AN IMPACT AND PENETRATION EFFECTS STUDY

Abstract

The Shaped Charge Hypervelocity Projectile Accelerator is being used to study impact and penetration effects upon various thicknesses of targets at velocities between 24,000 and 39,000 feet per second. This report presents and analyzes 208 data points gathered for impacts in the 29,000-33,000 fps velocity range, with 0.03-0.8 gram aluminum projectiles against 0.375-inch, 0. 500-inch, 1.00-inch and 4.0-inch thick 2024-T4 aluminum target plates; 19 data points gathered for impacts in the 35,00039,000 fps velocity range with 0.01-0.7 gram aluminum projectiles against 0.100-inch thick 2024-T4 aluminum target plates; and 63 data points gathered for impacts in the 22,00026,000 fps velocity range with 0.02-0.7 gram copper projectiles against 0.100-inch thick 2024-T4 aluminum target plates and 0.500-inch thick soft copper target plates. Angles of obliquity between the velocity and the target surface for these experiments were 90, 50 and 20 degrees. Curves, photographs, and flash radiographs illustrating the data are presented.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1963
Accession Number
AD0295595

Entities

People

  • J. E. Ferguson

Organizations

  • Aerojet Rocketdyne Holdings

Tags

DTIC Thesaurus Topics

  • Air Force
  • Ballistics
  • Cameras
  • Craters
  • Explosives
  • Government Procurement
  • Governments
  • Hypervelocity Projectiles
  • Instrumentation
  • Measurement
  • Munitions
  • Photographs
  • Projectiles
  • Shaped Charges
  • Target Angle
  • Terminal Ballistics
  • Thickness

Fields of Study

  • Physics

Readers

  • Explosive Engineering.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow