为满足透明结构空间碎片防护的需求,本文介绍了透明材料的撞击特性验证方法,针对PC、PMMA、耐辐照玻璃等透明材料开展了超高速撞击试验验证,获得了不同材料在超高速撞击后的破坏形式、缺陷大小等,并经分析得到了不同材料的弹道极限。结果表明,若以是否击穿为准则,本试验采用的透明材料的防护能力都强于1.5mm厚5A06铝板,PC材料的防护能力强于PMMA和耐辐照玻璃,PMMA的防护能力与耐辐照玻璃相当。
In order to meet the needs of space debris protection for transparent structure,the impact characteristics and verification method of transparent material are studied.Hypervelocity impact tests are carried out for PC,PMMA and anti-irradiation glasses.The failure forms,the defect sizes of different materials after hypervelocity impact and the ballistic limits of different materials are obtained.The results show that the protection ability of materials used in this test is stronger than that of 1.5mm thick 5A06 aluminum plate,the protection ability of PC is stronger than that of PMMA,and the protection ability of PMMA is equivalent to that of anti-irradiation glasses.
[1] 郑世贵,闫军.空间碎片防护需求与防护材料进展[J].国际太空,2014,426:49-53.
[2] 陈海波.微流星体模拟材料超高速撞击航天器结构损伤特性研究[D].哈尔滨:哈尔滨工业大学.
CHEN H B.Damage characteristics of micro-meteoroid imitation material hypervelocity impacting on the spacecraft[D].Harbin:Harbin Institute of Technology(in Chinese).
[3] 白羽,庞贺伟,龚自正.微小碎片对航天器舷窗玻璃损伤状况的跟踪研究[J].航天器环境工程,2009,26(5):407-410.
BAI Y,PANG H W,GONG Z Z.Research progress of spacecraft window damage caused by small space debris[J].Spacecraft Environment Engineering,2009,26(5):407-410(in Chinese).
[4] 海峰.太空垃圾己对空间站构成威胁[J].科学大观园.2016,14:71-72.
[5] 韩增尧,庞宝君.空间碎片防护研究最新进展[J]. 航天器环境工程,2012,29(4):369-378.
HAN Z Y,PANG B J.Review of recent development of space debris protection research [J].Spacecraft Environment Engineering,2012,29(4):369-378 (in Chinese).
[6] 闫军,郑世贵,于伟,等.空间站的碎片防护设计与实践[J].空间碎片研究,2021,21(2):1-9.
YAN J,ZHENG S G,YU W,et al.Space debris protection design for the space station [J].Space Debris Research,2021,21(2).1-9
[7] 闫军,郑世贵.空间站空间碎片防护设计[J].空间碎片研究,2017,17(1):24-29.
YAN J,ZHENG S G.Space debris protection design for the space station [J].Space Debris Research,2017,17(1):24-29(in Chinese).
[8] 侯明强,童靖宇,龚自正,等.多层冲击防护结构研究进展[J].装备环境工程,2009,6(4):27-32.
HOU M Q,TONG J Y,GONG Z Z,et al.Research progress in multilayer shock shield [J].Equipment Environmental Engineering,2009,6(4):27-32(in Chinese).
[9] 刘启超.空间碎片高速斜撞击填充防护结构的损伤与防护特性研究[D].哈尔滨:哈尔滨工业大学,2017.
LIU Q C.Damage and protection characteristics of stu-ffed shields against high speed oblique impact of space debris[D].Harbin:Harbin Institute of Technology,2017(in Chinese)
[10] 张志林,飞机座舱透明件设计理论及应用[D].南京:南京航空航天大学,2005.
[11] 庞贺伟,龚自正,张文兵,等.航天器舷窗玻璃超高速撞击损伤与M/OD撞击风险评估[J].航天器环境工程,2007,24(3):135-139.
PANG H W,GONG Z Z,ZHANG W B,et al. Hypervelocity impact damage of fused silica glass and M/OD impact risk assessment of spacecraft windshie-ld[J].Spacecraft Environment Engineering,2007,24(3):135-139(in Chinese).
[12] 苏晋,史娇红,汪存显,等.空间碎片对石英玻璃超高速撞击数值模拟研究[J].机械科学与技术,2017,36(11):1791-1797.
SU J,SHI J H,WANG C X,et al.Investigation on hypervelocity simulation for fused silica glass impacted by space debris [J].Mechanical Science and Technology for Aerospace Engineering.2017,36(11):1791-1797 (in Chinese).
[13] Davison D.Computer models of micrometeoroid imp-action fused silica glass mirrors[J].International Jo-urnal of Impact Engineering,2003,29:203-214.
[14] 陈千一,刘凯欣,刘伟东,等.熔融石英玻璃超高速撞击的数值模拟与分析[J].航天器环境工程,2009,26(12):5-8.
[15] 王巍,郑世贵,常洁.柔性多层冲击空间碎片防护结构设计与试验[J].中国空间科学技术,2019,39(4):82-86.
WANG W,ZHENG S G,CHANG J.Design and high velocity impact test verification of flexible space debris protection shield[J].Chinese Space Science and Technology,2019,39(4):82-86 (in Chinese).
[16] 张永,李明,韩增尧.弹丸正撞击Whipple防护结构后墙的穿孔孔径研究[J].航天器工程,2008,12(2):99-103.
ZHANG Y,LI M,HAN Z Y.Empirical hole size model for Whipple shield under projectile normal hypervelocity impact[J].Spacecraft Engineering,2019,39(4):82-86.
[17] 柳森,李毅.Whipple防护屏弹道极限参数试验[J].宇航学报,2004,25(2):205-207.
LIU S,LI Y.Ballistic limit parameter tests of the Whi-pple shield[J].Journal of Astronautics,2004,25(2):205-207.