Ballistic Evaluation of 19-Perforation Propellant in the 155-mm Propelling Charge, M203E1

Abstract

Top-zone propelling charges for the Army 155-mm Howitzer were manufactured using 19-perforation, M30A1, granular propellant and tested against M203E1 Propelling Charges employing standard 7-perforation propellant. Velocities, chamber pressures, pressure wave levels, and ignition delays were essentially equivalent for the two charges when fired at ambient temperatures or after cold conditioning. Significant differences in performance, however, were exhibited by the two charges when fired hot.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1979
Accession Number
ADA079896

Entities

People

  • A. W. Horst
  • J. J. Rocchio
  • J. R. Kelso
  • T. C. Minor

Organizations

  • Ballistic Research Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Artillery
  • Burning Rate
  • Combustion
  • Flow
  • Guns
  • High Temperature
  • Howitzers
  • Ignition
  • Ignition Lag
  • Low Temperature
  • Muzzle Velocity
  • Projectiles
  • Propellant Grains
  • Propellants
  • Propelling Charges
  • Temperature Coefficients
  • Weapons

Readers

  • Rocket Propulsion.