Ignition Times of Composite Propellants Based on Nitrophenolic Binders

H. L. GIRDHAR Department of Chemistry, University of Kashmir, Srinagar, 190006, India

A. J. ARORA Department of Chemistry, University of Kashmir, Srinagar, 190006, India

G. N. MALIK Department of Chemistry, University of Kashmir, Srinagar, 190006, India

Abstract

Ignition times for composite propellants containing nitrophenolic resins as fuel binders and NH₄ClO₄ or KClO₄ as oxidizers are measured by the hot plate technique. Activation energies of ignition process are calculated using thermal explosion theory. The results show the possibility of two different mechanisms of ignition process depending upon the heating temperature.

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Ignition Times of Composite Propellants Based on Nitrophenolic Binders

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Ignition Times of Composite Propellants Based on Nitrophenolic Binders

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