Fig. 1. Experimental speicmen: Solar array cells and carbon fiber honeycomb plate.太阳电池片单元与碳纤维蜂窝板试样

Fig. 2. Photograph of experimental specimen in hypervelocity tests.超高速撞击试件照片

Fig. 3. Impact point location: (a) Center of a cell; (b) edge of a cell; (c) joints of two or more cells.撞击点位置示意图 (a)单片中心A; (b)单片边缘B; (c)两片连接处C

Fig. 4. Damage morphology of solar cells: (a) Center of a cell; (b) joints of two cells; (c) edge of a cell.太阳电池片损伤形貌　(a)撞击单片中心区域No.5; (b)撞击两片连接处No.12; (c)撞击单片边界No.8

Fig. 5. A front-back perforation of the solar arrays exposed on the hubble space telescope caused by orbital debris impact^[1,6]哈勃望远镜太阳电池阵电池面超高速撞击穿孔形貌^[1,6]

Fig. 6. Measured parameters of perforation hole area and conchoidal area (No.16).穿孔面积与剥落区面积(No.16)

Fig. 7. Relationship between projectile diameter d and perforation diameter D_h. 穿孔直径D_h与弹丸直径d的关系

Fig. 8. Relationship between perforation diameter D_h and impact velocity v. 穿孔直径D_h与撞击速度v的关系

Fig. 9. Equations of perforation diameter D_h. 穿孔直径D_h方程的曲线

Fig. 10. Equations of conchoidal diameter D_s (Type A of impact position). 贝壳状剥落区直径D_s方程的曲线(撞击位置类型A)

Fig. 11. Equations of conchoidal diameter D_s (Type B and C of impact position). 贝壳状剥落区直径D_s方程的曲线(撞击位置类型B, C)

Fig. 12. Relationship between perforation diameter D_h and conchoidal diameter D_s. 穿孔直径D_h与剥落区等效直径D_s的关系