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Based on the analysis of the shield performance for different shield parameters and impact parameters, the influences of shield spacing, thickness of wall, impact velocities and impact angles on the shield performance are discussed. The shield performance of the Whipple shield is not influenced by shield spacing, when the impact velocities are less than 3 km/s, but significant influence of shield spacing is evident when the impact velocities are at the range of v>3 km/s. Better shield performance is found in thicker shield. The ballistic limit curves have three different trends. The critical projectile diameter increases with impact velocities at the range of v≤3 km/s or v≥7 km/s, and decreases with impact velocities at the range of 3 km/s<v<7 km/s. Namely, the shield performance sees three different trends with the impact velocities ranging from 0 to 15 km/s. And better performance is expected with larger impact angle. A design method for Corrugated Stuffed Whipple shield (CSW) is given. The results of analysis show that shield performance for CSW improves with increase of corrugated angle. 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articleAbstract=论述了流星体/空间碎片(M/OD)防护的重要性,给出了自主开发的空间碎片防护结构效能评价仿真平台总体框架。通过分析不同防护参数及碰撞参数条件下的防护结构效能,总结了防护间距、防护屏厚度、碰撞速度和碰撞角等参数对空间碎片防护结构效能的影响规律。针对基本的Whipple防护结构,碰撞速度v<3 km/s时,防护结构的防护效能不受防护间距变化的影响,碰撞速度v>3 km/s时,防护间距越大,防护结构的防护效能越好;Whipple防护结构的防护屏厚度越大,防护结构抗空间碎片撞击的能力越强,即其防护效能越好;在整个碰撞速度范围内(0~15 km/s),防护结构的防护效能呈现出3种不同的变化趋势,且防护结构的防护效能随碰撞角增大而提高。提出了一种波纹填充式防护结构,确定了可有效防护小尺寸空间碎片的防护设计参数。, authors=刘有英1,王海福2,黄海1, authorsList=刘有英;王海福;黄海, authorCompany=1. 北京航空航天大学宇航学院2. 北京理工大学, correspAuthors=null, authorNote=null, correspAuthorsNote=王海福, copyrightStatement=null, copyrightOwner=null, extLink=null, articleAbsUrl=null, sourceXml=null, magXml=null, pdfUrl=null, pdf=AvJlKFMwSv3cUkbfk71rMQ==, pdfFileSize=653920, pdfExtLink=null, richHtmlUrl=null, mobilePdfUrl=null, reviewReport=null, pdfFirstPage=null, abstractGraph=null, abstractGraphContent=null, abstractVideo=null, citation=null, cebUrl=null, magXmlContent=null, mapNumber=null, fund=null)}, authors=null, keywords=[Keyword(id=1242117247834066982, 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科技导报 |研究论文 2009 , 27 (0918) : 33 -37
空间碎片防护结构效能评价仿真系统和应用
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刘有英1,王海福2,黄海1
作者信息
    1. 北京航空航天大学宇航学院2. 北京理工大学
通讯作者:
王海福
Development and Application of a Performance Evaluation System for Meteoroid/Orbital Debris Shield
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    出版时间: 2009-09-28
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    论述了流星体/空间碎片(M/OD)防护的重要性,给出了自主开发的空间碎片防护结构效能评价仿真平台总体框架。通过分析不同防护参数及碰撞参数条件下的防护结构效能,总结了防护间距、防护屏厚度、碰撞速度和碰撞角等参数对空间碎片防护结构效能的影响规律。针对基本的Whipple防护结构,碰撞速度v<3 km/s时,防护结构的防护效能不受防护间距变化的影响,碰撞速度v>3 km/s时,防护间距越大,防护结构的防护效能越好;Whipple防护结构的防护屏厚度越大,防护结构抗空间碎片撞击的能力越强,即其防护效能越好;在整个碰撞速度范围内(0~15 km/s),防护结构的防护效能呈现出3种不同的变化趋势,且防护结构的防护效能随碰撞角增大而提高。提出了一种波纹填充式防护结构,确定了可有效防护小尺寸空间碎片的防护设计参数。
    流星体/空间碎片  /  防护结构  /  效能评价  /  航天器
    The importance of a Meteoroid/Orbital Debris (M/OD) shield is analyzed and the framework of a performance evaluation system for M/OD shield is given. Based on the analysis of the shield performance for different shield parameters and impact parameters, the influences of shield spacing, thickness of wall, impact velocities and impact angles on the shield performance are discussed. The shield performance of the Whipple shield is not influenced by shield spacing, when the impact velocities are less than 3 km/s, but significant influence of shield spacing is evident when the impact velocities are at the range of v>3 km/s. Better shield performance is found in thicker shield. The ballistic limit curves have three different trends. The critical projectile diameter increases with impact velocities at the range of v≤3 km/s or v≥7 km/s, and decreases with impact velocities at the range of 3 km/s<v<7 km/s. Namely, the shield performance sees three different trends with the impact velocities ranging from 0 to 15 km/s. And better performance is expected with larger impact angle. A design method for Corrugated Stuffed Whipple shield (CSW) is given. The results of analysis show that shield performance for CSW improves with increase of corrugated angle. The shield parameters of CSW are established to protect spacecraft from small orbital debris impact.
    Meteoroid/Orbital Debris  /  shield structure  /  performance evaluation  /  spacecraft
    刘有英;王海福;黄海. 空间碎片防护结构效能评价仿真系统和应用. 科技导报, 2009 , 27 (0918) : 33 -37 .
    . Development and Application of a Performance Evaluation System for Meteoroid/Orbital Debris Shield[J]. Science & Technology Review, 2009 , 27 (0918) : 33 -37 .

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    • 接收时间:2009-07-16
    • 首发时间:2009-09-28
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    2种不同金属材料的力学参数

    Family
    属数
    Number of
    genus
    种数
    Number of
    species
    占总种数比例
    Percentage of
    total species (%)

    Genus
    种数
    Number of
    species
    占总种数比例
    Percentage of total
    species (%)
    鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
    小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
    多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
    红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
    小菇属 Mycena 11 5.26
    光柄菇属 Pluteus 5 2.39
    红菇属 Russula 17 8.13
    栓菌属 Trametes 5 2.39
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