• Title of article

    Particle launch to 19 km/s for micro-meteoroid simulation using enhanced three-stage light gas gun hypervelocity launcher techniques

  • Author/Authors

    T.F. Thornhill، نويسنده , , L.C. Chhabildas، نويسنده , , W.D. Reinhart، نويسنده , , D.L. Davidson، نويسنده ,

  • Issue Information
    روزنامه با شماره پیاپی سال 2006
  • Pages
    13
  • From page
    799
  • To page
    811
  • Abstract
    Particle launch experiments were performed to study application of the enhanced hypervelocity launcher (EHVL), i.e. the third-stage addition to the two-stage gun, for launching micron to millimeter sized particulates at velocities unobtainable with a standard two-stage light gas gun launch. Three types of particles or fliers were tested along with several barrel designs. For micron scale particles fine-grain polycrystalline ceramics were impacted and fractured, launching particulate clouds at velocities of 15 km/s. Multiple titanium particles ∼400 μm diameter embedded in plastic were “shotgun” launched to velocities of 10 km/s. Flier plates of 3 mm diameter by 1 mm thick Ti6Al4V were launched to 19 km/s. All experiments used a second-stage projectile with graded density facing impacting a flier in an impact generated acceleration reservoir. This paper describes the modification and adaptation of the Sandia EHVL to provide micrometeoroid simulation capabilities.
  • Keywords
    meteoroid , Three stage , Flier , Hypervelocity , Two stage
  • Journal title
    International Journal of Impact Engineering
  • Serial Year
    2006
  • Journal title
    International Journal of Impact Engineering
  • Record number

    1251067