Christiansen E L. Meteroroid/Debris Shielding, NASA TP-2003-210788 [R]. USA: NASA Johnson Space Center, 2003.
[2]
Gong Z Z, Shi S C, Yang J Y, et al. A New Projectile/Sabot Aerodynamic Separating Technique in Hypervelocity Impact Experiments [J]. Spacecraft Environment Engineering, 2008, 25(3): 259-262. (in Chinese)
Piekutowski A J, Poormon K L. Development of a Three-Stage, Light-Gas Gun at the University of Dayton Research Institute [J]. Int J Impact Eng, 2006, 33(1-12): 615-624.
[5]
Chhabildas L C, Baker L M, Asay J R, et al. Launch Capabilities to over 10 km/s [A]//Schmidt S C, Dick R D, Forbes J W, et al. Shock Waves in Condensed Matter-1991 [C]. Amsterdam: North Holland, 1992: 1025-1031.
[6]
Chhabildas L C, Dunn J E, Reinhart W D, et al. An Impact Technique to Accelerate Flier Plates to Velocities over 12 km/s [J]. Int J Impact Eng, 1993, 14(1-4): 121-132.
[7]
Chhabildas L C, Kmetyk L N, Reinhart W D, et al. Launch Enhanced Hypervelocity Launcher-Capabilities to over 16 km/s [J]. Int J Impact Eng, 1995, 17(1-4): 183-194.
[8]
Walker J D, Grosch D J, Mullin S A. Experimental Impacts above 10 km/s [J]. Int J Impact Eng, 1995, 17(4-6): 903-914.