Volume 28 Issue 3
Jun 2015
Turn off MathJax
Article Contents
WANG Qing-Song, WANG Xiang, HAO Long, DAI Cheng-Da, BAI Jin-Song, TAN Hua. Progress on Hypervelocity Launcher Techniques Using a Three-Stage Gun[J]. Chinese Journal of High Pressure Physics, 2014, 28(3): 339-345. doi: 10.11858/gywlxb.2014.03.012
Citation: WANG Qing-Song, WANG Xiang, HAO Long, DAI Cheng-Da, BAI Jin-Song, TAN Hua. Progress on Hypervelocity Launcher Techniques Using a Three-Stage Gun[J]. Chinese Journal of High Pressure Physics, 2014, 28(3): 339-345. doi: 10.11858/gywlxb.2014.03.012

Progress on Hypervelocity Launcher Techniques Using a Three-Stage Gun

doi: 10.11858/gywlxb.2014.03.012
  • Received Date: 10 Nov 2012
  • Rev Recd Date: 15 Feb 2013
  • A study on hypervelocity launcher techniques was carried out on the two-stage light-gas gun with quasi-isentropic compression of the flier-plate material with graded impedance.A 25-millimeter diameter aluminum alloy projectile was accelerated over 11 km/s using the hypervelocity launcher, and a 10-millimeter diameter titanium alloy projectile was accelerated over 15 km/s using the enhanced hypervelocity launcher.The hypervelocity launcher techniques using a three-stage gas gun was suitable for researches on the hypervelocity impact effect of spacecrafts.

     

  • loading
  • [1]
    Palmieri D, Schafer F, Hiermaier S, et al. Numerical simulation of non-perforation impacts on shielded gas-filled pressure vessels[J]. Int J Impact Eng, 2001, 26: 591-602. doi: 10.1016/S0734-743X(01)00119-1
    [2]
    龚自正, 韩增尧, 庞宝君.空间碎片防护研究现状与国内发展建议[J].航天器环境工程, 2010, 27(1): 24-31.

    Gong Z Z, Hand Z Y, Pang B J. A historical review and some suggestions on Chinese space technology[J]. Spacecraft Environment Engineering, 2010, 27(1): 24-31. (in Chinese)
    [3]
    闽桂荣, 肖名鑫.防止微流星体击穿航天器舱壁的可靠性设计[J].中国空间科学技术, 1986, 7(6): 45-48.

    Min G R, Xiao M X. Reliability design spacecraft module wall against meteoroid perforation[J]. Chinese Space Science and Technology, 1986, 7(6): 45-48. (in Chinese)
    [4]
    Hayhurst C J, Clegg R A. Cylindrically symmetric SPH simulation of the hypervelocity impact on thin plates[J]. Int J Impact Eng, 1997, 20: 337-348. doi: 10.1016/S0734-743X(97)87505-7
    [5]
    张伟, 庞宝君, 贾斌, 等.弹丸超高速撞击防护碎片云数值模拟[J].高压物理学报, 2004, 18(1): 47-52. http://www.cqvip.com/Main/Detail.aspx?id=9280194

    Zhang W, Pang B J, Jia B, et al. Numerical simulation of debris cloud produced by hypervelocity impact of projecttile on bumper[J]. Chinese Journal of High Pressure Physics, 2004, 18(1): 47-52. (in Chinese) http://www.cqvip.com/Main/Detail.aspx?id=9280194
    [6]
    Winfree N A, Chhabildas L C, Reinhart W D. EOS data of Ti-6Al-4V to impact velocities of 10.4 km/s on a three-stage gun[C]//Furnish M D, Thadhani N N, Horie Y. Shock Compression of Condensed Matter-2001. New York: AIP, 2002: 75-78.
    [7]
    柏劲松, 谭华, 李平, 等.阻抗梯度飞片加载下的超高速发射二维数值模拟方法[J].计算物理, 2004, 21(7): 305-310.

    Bai J S, Tan H, Li P, et al. Numerical simulation method for 2D hypervelocity launcher under the graded densty impactor drives[J]. Chinese Journal of Computational Physics, 2004, 21(7): 305-310. (in Chinese)
    [8]
    林绍明, 徐南仙, 陈栋泉.超高速发射装置数值模拟[J].高压物理学报, 2000, 14(2): 139-145.

    Lin S M, Xu N X, Chen D Q. Numerical simulation of hypervelocity launchers[J]. Chinese Journal of High Pressure Physics, 2000, 14(2): 139-145. (in Chinese)
    [9]
    Wang C B, Shen Q, Zhang L M. A flier-plate material with graded impedance used in dynamic high-pressure physics[J]. Journal of Wuhan University of Technology-Mater, 2002, 17(4): 32-35. doi: 10.1007/BF02838412
    [10]
    王青松, 王翔, 戴诚达, 等.三级炮加载技术在超高压状态方程研究中的应用[J].高压物理学报, 2010, 24(3): 187-191.

    Wang Q S, Wang X, Dai C D, et al. Research on EOS at extremely high pressure using a three-stage gas gun hypervelocity launcher techniques[J]. Chinese Journal of High Pressure Physics, 2010, 24(3): 187-191. (in Chinese)
    [11]
    沈强, 张联盟, 王传彬, 等.梯度飞片材料的波阻抗分布设计与优化[J].物理学报, 2003, 52(7): 1663-1667.

    Shen Q, Zhang L M, Wang C B, et al. Design and optimization of wave impedance distribution for flyer materials[J]. Acta Phys Sin, 2003, 52(7): 1663-1667. (in Chinese)
    [12]
    沈强, 王传彬, 张联盟, 等.为实现准等熵压缩的波阻抗梯度飞片的实验研究[J].物理学报, 2002, 51(8): 1759-1763.

    Shen Q, Wang C B, Zhang L M, et al. A study on generating quasi-isentropic compression via graded impedance flyer[J]. Acta Phys Sin, 2002, 51(8): 1759-1763. (in Chinese)
    [13]
    Chhabildas L C, Kmetyk L N, Reinhart W D, et al. Enhanced hypervelocity launcher-capabilities to 16 km/s[J]. Int J Impact Eng, 1995, 17(1/2/3): 183-194.
    [14]
    Timothy G T, Chhabildas L C. Computational design of hypervelocity launchers[J]. Int J Impact Eng, 1995, 17(4/5/6): 849-860.
    [15]
    柏劲松, 华劲松, 胡建波, 等.超高速发射实验及数值分析[J].应用力学学报, 2008, 25(2): 177-181.

    Bai J S, Hua J S, Hu J B, et al. Experimental research and numerical analysis for hypervelocity lauch[J]. Chinese Journal of Applied Mechanics, 2008, 25(2): 177-181. (in Chinese)
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Figures(7)  / Tables(1)

    Article Metrics

    Article views(7315) PDF downloads(279) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return