A STUDY OF THE FUNDAMENTALS OF LIQUID PROPELLANT SENSITIVITY

Abstract

Preliminary sensitivity tests of lead azide samples, with initial temperatures to -170 C, were performed in the new cryogenic IITRI shocktube facility. Detonations were generally identified within 200 microseconds of the time that incident Mach 2.6 nitrogen shocks were reflected from the surface of the sample. Two characteristic induction periods were noted. The first period can be considered typical. The second period exhibited an increasing light output which stabilizes. Subsequent light output jumps instantaneously and work output follows within 10-20 microseconds. An appreciable sensitivity increase was identified with traces of air (oxygen) in the driven gas and lowered initial azide sample temperatures of 200 C; at otherwise constant conditions time delays decreased by factors of 10 and 2.

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Document Details

Document Type
Technical Report
Publication Date
Mar 10, 1964
Accession Number
AD0437384

Entities

People

  • Ted Erikson

Organizations

  • IIT Research Institute

Tags

Communities of Interest

  • Counter IED
  • Energy and Power Technologies
  • Sensors

DTIC Thesaurus Topics

  • Air Force
  • Azides
  • Decomposition
  • Detectors
  • Detonations
  • Energy Bands
  • Explosions
  • Explosives
  • Instrumentation
  • Lead Azides
  • Liquid Propellants
  • Materials Science
  • Nitrogen
  • Propellants
  • Sensitivity
  • Shock Tubes
  • Tubes

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Combustion science or combustion engineering.
  • Mathematics or Statistics