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Investigations of Hypervelocity Impact Physics

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  • Additional Information
    • Contributors:
      Mechanical Engineering; Bayandor, Javid; Battaglia, Francine; O'Brien, Walter F. Jr.; Scales, Wayne A.; Samareh, Jamshid A.
    • Publication Information:
      Virginia Tech
    • Publication Date:
      2014
    • Collection:
      VTechWorks (VirginiaTech)
    • Abstract:
      Spacecraft and satellites in orbit are under an increasing threat of impact from orbital debris and naturally occurring meteoroids. While objects larger than 10 cm are routinely tracked and avoided, collisions inevitably occur with smaller objects at relative velocities exceeding 10 km/s. Such hypervelocity impacts (HVI) create immense shock pressures and can melt or vaporize aerospace materials, even inducing brief plasmas at higher speeds. Sacrificial shields have been developed to protect critical components from damage under these conditions, but the response of many materials in such an extreme event is still poorly understood. This work presents the summary of computational analysis methods to quantify the relevant physical mechanisms at play in a hypervelocity impact. Strain rate-dependent behavior was investigated using several models, and fluid material descriptions were used to draw parallels under high shear rate loading. The production and expansion of impact plasmas were modeled and compared to experimental evidence. Additionally, a parametric study was performed on a multitude of possible material candidates for sacrificial shield design, and new shielding configurations were proposed. A comparison of material models indicated that the Johnson-Cook and Steinberg-Cochran-Guinan-Lund metallic formulations yielded the most consistent results with the lowest deviation from experimental measures in the strain rate regime of interest. Both meshless Lagrangian and quasi-Eulerian meshed schemes approximated the qualitative and quantitative characteristics of HVI debris clouds with average measurable errors under 5%. While the meshless methods showed better resolution of interfaces and small details, the meshed methods were shown to converge faster under several metrics with fewer regions of spurious instability. Additionally, a new technique was introduced using hypothetical viscous fluids to approximate debris cloud behavior, which showed good correlation to experimental results when such models were ...
    • File Description:
      ETD; application/pdf
    • Relation:
      vt_gsexam:3605; http://hdl.handle.net/10919/95298
    • Online Access:
      http://hdl.handle.net/10919/95298
    • Rights:
      In Copyright ; http://rightsstatements.org/vocab/InC/1.0/
    • Accession Number:
      edsbas.77D18C22