Studies of Shell Fragment Mass Distribution

Abstract

This report gives fragment mass distribution data requested by the Bureau of Ordnance for the Navy 3"/50 A.A. projectiles, Mk. 27-3 and Mk. 31-1. Part II (CSRD Report No. 5606) gives similar data for the 3"/50 A.P. projectile, Mk. 29-2. Part III (OSRD Report No. 5608) contains a preliminary investigation of the effect of booster size upon the fragment mass distribution. The experimental procedure for fragment recovery at this laboratory is described. The fragments are caught in sawdust and recovered by a magnetic separator. Methods of analyzing the data are reviewed. No attempt has been made at this time to examine the physical theory of shell break-up but the results have been described in terms of Mott's semi-empirical exponential distribution law. Physical tests made upon samples from a single lot, Lot No. 1350 of Mk. 27-3 3" A.A. projectiles showed that the shell were by no means uniform in such properties as hardness and tensile strength. It appeared that a simple hardness test could be used to eliminate sub-standard shell without rendering them unfit for use. A set of ten shell selected for uniform hardness did indeed give satisfactorily reproducible fragment mass distribution data when fragmented with cast TNT fillings. At least one additional shell from the same lot but showing subnormal hardness gave a fragment mass distribution significantly coarser than the others.

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Document Details

Document Type
Technical Report
Publication Date
Jan 05, 1946
Accession Number
ADB277452

Entities

People

  • D. P. Macdougall
  • J. F. Lemons
  • M. A. Paul
  • W. K. Hall

Tags

DTIC Thesaurus Topics

  • Chi Square Test
  • Detonators
  • Diameters
  • Equations
  • Explosives
  • Metals
  • Munitions
  • Ordnance Laboratories
  • Physical Properties
  • Plastic Explosives
  • Projectiles
  • Radio Proximity Fuzes
  • Rotating Bands
  • Separators
  • Square Roots
  • Standards
  • Tensile Strength

Readers

  • Aerosol Science/Aerosol Physics
  • Materials Science (Mechanical Engineering).
  • Rocket Propulsion.