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)
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)
Christiansen E L. Enhanced Meteoroid and Orbital Debris Shielding [J]. Int J Impact Eng, 1995, 17: 217-228.
[6]
Gehring J W. Engineering Considerations [A]. //Kinslow R. High-Velocity Impact Phenomena [C]. New York: Academic Press, 1970: 463-512.
[7]
Hayashida K B, Robinson J H. Single Wall Penetration Equations [R]. NASA-CR 3190, 1983: 8-12.
[8]
Christiansen E L, Cykowski E, Ortega J. Highly Oblique Impact into Thick and Thin Targets [J]. Int J Impact Eng, 1993, 14: 157-168.
[9]
Hayhurst C J, Ranson H J, Gardner D J, et al. Modelling of Micro-Particle Hypervelocity Oblique Impacts on Thick Targets [J]. Int J Impact Eng, 1995, 17: 375-386.
[10]
AUTODYN Users Manual Revision 4. 3 [CP]. San Ramon, CA94583 USA: Century Dynamics, Incorporated, 2003.
