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ZHAO Shi-Cao, SONG Zhen-Fei, JI Guang-Fu, GONG Zi-Zheng, ZHAO Xiao-Ping. A Novel Design of a Hypervelocity Launcher Based on Two-Stage Gas Gun Facilities[J]. Chinese Journal of High Pressure Physics, 2011, 25(6): 557-564. doi: 10.11858/gywlxb.2011.06.012
Citation: ZHAO Shi-Cao, SONG Zhen-Fei, JI Guang-Fu, GONG Zi-Zheng, ZHAO Xiao-Ping. A Novel Design of a Hypervelocity Launcher Based on Two-Stage Gas Gun Facilities[J]. Chinese Journal of High Pressure Physics, 2011, 25(6): 557-564. doi: 10.11858/gywlxb.2011.06.012

A Novel Design of a Hypervelocity Launcher Based on Two-Stage Gas Gun Facilities

doi: 10.11858/gywlxb.2011.06.012
  • Received Date: 09 Sep 2010
  • Rev Recd Date: 21 Jan 2011
  • Issue Publish Date: 15 Dec 2011
  • A new scheme of hypervelocity launcher was put forward in this paper by means of strong detonation. An explosive ring was fixed internally in a specially designed third-stage barrel in which the projectile launched by two-stage gas gun at velocity ranging from 6 to 7 km/s was able to be accelerated subsequently to a hypervelocity of 10 km/s or so. Based on hydrocode simulations, the shape of flyer and explosive ring was optimally designed. In addition, through the encapsulation of the sphere projectile by epoxy resin, the projectile damages resulted both from detonation-induced jet and spalling due to the characteristic of short pressure pulse imposed on centimeter-sized projectiles would be suppressed. The simulations illustrate that the optimized hypervelocity launcher has the capability of accelerating 1.03 g aluminum alloy projectile with a velocity of 6 km/s to 9.6 km/s, keeping the sphere-like shape with the velocity amplification ratio of 1.6.

     

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  • Christiansen E L. Meteroroid/Debris Shielding, NASA TP-2003-210788 [R]. USA: NASA Johnson Space Center, 2003.
    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)
    龚自正, 施尚春, 杨继远, 等. 一种用于超高速撞击实验的新型弹丸弹托分离技术 [J]. 航天器环境工程, 2008, 25(3): 259-262.
    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.
    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.
    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.
    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.
    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.
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