Morrison R H. A preliminary investigation of projectile shape effects in hypervelocity impact of a double-sheet structure, NASA TN D-6944 [R]. Washington D C: National Aeronautics and Space Administration, 1972.
[2]
Christiansen E L, Justin H K. Projectile shape effects on shielding performance at 7 km/s and 11 km/s [J]. Int J Impact Eng, 1997, 20(1-5): 165-172.
[3]
Hu K, Schonberg W P. Ballistic limit curves for non-spherical projectiles impacting dual-wall spacecraft systems [J]. Int J Impact Eng, 2003, 29(1-10): 345-355.
[4]
Thornhill T F, Chhabildas L C, Reinhart W D, et al. Particle launch to 19 km/s for micro-meteoroid simulation using enhanced three-stage light gas gun hypervelocity launcher techniques [J]. Int J Impact Eng, 2006, 33(1): 799-811.
[5]
Protection manual, IADC-WD-00-03 [R]. Inter-Agency Space Debris Coordination Committee, 2008.
[6]
Zhang W, Pang B J, Luo D K, et al. Investigation into material state characterization of debris cloud created by cylindrical projectile impact on bumper [J]. Chinese Space Science and Technology, 2001, 3: 53-59. (in Chinese)
Ma W L, Zhang W, Guan G S, et al. Numerical simulation of debris cloud produced by ellipsoidal projectile hypervelocity impact on bumper [J]. Materials Science & Technology, 2005, 13(3): 294-298. (in Chinese)
Zhang W, Ma W L, Guan G S, et al. Numerical simulation of non-spherical projectiles hypervelocity impact on spacecraft shield configuration [J]. Explosion and Shock Waves, 2007, 27(3): 240-245. (in Chinese)
Xu J Z. Research on the characteristics of debris clouds produced by hypervelocity impacts of space debris and the design and optimization of the shielding structure using SPH method [D]. Changsha: National University of Defense Technology, 2008: 120-133. (in Chinese)
Schonberg W P, Williamsen J E. RCS-based ballistic limit curves for non-spherical projectiles impacting dual-wall spacecraft systems [J]. Int J Impact Eng, 2006, 33(1-12): 763-770.
[15]
Williamsen J E, Evans S W. Predicting orbital debris shape and orientation effects on spacecraft shield ballistic limits based on characteristic length [J]. Int J Impact Eng, 2006, 33(1-12): 862-871.
[16]
Williamsen J E, Schonberg W P, Evans H, et al. A comparison of NASA, DoD, and hydrocode ballistic limit predictions for spherical and non-spherical shapes versus dual- and single-wall targets, and their effects on orbital debris penetration risk [J]. Int J Impact Eng, 2008, 35(12): 1870-1877.
[17]
Liou J C, Matney M J, Phillip D, et al. The new NASA orbital debris engineering model ORDEM2000, NASA/TP-2002-210780 [R]. USA: NASA Johnson Space Center, 2002.
[18]
Mcnight D S, Johnson N L, Fudge M L, et al. Satellite orbital debris characterization impact test (SOCIT) series data collection report, NAS 9-19215 [R]. Colorado Springs, CO, USA: Kaman Sciences Corporation, 1995.
