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HYPER VELOCITY IMPACT DAMAGE TO SPACE FLYER UNIT THERMAL CONTROL SURFACES

机译：超速撞击对飞行器单元热控制表面的损害

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Presented here are the latest results of the post-flight analysis of the Space Flyer Unit, Japan's first retrievable spacecraft.rnThe morphology of impact features in silverised Teflon second-surface mirrors (SSMs) and aluminised Kapton multi-layer insulation (MLI) is discussed. Morphological comparisons are made between laboratory and space impacts into MLI material.rnFlux figures are shown for various SFU surfaces and compared with fluxes from earlier spacecraft, such as the Long Duration Exposure Facility and EuReCa.rnA summary of the hypervelocity impact calibration programme is given, including laboratory tests carried out at 5 km s~(-1) and around 3.5 km s~(-1) into Kapton film of various thicknesses. The results of these tests are shown.

机译：此处介绍的是日本首架可回收航天器太空飞行器单元飞行后分析的最新结果。rn讨论了镀银的特富龙第二面反射镜（SSM）和镀铝的Kapton多层绝缘材料（MLI）的撞击特征形态。对实验室和空间撞击MLI材料的形态进行了比较.rn示出了各种SFU表面的通量数据，并将其与早期航天器的通量进行了比较，例如长期暴露设施和EuReCa.rn给出了超高速撞击校准程序的摘要，包括在5 km s〜（-1）和3.5 km s〜（-1）左右的各种厚度的Kapton薄膜中进行的实验室测试。显示了这些测试的结果。

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来源
《Materials in space environment》|1997年|477-484|共8页
会议地点 Toulouse(FR)
作者
M.J. Neish; H. Yano; S. Kibe; S.P. Deshpande; Y. Kitazawa; S. Yamamoto;
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作者单位

National Aerospace Laboratory, 7-44-1 Jindaijihigashi-machi, Chofu City, Tokyo 182, Japan;

Institute of Space and Astronautical Sciences, 3-1-1 Yoshinodai, Sagamihara City, Kanagawa 229, Japan;

National Aerospace Laboratory, 7-44-1 Jindaijihigashi-machi, Chofu City, Tokyo 182, Japan;

National Aerospace Laboratory, 7-44-1 Jindaijihigashi-machi, Chofu City, Tokyo 182, Japan;

Ishikawajima-Harima Heavy Industries (IHI), 1 Shin Nakahara-cho, Isogoku, Yokohama City, Kanagawa 235, Japan;

Kobe University, Rokkodai-cho, Nada-ku, Kobe 657, Japan;

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原文格式 PDF
正文语种 eng
中图分类航空用材料;地面设备、试验场、发射场、航天基地;
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机译：激光加速飞行器在超高速冲击下的CFRP断裂
3. Deformation and Fracture of CFRP under Hyper-Velocity Impact Test Using Laser-Accelerated Flyer [J] . Yoshiaki Yamauchi, Motohiro Nakano, Keizo Kishida 日本航空宇宙学会論文集 . 2001,第571期

机译：激光加速飞行器超高速冲击试验下CFRP的变形和断裂
4. HYPER VELOCITY IMPACT DAMAGE TO SPACE FLYER UNIT THERMAL CONTROL SURFACES [C] . International symposium on materials in space environment . 1997

机译：超速冲击损坏空间传单单元热控制表面
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8. Sunspot: A program to model the behavior of hypervelocity impact damaged multilayer insulation in the Sunspot thermal vacuum chamber of Marshall Space Flight Center [R] . Rule, W. K., Hayashida, K. B. 1992

机译：太阳黑子：一个模拟马歇尔太空飞行中心太阳黑子热真空室中超高速撞击破坏多层绝缘的行为的程序

HYPER VELOCITY IMPACT DAMAGE TO SPACE FLYER UNIT THERMAL CONTROL SURFACES

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