Article(id=1322971675096133929, tenantId=1146029695717560320, journalId=1255847867265597444, issueId=1322971592304763246, articleNumber=null, orderNo=null, doi=null, pmid=null, cstr=null, oa=null, hot=null, price=null, onlineType=0, articleFormat=0, articleType=null, articleTypeStr=null, receivedDate=1227974400000, receivedDateStr=2008-11-30, revisedDate=1235232000000, revisedDateStr=2009-02-22, acceptedDate=null, acceptedDateStr=null, onlineDate=1793350626967, onlineDateStr=2026-10-30, pubDate=1260806400000, pubDateStr=2009-12-15, doiRegisterDate=null, doiRegisterDateStr=null, onlineIssueDate=1793350626967, onlineIssueDateStr=2026-10-30, onlineJustAcceptDate=null, onlineJustAcceptDateStr=null, onlineFirstDate=null, onlineFirstDateStr=null, sourceXml=null, magXml=null, createTime=1793350626967, creator=13701087609, updateTime=1793350626967, updator=13701087609, issue=Issue{id=1322971592304763246, tenantId=1146029695717560320, journalId=1255847867265597444, year='2009', volume='23', issue='6', pageStart='401', pageEnd='480', issueExtLink='null', onlineDate='null', pubDate='1260806400000', pubDateStr='2009-12-15', beforeIssueId=null, nextIssueId=null, price=null, status=1, issueComplete=1, articleOrder=1, issueType=-1, specialIssue=null, createTime=1793350607229, creator='13701087609', updateTime=1793350607229, updator='13701087609', preIssue=null, nextIssue=null, articleTotal=null, ext=null, issueFiles=null, downloadFileDto=null}, startPage=453, endPage=459, ext={EN=ArticleExt(id=1322971678438994223, articleId=1322971675096133929, tenantId=1146029695717560320, journalId=1255847867265597444, language=EN, title=Numerical Simulation Investigation in Hypervelocity Impact on Shield Structure Containing Aluminum Foam, columnId=null, journalTitle=Chinese Journal of High Pressure Physics, columnName=null, runingTitle=null, highlight=null, articleAbstract=

Aluminum foam is a new type of material for shield of spacecrafts which bears fine characteristics when subjected to hypervelocity impact of space debris. A microstructure model of geometry for metallic foams was developed to simulate their manufacturing process. Numerical simulations on hypervelocity impact were carried out using self-programmed Smooth Particle Hydrodynamics, and the proposed model is validated by comparison with experimental results. Two Al-foam-containing shield structures against space debris were presented including Al-foam stuffed shield and Al-foam sandwiched shield. Ballistic limit curves of both shields were obtained respectively through numerical simulations. Analyses results indicate that the shield performance of Al-foam stuffed shield is better than that of Al-foam sandwiched shield for the majority of impact speed range referring to shield against space debris.

, authors=Bin JIA1, Zhi-Tao MA2, Bao-Jun PANG1, authorsList=Bin JIA, Zhi-Tao MA, Bao-Jun PANG, authorCompany=null, correspAuthors=null, authorNote=null, correspAuthorsNote=null, copyrightStatement=null, copyrightOwner=null, extLink=null, articleAbsUrl=null, sourceXml=null, magXml=null, pdfUrl=null, pdf=null, pdfFileSize=null, 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), CN=ArticleExt(id=1322971683438604596, articleId=1322971675096133929, tenantId=1146029695717560320, journalId=1255847867265597444, language=CN, title=含泡沫铝防护结构的超高速撞击数值模拟研究, columnId=0, journalTitle=高压物理学报, columnName=, runingTitle=null, highlight=null, articleAbstract=

泡沫铝是一种新型航天器防护材料,拥有良好的抵御空间碎片超高速撞击的特性。模仿泡沫金属的生产原理,建立了泡沫金属微结构几何模型,结合自编的光滑质点流体动力学程序进行了超高速撞击数值仿真,通过与实验结果的对比,验证了模型的有效性。提出了两种含泡沫铝的空间碎片防护结构,即填充泡沫铝结构和夹层泡沫铝结构。对这两种结构分别进行了仿真计算,获得了其撞击极限曲线。分析结果表明,在空间碎片防护领域涉及的大部分撞击速度区间内,填充泡沫铝结构的防护性能优于夹层泡沫铝结构。

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贾斌(1975—),男,博士,副教授,主要从事航天器空间碎片防护研究. E-mail:

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贾斌(1975—),男,博士,副教授,主要从事航天器空间碎片防护研究. E-mail:

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articleId=1322971675096133929, language=CN, orderNo=5, keyword=撞击极限), Keyword(id=1322971715436949870, tenantId=1146029695717560320, journalId=1255847867265597444, articleId=1322971675096133929, language=CN, orderNo=6, keyword=空间碎片)], refs=[Reference(id=1322971720851796343, tenantId=1146029695717560320, journalId=1255847867265597444, articleId=1322971675096133929, doi=null, pmid=null, pmcid=null, year=null, volume=null, issue=null, pageStart=null, pageEnd=null, url=null, language=null, rfNumber=[1], rfOrder=0, authorNames=null, journalName=null, refType=null, unstructuredReference=Min G R, Xiao M X. 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Selecting Enhanced Space Debris Shields for Manned Spacecraft[J]. Int J Impact Eng, 2006, 33: 219-230., articleTitle=null, refAbstract=null), Reference(id=1322971733808001415, tenantId=1146029695717560320, journalId=1255847867265597444, articleId=1322971675096133929, doi=null, pmid=null, pmcid=null, year=null, volume=null, issue=null, pageStart=null, pageEnd=null, url=null, language=null, rfNumber=[10], rfOrder=12, authorNames=null, journalName=null, refType=null, unstructuredReference=Hayhurst C J, Livingstone I H. Advanced Numerical Simulations for Hypervelocity Impacts[R]. 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含泡沫铝防护结构的超高速撞击数值模拟研究
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贾斌 1 , 马志涛 2 , 庞宝君 1
高压物理学报 | 2009,23(6): 453-459
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高压物理学报 | 2009 , 23 (6) : 453 -459
含泡沫铝防护结构的超高速撞击数值模拟研究
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贾斌1 , 马志涛2, 庞宝君1
作者信息
  • 1.哈尔滨工业大学航天工程系,黑龙江 哈尔滨 150001
  • 2.清华大学航天航空学院,北京 100084
作者简介:

贾斌(1975—),男,博士,副教授,主要从事航天器空间碎片防护研究. E-mail:

Numerical Simulation Investigation in Hypervelocity Impact on Shield Structure Containing Aluminum Foam
Bin JIA1 , Zhi-Tao MA2, Bao-Jun PANG1
Affiliations
  • 1.Department of Astronautics Engineering, Harbin Institute of Technology, Harbin 150001, China
  • 2.School of Aerospace, Tsinghua University, Beijing 100084, China
出版时间: 2009-12-15
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泡沫铝是一种新型航天器防护材料,拥有良好的抵御空间碎片超高速撞击的特性。模仿泡沫金属的生产原理,建立了泡沫金属微结构几何模型,结合自编的光滑质点流体动力学程序进行了超高速撞击数值仿真,通过与实验结果的对比,验证了模型的有效性。提出了两种含泡沫铝的空间碎片防护结构,即填充泡沫铝结构和夹层泡沫铝结构。对这两种结构分别进行了仿真计算,获得了其撞击极限曲线。分析结果表明,在空间碎片防护领域涉及的大部分撞击速度区间内,填充泡沫铝结构的防护性能优于夹层泡沫铝结构。

泡沫铝  /  防护结构  /  超高速撞击  /  SPH  /  撞击极限  /  空间碎片

Aluminum foam is a new type of material for shield of spacecrafts which bears fine characteristics when subjected to hypervelocity impact of space debris. A microstructure model of geometry for metallic foams was developed to simulate their manufacturing process. Numerical simulations on hypervelocity impact were carried out using self-programmed Smooth Particle Hydrodynamics, and the proposed model is validated by comparison with experimental results. Two Al-foam-containing shield structures against space debris were presented including Al-foam stuffed shield and Al-foam sandwiched shield. Ballistic limit curves of both shields were obtained respectively through numerical simulations. Analyses results indicate that the shield performance of Al-foam stuffed shield is better than that of Al-foam sandwiched shield for the majority of impact speed range referring to shield against space debris.

aluminum foam  /  shield structure  /  hypervelocity impact  /  SPH  /  ballistic limit  /  space debris
贾斌, 马志涛, 庞宝君. 含泡沫铝防护结构的超高速撞击数值模拟研究. 高压物理学报, 2009 , 23 (6) : 453 -459 .
Bin JIA, Zhi-Tao MA, Bao-Jun PANG. Numerical Simulation Investigation in Hypervelocity Impact on Shield Structure Containing Aluminum Foam[J]. Chinese Journal of High Pressure Physics, 2009 , 23 (6) : 453 -459 .
  • 中国空间技术研究院创新基金(CAST200723)
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2009年第23卷第6期
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  • 接收时间:2008-11-30
  • 首发时间:2026-10-30
  • 出版时间:2009-12-15
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  • 收稿日期:2008-11-30
  • 修回日期:2009-02-22
基金
中国空间技术研究院创新基金(CAST200723)
作者信息
    1.哈尔滨工业大学航天工程系,黑龙江 哈尔滨 150001
    2.清华大学航天航空学院,北京 100084
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2种不同金属材料的力学参数
科
Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)
属
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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