Changes in the Calorimetric Value and Ignition Temperature of Composite Solid Propellants During Ageing-A Note
Keywords:
Carboxy terminated, Ammonium perchlorate propellant
Abstract
Calorimetric value and ignition temperature of carboxy terminated polybutadiene/ammonium perchlorate propellant decrease during accelerated ageing. The behaviour has been explained on account of binder loss and condensed phase reactions in the propellant matrix.
Published
2014-01-21
How to Cite
Kishore, K., Sankaralingam, S., & Begum, A. (2014). Changes in the Calorimetric Value and Ignition Temperature of Composite Solid Propellants During Ageing-A Note. Defence Science Journal, 36(4), 425-428. https://doi.org/10.14429/dsj.36.5991
Issue
Section
General Papers
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