The Kinetics and Thermochemistry of the Thermal Decomposition of the Initiating Explosive, Tetrazene, near its Ignition Temperature (between 385 K and 400 K).

Abstract

The efficient explosive pick-up of the AMRL gasless cap composition based on boron / Pb3O4 / tetrazene and of many in-service stab and percussion- sensitive compositions based on primary explosive lead salts mixed with tetrazene arises from the explosive behaviour of tetrazene and its functioning as an energetic sensitizer. Using the thermoanalytical techniques of differential scanning calorimetry and thermogravimetry, it was established that tetrazene decomposes in a series of steps, close to its ignition temperature, ca. 140 deg C (413 K); initially, it softens, then it decomposes exothermically in a two-stage process, the first and main stage following an autocatalytic rate law of the form d(a)/dt = k2 a(1 - a). where a is the degree of reaction in this first stage, and t, the time. From an analysis of the kinetics carried out between 387.9 K and 398 K, it has been shown that the kinetics follow an Arrhenius rate dependency, leading to an activation energy (which can be related to the energetics in the bond-breaking processes) of 185.4 kJ/ mol and a preexponential factor, related to the entropy of the reaction, In A (/min), of 56.23.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1996
Accession Number
ADA322325

Entities

People

  • Daniel J. Whelan
  • Mark R. Fitzgerald

Organizations

  • Defence Science and Technology Group

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Calorimetry
  • Chemical Kinetics
  • Chemical Reactions
  • Chemistry
  • Department Of Defense
  • Energetic Materials
  • Energy
  • Equations
  • Explosives
  • Gravimetric Analysis
  • Heat Of Activation
  • Insensitive Explosives
  • Materials
  • Munitions
  • Organic Chemistry
  • Organic Compounds
  • Thermochemistry

Fields of Study

  • Materials science

Readers

  • Combustion science or combustion engineering.
  • Rocket Propulsion.