Study on Protection of Space Structure from Micrometeoroid Impact
Study on Protection of Space Structure from Micrometeoroid Impact
批准号:
01460086
负责人:
SAWAOKA Akira
金额:
$3.52万
依托单位国家:
日本
项目类别:
Grant-in-Aid for General Scientific Research (B)
财政年份:
1989
资助国家:
日本
项目状态:
已结题
起止时间:
1989 至 1990
中文摘要
为模拟微流星体对空间站等空间结构的超高速撞击,研制了一台等离子体加速器,并在10 km/s的撞击速度下进行了试验。随着碰撞速度的增加,要求增加保险杠板的厚度和主墙与保险杠之间的间隙。为了减轻防护结构的重量和减小防护结构的间隙距离,对由高、低冲击阻抗材料组成的双层缓冲板进行了试验研究。0.5用100毫米的玻璃珠作为微流星体的模型。这种大小的珠子已经被加速到13.8公里/秒。这个值是世界纪录。对由2024铝合金和铜组成的双层缓冲板进行了试验。结果表明,由前铝合金和后铜组成的缓冲器在大于10 km/s的冲击速度下具有很高的防护能力,但由于铜的密度较高,不适合作为空间站的结构材料,陶瓷材料被认为是一种密度较轻的高冲击阻抗材料。下一阶段的研究将对铝合金和氧化铝组成的新型保险杠进行测试。
英文摘要
For the hypervelocity impact simulation of micrometeoroids on the space station and other space structures, a plasma accelerator was constructed and tested over the impact velocity of 10 km/s.The effective protection structure is the dual element shield structure. It is required to increase of thickness of the bumper plate and gap between main wall and bumper with increasing impact velocity. A double layer bumper plate consisted of high and low shock impedance materials were tested for reducing weight and gap distance of the protection structure. 0.5 mm glass beads were used as a model of micrometeoroids. This size of beads has been accelerated up to 13.8 km/s.This value is the world record. The double layered bumper plates consisted of 2024Al alloy and copper were tested. It was found thated protection ability of the bumper consisted of front aluminum alloy and rear-copper is very high in the case higher than 10 km/s impact velocity.Since copper density is high, usage of this material as space station structure is not suitable.Ceramics have been considered as light density and high shock impedance materials. The new type bumper consisted of aluminum alloy and aluminum oxide will be tested on the next phase study.
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H.Tamura: "projectile Hypervelocity Impact Simulation" ISAS Report SP No.11. 21-29 (1990)
H.Tamura:“射弹超高速撞击模拟”ISAS 报告 SP No.11。
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臼井 俊央: "微小隕石防護用二重薄板シ-ルド構造の研究(II)" 圧力技術. 28. 71-81 (1990)
臼井敏夫:“微陨石防护的双薄板屏蔽结构的研究(二)”压力技术28. 71-81(1990)。
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T. Usui: "Separation Method of Projectile from Sabot at Hypervelocity (II)" Prpc.1989 National Symposium on Shock Wave Phenomena. 119-126 (1990)
T.臼井:“超高速弹丸与木托的分离方法(II)”Prpc.1989全国冲击波现象研讨会。
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H.Tamura: "Microprojectile Acceleration by Plasma Accelerator" Proc.American Physical Society Topical Conference,Shock Compression of Condensed Matterー1989. 993-996 (1990)
H. Tamura:“等离子体加速器的微射弹加速”,美国物理学会专题会议,凝聚态物质的冲击压缩 - 1989 (1990)。
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K.Ueda: "Acceleration of 500μm Glass Beads up to 14 km/s by Plasma Accelerator" Rev.Sci.Instr.
K.Ueda:“通过等离子体加速器将 500μm 玻璃珠加速至 14 km/s”Rev.Sci.Instr。
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Development of Plasma Gun as a Micro Meteorite Impact Simulator
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