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
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