An alternative approach to improve burning rate characteristics and processing parameters of composite propellant

Volume: 209, Pages: 357 - 362
Published: Nov 1, 2019
Abstract
null null Modification in burn rate of composite solid propellant has become a necessity of a mission. Burn rate can be modified by various mean viz. (i) tailoring the ammonium perchlorate (AP) particle size, (ii) use of nano-sized particles and (iii) incorporating burn rate modifiers. Literature discusses about various burn rate modifiers. Out of these, Iron oxide (Fe2O3)/IO is the well known burn rate enhancer. Here a systematic study was...
Paper Details
Title
An alternative approach to improve burning rate characteristics and processing parameters of composite propellant
Published Date
Nov 1, 2019
Volume
209
Pages
357 - 362
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