Changes in the Calorimetric Value and Ignition Temperature of Composite Solid Propellants During Ageing-A Note
Keywords: Carboxy terminated, Ammonium perchlorate propellant
AbstractCalorimetric 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.
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
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