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Micrometeoroid and Orbital Debris Environments for the International Space Station

机译：国际空间站的微流星体和轨道碎片环境

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Baseline micrometeoroid and orbital debris fluence estimates for spacecraft in low Earth orbit (LEO) are provided. For these calculations, an orbit similar to that of the International Space Station (ISS) is used.

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作者
Gallini, T. E. ; Hackwell, J. A. ; Marin, D. C. ; Zambran, M. ; Peterson, G. E.;
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年度 2007
页码 p.1-12
总页数 12
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Spacecraft; Earth orbits; Meteoroids; Space stations; Damage; Particles; International; Comets; Asteroids; Silicates; Radiofrequency; Base lines; Estimates; Debris;

机译：航天器;地球轨道;流星体;空间站;损坏;粒子;国际;彗星;小行星;硅酸盐;射频;基线;估计;碎片;

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专利

1. The effect of thin deployable construction elements of the international space station on the probability of its hull penetration by meteoroids and orbital debris [J] . V.G. Sokolov, E.L. Christiansen, A.V. Gorbenko International journal of impact engineering . 2001,第1a10期

机译：国际空间站可展开的薄型建筑构件对其流星体和轨道碎片穿透其船体的可能性的影响
2. Low Earth Orbit Space Environment Testing of Extreme Temperature 6H-SiC JFETs on the International Space Station [J] . Philip G. Neudeck, Norman F. Prokop, Lawrence C. Greer III, Materials science forum . 2011,第期

机译：国际空间站上的高温6H-SiC JFET的低地球轨道空间环境测试
3. Erosion yield of epoxy-silica nanocomposites at the lower earth orbit environment of the International Space Station [J] . Yagnamurthy S., Chen Q., Chen C., Journal of Composite Materials . 2013,第1期

机译：国际空间站低地球轨道环境中环氧二氧化硅纳米复合材料的冲蚀收率
4. Consequences of micrometeoroid/orbital debris penetrations on the International Space Station [C] . Hilary J. Evans, James L. Hyde, Eric L. Christansen, Hypervelocity Impact Symposium . 2019

机译：微型物体/轨道碎片渗透在国际空间站的后果
5. Meteoroid and orbital debris (M/OD) shielding concepts for utility lines on the International Space Station. [D] . Dale, Steven Edward. 1998

机译：国际空间站上通用线路的流星体和轨道碎片（MMOD）屏蔽概念。
6. The space-flight environment: the International Space Station and beyond [O] . Robert Thirsk, Andre Kuipers, Chiaki Mukai, 2009

机译：太空飞行环境：国际空间站及以后
7. Bounding the Risk of Crew Loss Following Orbital Debris Penetration of the International Space Station at Assembly Stages 1J and 1E [O] . Bohl W., Lewis H., Evans S., 2002

机译：在组装阶段1J和1E侵害国际空间站的轨道碎片后，机组人员流失的风险必将上升

Micrometeoroid and Orbital Debris Environments for the International Space Station

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