Article(id=1325114485895200924, tenantId=1146029695717560320, journalId=1255847867265597444, issueId=1325114485136044925, 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=1279555200000, receivedDateStr=2010-07-20, revisedDate=1287244800000, revisedDateStr=2010-10-17, acceptedDate=null, acceptedDateStr=null, onlineDate=1793861512874, onlineDateStr=2026-11-05, pubDate=1329235200000, pubDateStr=2012-02-15, doiRegisterDate=null, doiRegisterDateStr=null, onlineIssueDate=1793861512874, onlineIssueDateStr=2026-11-05, onlineJustAcceptDate=null, onlineJustAcceptDateStr=null, onlineFirstDate=null, onlineFirstDateStr=null, sourceXml=null, magXml=null, createTime=1793861512874, creator=13701087609, updateTime=1793861512874, updator=13701087609, issue=Issue{id=1325114485136044925, tenantId=1146029695717560320, journalId=1255847867265597444, year='2012', volume='26', issue='1', pageStart='1', pageEnd='120', issueExtLink='null', onlineDate='null', pubDate='1329235200000', pubDateStr='2012-02-15', beforeIssueId=null, nextIssueId=null, price=null, status=1, issueComplete=1, articleOrder=1, issueType=-1, specialIssue=null, createTime=1793861512693, creator='13701087609', updateTime=1793861512693, updator='13701087609', preIssue=null, nextIssue=null, articleTotal=null, ext=null, issueFiles=null, downloadFileDto=null}, startPage=1, endPage=6, ext={EN=ArticleExt(id=1325114486188802205, articleId=1325114485895200924, tenantId=1146029695717560320, journalId=1255847867265597444, language=EN, title=Damage Characteristics of Rear Walls of Aluminum Whipple Shields by Oblique Hypervelocity Impact of Aluminum Spheres, columnId=null, journalTitle=Chinese Journal of High Pressure Physics, columnName=null, runingTitle=null, highlight=null, articleAbstract=

In order to simulate and study the oblique hypervelocity impacts of space debris on bumper of spacecrafts, a series of oblique hypervelocity impact experiments of aluminum Whipple shields are carried out by a two-stage light gas gun. The aluminum alloy projectile diameter is 3.97 mm, the impact velocities range from 1.14 to 5.35 km/s, and the impact angles range from 0° to 70°. The crater distributions on the rear wall of aluminum Whipple shield obliquely impacted by aluminum spheres are obtained and analyzed. In addition, the forecast equations for crater distribution on the rear wall of aluminum Whipple shield by oblique hypervelocity impact are derived. The results indicate that there are two crater distribution areas on the rear wall under hypervelocity oblique impact. The critical fragmentation velocity of projectile will bring effect on the relationship between the impact damage law of rear wall and impact angle. For aluminum alloy Whipple shield, there exists a critical initial collision angle at which the impact damage on the rear wall is the most severe.

, authors=Gong-Shun GUAN, Yue HA, Bao-Jun PANG, authorsList=Gong-Shun GUAN, Yue HA, 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=1325114486629204126, articleId=1325114485895200924, tenantId=1146029695717560320, journalId=1255847867265597444, language=CN, title=铝球弹丸高速斜撞击铝Whipple防护结构时后板的损伤特性, columnId=0, journalTitle=高压物理学报, columnName=, runingTitle=null, highlight=null, articleAbstract=

为了研究空间碎片对航天器防护结构的高速斜撞击损伤特性,采用二级轻气炮发射铝球弹丸,对铝Whipple防护结构进行高速斜撞击实验。弹丸直径为3.97 mm,撞击速度为1.14~5.35 km/s,撞击角度为0°~70°。实验得到了铝Whipple防护结构在不同撞击速度区间的后板损伤模式,分析了后板撞击损伤及弹坑分布特性,建立了预测铝球弹丸高速斜撞击铝Whipple防护结构时后板弹坑分布的经验公式。结果表明:在大角度斜撞击条件下,对于一定的撞击速度,铝Whipple防护结构的后板弹坑分布会出现两个区域;弹丸的撞击破碎临界速度将影响后板损伤随撞击角的变化关系;对于铝Whipple防护结构,存在使后板撞击损伤最严重的临界撞击角。

, authors=管公顺, 哈跃, 庞宝君, authorsList=管公顺, 哈跃, 庞宝君, authorCompany=null, correspAuthors=null, authorNote=

管公顺(1969—),男,博士,副教授,主要从事超高速撞击动力学及航天器空间碎片防护技术研究. E-mail:

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管公顺(1969—),男,博士,副教授,主要从事超高速撞击动力学及航天器空间碎片防护技术研究. E-mail:

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管公顺(1969—),男,博士,副教授,主要从事超高速撞击动力学及航天器空间碎片防护技术研究. E-mail:

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orderNo=1, keyword=高速斜撞击), Keyword(id=1325114489263227062, tenantId=1146029695717560320, journalId=1255847867265597444, articleId=1325114485895200924, language=CN, orderNo=2, keyword=Whipple防护), Keyword(id=1325114489334530231, tenantId=1146029695717560320, journalId=1255847867265597444, articleId=1325114485895200924, language=CN, orderNo=3, keyword=空间碎片), Keyword(id=1325114489401639096, tenantId=1146029695717560320, journalId=1255847867265597444, articleId=1325114485895200924, language=CN, orderNo=4, keyword=损伤)], refs=[Reference(id=1325114489607159994, tenantId=1146029695717560320, journalId=1255847867265597444, articleId=1325114485895200924, 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=Christiansen E L, Cykowskia E, Ortegaa J. Highly oblique impacts into thick and thin targets[J]. Int J Impact Eng, 1993, 14(1-4): 157-168., articleTitle=null, refAbstract=null), Reference(id=1325114489707823291, tenantId=1146029695717560320, journalId=1255847867265597444, articleId=1325114485895200924, doi=null, pmid=null, pmcid=null, year=null, volume=null, issue=null, pageStart=null, pageEnd=null, url=null, language=null, rfNumber=[2], rfOrder=1, authorNames=null, journalName=null, refType=null, unstructuredReference=Higashide M, Koura T, Akahoshi Y, et al. Debris cloud distributions at oblique impacts[J]. 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铝球弹丸高速斜撞击铝Whipple防护结构时后板的损伤特性
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管公顺 , 哈跃 , 庞宝君
高压物理学报 | 2012,26(1): 1-6
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高压物理学报 | 2012 , 26 (1) : 1 -6
铝球弹丸高速斜撞击铝Whipple防护结构时后板的损伤特性
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管公顺 , 哈跃, 庞宝君
作者信息
  • 哈尔滨工业大学航天学院,黑龙江 哈尔滨 150080
作者简介:

管公顺(1969—),男,博士,副教授,主要从事超高速撞击动力学及航天器空间碎片防护技术研究. E-mail:

Damage Characteristics of Rear Walls of Aluminum Whipple Shields by Oblique Hypervelocity Impact of Aluminum Spheres
Gong-Shun GUAN , Yue HA, Bao-Jun PANG
Affiliations
  • School of Astronautics, Harbin Institute of Technology, Harbin 150080, China
出版时间: 2012-02-15
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为了研究空间碎片对航天器防护结构的高速斜撞击损伤特性,采用二级轻气炮发射铝球弹丸,对铝Whipple防护结构进行高速斜撞击实验。弹丸直径为3.97 mm,撞击速度为1.14~5.35 km/s,撞击角度为0°~70°。实验得到了铝Whipple防护结构在不同撞击速度区间的后板损伤模式,分析了后板撞击损伤及弹坑分布特性,建立了预测铝球弹丸高速斜撞击铝Whipple防护结构时后板弹坑分布的经验公式。结果表明:在大角度斜撞击条件下,对于一定的撞击速度,铝Whipple防护结构的后板弹坑分布会出现两个区域;弹丸的撞击破碎临界速度将影响后板损伤随撞击角的变化关系;对于铝Whipple防护结构,存在使后板撞击损伤最严重的临界撞击角。

高速斜撞击  /  Whipple防护  /  空间碎片  /  损伤

In order to simulate and study the oblique hypervelocity impacts of space debris on bumper of spacecrafts, a series of oblique hypervelocity impact experiments of aluminum Whipple shields are carried out by a two-stage light gas gun. The aluminum alloy projectile diameter is 3.97 mm, the impact velocities range from 1.14 to 5.35 km/s, and the impact angles range from 0° to 70°. The crater distributions on the rear wall of aluminum Whipple shield obliquely impacted by aluminum spheres are obtained and analyzed. In addition, the forecast equations for crater distribution on the rear wall of aluminum Whipple shield by oblique hypervelocity impact are derived. The results indicate that there are two crater distribution areas on the rear wall under hypervelocity oblique impact. The critical fragmentation velocity of projectile will bring effect on the relationship between the impact damage law of rear wall and impact angle. For aluminum alloy Whipple shield, there exists a critical initial collision angle at which the impact damage on the rear wall is the most severe.

oblique hypervelocity impact  /  Whipple shield  /  space debris  /  damage
管公顺, 哈跃, 庞宝君. 铝球弹丸高速斜撞击铝Whipple防护结构时后板的损伤特性. 高压物理学报, 2012 , 26 (1) : 1 -6 .
Gong-Shun GUAN, Yue HA, Bao-Jun PANG. Damage Characteristics of Rear Walls of Aluminum Whipple Shields by Oblique Hypervelocity Impact of Aluminum Spheres[J]. Chinese Journal of High Pressure Physics, 2012 , 26 (1) : 1 -6 .
  • 国防科工局空间碎片专题研究项目(KJSP06211)
参考文献 引证文献
排序方式:
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2012年第26卷第1期
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  • 接收时间:2010-07-20
  • 首发时间:2026-11-05
  • 出版时间:2012-02-15
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  • 收稿日期:2010-07-20
  • 修回日期:2010-10-17
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国防科工局空间碎片专题研究项目(KJSP06211)
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    哈尔滨工业大学航天学院,黑龙江 哈尔滨 150080
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2种不同金属材料的力学参数
科
Family
属数
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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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