Temperature Sensitivity in Artillery Charge Design

Abstract

Charge design for large-caliber artillery weapons must allow for many factors which can reduce efficiency and safety when these rounds are used in field situations. One of those factors is the temperature sensitivity of the propellant -- the change in performance caused by differing initial charge temperatures in otherwise identical artillery rounds. By comparing computer simulations of interior ballistic calculations, three factors in propellant grain design are explored -- geometry, deterrent layers and ignition delay. The IBHVG2 code is used to show the effects of each factor in a typical 1200-mm gun system. Temperature-related trends are computed, and the results are compared in tables and graphs.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1991
Accession Number
ADA232239

Entities

People

  • Robert T. Puhalla
  • Ronald D. Anderson

Organizations

  • Ballistic Research Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Artillery
  • Artillery Ammunition
  • Ball Powder Propellants
  • Base Pressure
  • Burning Rate
  • Combustion
  • Computer Simulations
  • Geometry
  • Ignition
  • Ignition Lag
  • Jet Propulsion
  • Materials
  • Mechanical Engineering
  • Military Research
  • Projectiles
  • Propellant Grains
  • Propellants

Fields of Study

  • Physics

Readers

  • Computer Science.
  • Rocket Propulsion.
  • Thermal Physics or Thermal Science.