FUNDAMENTALS OF LIQUID PROPELLANT SENSITIVITY

Abstract

In tests with Compound T, using nitrogen driven gas shocked to reflected temperatures about 1150 K, the corresponding changes in time for induction delay and sample consumption for increases in reflected-shock pressure from 500 to 1500 psia were 400 to 50 and near zero to 500 microseconds, respectively. Although the induction time decreases at higher pressure the decreased consumption rate indicates a relatively slow-burning that is an improvement in explosion sensitivity. A vaporization mechanism which appears to be inhibited by high external pressure was proposed to be a rate-controlling step in the explosion transition of most CNF type compounds that were studied to date. In additional experiments, explosions were simulated by spark discharges so as to verify certain characteristics of the light and pressure sensors as used in shock-tube sensitivity testing of cryogenic compounds. Efforts to characterize the vaporization of inert freons were only partly successful.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1966
Accession Number
AD0823599

Entities

People

  • Allen J. Tulis
  • Ted A. Erikson

Organizations

  • IIT Research Institute

Tags

Communities of Interest

  • Energy and Power Technologies
  • Sensors
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Chemical Reactions
  • Chemistry
  • Explosions
  • Explosives
  • Frequency
  • Instrumentation
  • Lead Azides
  • Liquid Propellants
  • Mass Transfer
  • Materials Laboratories
  • Materials Science
  • Plastic Explosives
  • Rocket Propulsion
  • Shock Tubes
  • Shock Waves

Readers

  • Combustion science or combustion engineering.
  • Fluid Dynamics.