Development of Novel Polynitrogen-Based High-Performance Solid Propellants

Abstract

In this STTR program, CFDRC, in collaboration with the University of Idaho, proposed to develop some novel high-performance polynitrogen energetic materials for propellant applications. As a proof-of-concept, we synthesized a number of promising high energy amine substituted tetrazole based compounds. These compounds were first theoretically investigated to obtain their heats of formation, densities, specific impulses, detonation pressures and velocities. The synthesized compounds were characterized, and densities, melting points and impact sensitivities were measured in the laboratory. Some of these compounds have remarkably low impact sensitivities. We conclude that at least five compounds have excellent potential for use a propellant ingredient. Impact sensitivities were further measured in a mixture of ammonium nitrate. We observed that a small percentage of ammonium nitrate improves the impact sensitivities further while improving the oxygen balance. In Phase II, these compounds will be formulated, and undergo a rigorous set of tests, such as burn rate, compatibility, mechanical strength, to evaluate their performance in practical situations.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 2009
Accession Number
ADA522116

Entities

People

  • Debasis Sengupta
  • Jean'ne Shreeve

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Ammonium Nitrate
  • Chemical Properties
  • Chemical Synthesis
  • Chemistry
  • Computer Programs
  • Elements
  • Energetic Materials
  • High Energy
  • Materials
  • Materials Laboratories
  • Melting Point
  • Neural Networks
  • Organic Chemistry
  • Propellants
  • Rocket Oxidizers
  • Solid Propellants
  • Specific Impulse

Readers

  • Computational Fluid Dynamics (CFD)
  • Organic Chemistry
  • Rocket Propulsion.