Ignition and Combustion of Liquid Propellants

Abstract

A comprehensive experimental program has been conducted to gain fundamental understanding on the gasification and microexplosion characteristics of droplets of water-based liquid gun propellants consisting of hydroxylammonium nitrate and triethanol ammonium nitrate, under atmospheric as well as elevated pressures. Results demonstrate that the propellant microexplosion temperature is around 200 C and is substantially in excess of previously reported values, that liquid-phase reaction plays a key role in the droplet gasification characteristics, and that increasing the environment pressure increases the droplet gasification rate and advances the onset of droplet microexplosion. Keywords: Liquid propellants, Ignition, Droplet combustion, Microexplosion.

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Document Details

Document Type
Technical Report
Publication Date
Jan 15, 1990
Accession Number
ADA224150

Entities

People

  • Chung K. Law

Organizations

  • University of California

Tags

Communities of Interest

  • C4I
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Barometric Pressure
  • Burning Rate
  • Chambers
  • Chemical Analysis
  • Chemical Reactions
  • Combustion
  • Combustion Chambers
  • Decomposition
  • Fluids
  • Gun Propellants
  • High Pressure
  • Ignition
  • Liquid Gun Propellants
  • Liquid Phases
  • Liquid Propellants
  • Liquids
  • Propellants

Fields of Study

  • Chemistry
  • Environmental science

Readers

  • Combustion science or combustion engineering.
  • Rocket Propulsion.