护结构试验和仿真分析

朱凼凼;孙英超;庞宝君;贾斌

振动与冲击 ›› 2010, Vol. 29 ›› Issue (7) : 213-215.

PDF(781 KB)
PDF(781 KB)
振动与冲击 ›› 2010, Vol. 29 ›› Issue (7) : 213-215.
论文

多孔脆性火山岩弹丸高速撞击航天器典型防护结构试验和仿真分析

  • 朱凼凼1,2;孙英超1;庞宝君1;贾斌1
作者信息 +

The High-velocity Impact Test and Simulation of brittleness Lava Pill on Spacecraft Typical Shield

  • Zhu dangdang1,2;Sun yingchao1;Pang baojun1
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摘要

本文采用多孔脆性火山岩弹丸,对航天器典型whipple防护结构进行高速撞击试验和仿真计算,分析表明在低速撞击阶段,造成前板铝脱落,但后板并没有发生剥离现象,当撞击试验速度达到2.78km/s时,后板出现剥离现象,此速度可近似为Whipple防护结构遭到破坏的临界速度,试验与仿真结果基本吻合。

Abstract

In order to analyze the damage caused by brittleness meteoroid impaction, This paper use brittleness lava pill with hole to impact spacecraft typical whipple shield with high-velocity. Research show that on the slow velocity phase, impaction causes the front aluminum plate cut down, and when the velocity up to 2.778km/s, the black aluminum plate cut down, this velocity can approximated as critical velocity. The result of simulation is the same as those of tests.

关键词

多孔脆性 / 火山岩 / 高速撞击 / Whipple防护结构 / 损伤特性

Key words

Brittleness / Lava / Pill / High-velocity Impact / spacecraft Whipple Shield / Damage

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导出引用
朱凼凼;孙英超;庞宝君;贾斌. 多孔脆性火山岩弹丸高速撞击航天器典型防护结构试验和仿真分析[J]. 振动与冲击, 2010, 29(7): 213-215
Zhu dangdang;Sun yingchao;Pang baojun. The High-velocity Impact Test and Simulation of brittleness Lava Pill on Spacecraft Typical Shield[J]. Journal of Vibration and Shock, 2010, 29(7): 213-215

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