Advanced Gun Propellant Concepts

Abstract

A new series of cool burning, high impetus, low molecular weight gun propellants has been identified. These propellants contain either cyclic or linear nitramines as crystalline oxidizers in the propellant matrix. Current development efforts are concentrating on lowering the inherently high pressure exponent of the linear burning rate associated with these high energy systems. When these advanced formulations become operational, thermal barrel erosion will be virtually eliminated, hypervelocity projectile firing from operational guns will become possible, and the potentiality for catastrophic failure resulting from the use of aluminum cartridges will be removed. To realize these benefits, the nitramine combustion anomaly must be obviated.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1973
Accession Number
AD0908282

Entities

People

  • Otto Heiney

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Ammunition
  • Burning Rate
  • Cartridge Cases
  • Combustion
  • Combustion Products
  • Composite Propellants
  • Energetic Materials
  • Energy
  • Equations
  • Explosives
  • Gun Propellants
  • High Energy
  • Materials Laboratories
  • Molecular Weight
  • Propellants
  • Single Base Propellants
  • Test And Evaluation

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.
  • Systems Analysis and Design
  • ballistics.

Technology Areas

  • Hypersonics