The stuffed shield with multi-layer insulation(MLI) was designed by improving on Al Whipple shield, and a series of high-velocity impact tests were practiced with a two-stage light gas gun facility at vacuum environment. The damage model of the stuffed shield with different MLI location by Al-sphere projectile impacting was obtained. The effect of MLI on damage of the stuffed shield by high-velocity impact was studied. The results indicate when the MLI is located at front side of the first Al-plate, the protection performance of the stuffed shield is improved with the larger perforation diameter of the first Al-plate and more impact kinetic energy dissipation of the projectile. When MLI is arranged at back side of the first Al-plate, the expansion of the secondary debris cloud from projectile impacting the first Al-plate is restrained, it is not good to improve the protection performance of the stuffed shield. When MLI is arranged at front side of the stuffed wall, the perforation size of the stuffed wall increases; when MLI is arranged at front side of the rear wall, the distribution range of crater on the rear wall decreases.
GAO Y , WANG Z , LU C , et al. State of arts of the dynamic mechanical behaviors of high performance polymer composites in typical aerospace environments[J]. Journal of Materials Engineering, 2015, 43 (3): 106- 112.
MA S H , HUI L , ZHOU S , et al. Influence of corrosion environments on corrosion fatigue property of pre-corroded aluminum alloy[J]. Journal of Materials Engineering, 2015, 43 (2): 91- 95.
4
PALMIERI D , LAMBERT M , MENDOZA M . Effect of multi-layer insulation on top of spacecraft meteoroids/debris shields:prediction of the automated transfer vehicle pressure module ballistic limit[J]. International Journal of Impact Engineering, 2003, 29 (1-10): 537- 548.
doi: 10.1016/j.ijimpeng.2003.10.003
5
WHITE D M , WICKLEIN M , CLEGG R A , et al. Multi-layer insulation material models suitable for hypervelocity impact simulations[J]. International Journal of Impact Engineering, 2008, 35 (12): 1853- 1860.
doi: 10.1016/j.ijimpeng.2008.07.017
LI Y C , LIU Q , MA H J , et al. Thermal properties of multi-layer insulation materials in vacuum[J]. Aerospace Materials & Technology, 2012, (4): 90- 92.
JIANG J S . Multi-layer insulation materials and their application to spacecrafts[J]. Aerospace Materials & Technology, 2000, (4): 17- 25.
8
STADERMANN F J , HEISS C H , REICHLING M . Evaluation of impact craters on solar cell samples and thermal MLI blankets[J]. Advances in Space Research, 1997, 20 (8): 1517- 1521.
doi: 10.1016/S0273-1177(97)00429-8
9
TURNER R J , TAYLOR E A , McDONNELL J A M , et al. Cost effective honeycomb and multi-layer insulation debris shield for unmanned spacecraft[J]. International Journal of Impact Engineering, 2001, 26 (1-10): 785- 796.
doi: 10.1016/S0734-743X(01)00131-2
10
KLINKRAD H . Collision risk analysis for low Earth orbits[J]. Advances in Space Research, 1993, 13 (8): 177- 186.
doi: 10.1016/0273-1177(93)90588-3
HAN H Y , HUANG J R , CHENG W L , et al. The influence of debris shield enhancement on thermal insulation performance of MLI[J]. Journal of Astronautics, 2010, 31 (1): 259- 263.
12
LAMBERT M , SCHAEFER F , GEYER T . Impact damage on sandwich panels and multi-layer insulation[J]. Internatinal Journal of Impact Engineering, 2001, 26 (1-10): 369- 380.
doi: 10.1016/S0734-743X(01)00108-7
HUANG J , MA Z X , LAN S W , et al. Study on hypervelocity impact characteristics for honeycomb sandwich with multi-layer insulation[J]. Journal of Astronautics, 2010, 31 (8): 2043- 2049.
14
CHRISTIANSEN E L , CREWS J I , WILLIAMSEN J E , et al. Enhanced meteoroid and orbital debris shielding[J]. International Journal of Impact Engineering, 1995, 17 (1-3): 217- 228.
doi: 10.1016/0734-743X(95)99848-L
GUAN G S , CHEN L W , WANG S H , et al. Experimental investigation on resist capability of stainless steel mesh/Al multi-shock shield by high-velocity impact[J]. Chinese Journal of High Pressure Physics, 2012, 26 (2): 127- 134.
2016, Vol. 44 
), 曾明, 李航杰
