Experimental Study on the Behavior of a New Multilayer Shield Against Hypervelocity Debris Impact

被引:5
作者
Changqing, Miao [1 ]
Bo, Liu [2 ]
机构
[1] Harbin Inst Technol, Ctr Composite Mat, Harbin 150080, Peoples R China
[2] Beijing Res Inst Automat Machinery Ind RIAMB, Beijing 100076, Peoples R China
关键词
Space debris; Hypervelocity impact; Multilayer Shield; SPACE DEBRIS;
D O I
10.1177/096739111402200203
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
To protect the spacecraft from hypervelocity impact of the space debris, anew kind of multilayer shield laminated of aluminum layers and CFRP layers was designed and investigated. Three different shields with the same area density were manufactured, including single aluminum alloy layer, single CFRP layer, and multilayer of aluminum/CFRP. The hypervelocity impact experiment was carried, in which the hypervelocity projectile was launched by a two-stage light gas gun. To compare the hypervelocity impact behavior and evaluate the protection ability of the different shields, the area and depth of the projectile pits were analyzed. The experiments results show that the protection effect of the multilayer shield laminated of aluminum/CFRP layers is better than the single aluminum layer or the single CFRP layer, though they are in the same area density.
引用
收藏
页码:99 / 103
页数:5
相关论文
共 10 条
  • [1] Development of bumper shield using low density materials
    Akahoshi, Y
    Nakamura, R
    Tanaka, M
    [J]. INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2001, 26 (1-10) : 13 - 19
  • [2] DESIGN AND PERFORMANCE EQUATIONS FOR ADVANCED METEOROID AND DEBRIS SHIELDS
    CHRISTIANSEN, EL
    [J]. INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1993, 14 (1-4) : 145 - 156
  • [3] Selecting enhanced space debris shields for manned spacecraft
    Destefanis, R.
    Schaefer, F.
    Lambert, M.
    Faraud, M.
    [J]. INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2006, 33 (1-12) : 219 - 230
  • [4] Prediction of the behaviour of CFRPs against high-velocity impact of solids employing an artificial neural network methodology
    Fernandez-Fdz, D.
    Lopez-Puente, J.
    Zaera, R.
    [J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2008, 39 (06) : 989 - 996
  • [5] Hypervelocity impact tests against metallic meshes
    Higashide, M.
    Tanaka, M.
    Akahoshi, Y.
    Harada, S.
    Tohyama, F.
    [J]. INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2006, 33 (1-12) : 335 - 342
  • [6] Ioilev AG, 2003, INT J IMPACT ENG, V29, P357, DOI 10.1016/j.ijimpeng.2003.009.031
  • [7] The ESA Space Debris Mitigation Handbook 2002
    Klinkrad, H
    Beltrami, P
    Hauptmann, S
    Martin, C
    Sdunnus, H
    Stokes, H
    Walker, R
    Wilkinson, J
    [J]. SPACE DEBRIS, 2004, 34 (05): : 1251 - 1259
  • [8] Shiraki K., 1999, J JAPAN SOC AERONAUT, V47, P189
  • [9] Single bumper shields based on Vectran fibers
    Tanaka, M
    Moritaka, Y
    [J]. SPACE DEBRIS, 2004, 34 (05): : 1076 - 1079
  • [10] Predicting orbital debris shape and orientation effects on spacecraft shield ballistic limits based on characteristic length
    Williamsen, J. E.
    Evans, S. W.
    [J]. INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2006, 33 (1-12) : 862 - 871