The Mechanical Behavior of Gun Propellant Grains in Interior Ballistics.

Abstract

The interior ballistics problem associated with the erratic and adnormal burning of gun propellant grains is addressed interms of the mechanical behavior of the propellant. Compressive mechanical properties, grain failure, and burning performance of two triple base propellants tested as a strain rate of 1000% per second and at ambient temperatures ranging from 20 C to -60 C are presented. As the test temperature is lowered the propellants undergo a change from ductile to brittle mechanical stress-strain behavior; the associated grain failure proceeds with a decrease in the amount of plastic nonfragmenting type deformation and an increase in the extend of fragmenting type fracture. The extent of fracture or breakup changes the prescribed surface area of the characteristics of the propellant design. Closed bomb tests with normal and with mechanically-failed grains show increases in relative quickness sufficient to produce unsafe gun firing conditions. Changes in the mechanical properties of nitroguanidine propellants observed over a period of 1 year suggest that aging can cause propellant embrittlement.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1982
Accession Number
ADA117011

Entities

People

  • D. A. Wiegand
  • James O. Pinto
  • S. Nicolaides

Organizations

  • United States Army Armament Research, Development and Engineering Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Ballistics
  • Closed Bomb Tests
  • Compression
  • Compressive Strength
  • Ductile Brittle Transition
  • Embrittlement
  • Glass Transition Temperature
  • Gun Propellants
  • Interior Ballistics
  • Material Degradation Processes
  • Materials Laboratories
  • Measurement
  • Mechanical Properties
  • Propellant Grains
  • Propellants
  • Transition Temperature
  • Triple Base Propellants

Fields of Study

  • Physics

Readers

  • Explosive Engineering.
  • Powder metallurgy of Titanium alloys.
  • Rocket Propulsion.