[1] |
Min G R, Xiao M X. Reliability Design of Spacecraft Module Wall against Meteoroid Perforation [J]. Chinese Space Science and Technology, 1986, (6): 45-48. (in Chinese) |
[2] |
闽桂荣, 肖名鑫. 防止微流星击穿航天器舱壁的可靠性设计 [J]. 中国空间科学技术, 1986, (6): 45-48. |
[3] |
Zhang W, Pang B J, Zou J X, et al. Meteoroid and Space Debris Shielding Concepts for Spacecraft [J]. Journal of Harbin Institute of Technology, 1999, 32(2): 18-22. (in Chinese) |
[4] |
张伟, 庞宝君, 邹经湘, 等. 航天器微流星体及空间碎片防护方案 [J]. 哈尔滨工业大学学报1999, 32(2): 18-22. |
[5] |
Christiansen E L. Enhanced Meteoroid and Orbital Debris Shielding [J]. Int J Impact Engng, 1995, 17: 217-228. |
[6] |
Hiermaier S, Konke D, Stilp A J, et al. Computational Simulation of the Hypervelocity Impact of Al-Spheres on Thin Plates of Different Materials [J]. Int J Impact Engng, 1997, 20: 363-374. |
[7] |
Hayhurst C J, Clegg R A. Cylindrically Symmetric SPH Simulations of Hypervelocity Impacts on Thin Plates [J]. Int J Impact Engng, 1997, 20: 337-348. |
[8] |
Hayhurst C J, Hiermaier S J, Clegg R A, et al. Development of Material Models for Nextel and Kevlar-Epoxy for High Pressure and Strain Rates [J]. Int J Impact Engng, 1999, 23: 365-376. |
[9] |
AUTODYN Users Manual Revision 4. 3 [Z]. San Ramon, CA94583 USA: Century Dynamics, Incorporated, 2003. |
[10] |
Piekutowski A J. Formation and Description of Debris Cloud Produced by Hypervelocity Impact [R]. 4707, 1996. |
[11] |
Piekutowski A J. Characteristics of Debris Clouds Produced by Hypervelocity Impact of Aluminum Spheres with Thin Aluminum Plates [J]. Int J Impact Engng, 1993, 14, 573-586. |