Megabar Liner Experiments on Pegasus II

Abstract

Using pulsed power to implode a liner onto a target can produce high shock pressures for many interesting application experiments. With the Pegasus II facility in Los Alamos, a detailed theoretical analysis has indicated that the highest attainable pressure is around 2 Mbar for a best designed aluminum liner. Recently, an interesting composite liner design has been proposed which can boost the shock pressure performance by a factor 4 over the aluminum liner. This liner design was adopted in the first megabar (Megarbar- 1) liner experiment carried out on Pegasus last year to verify the design concept and to compare the effect of Rayleigh-Taylor instabilities on liner integrity with the code simulations. We present briefly the physical explanation why the composite liner provides the best shock pressure performance. The theoretical modeling and performance of Megabar- 1 liner are discussed. Also presented are the first experimental results and the liner design modification for our next experiment.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1997
Accession Number
ADA640506

Entities

People

  • D. Platts
  • D. W. Scudder
  • Hanwool Lee
  • Henn Oona
  • J. Cochrane
  • J. Stokes
  • L. Veeser
  • M. Rich
  • R. E. Chrien
  • R. L. Bowers
  • R. R. Bartsch
  • W. Broste
  • W. R. Shanahan
  • Walter L. Atchison
  • William Anderson

Organizations

  • Los Alamos National Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aluminum
  • Buildings And Structures
  • Collisions
  • Composite Materials
  • Electrodes
  • Elements
  • High Density
  • Implosions
  • Instability
  • Materials
  • Melting Point
  • Metals
  • Pulsed Power
  • Radial Stress
  • Rayleigh Taylor Instability
  • Simulations
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Pulsed Power and Plasma Physics.