Changes in the Calorimetric Value and Ignition Temperature of Composite Solid Propellants During Ageing-A Note

  • K. Kishore Indian Institute of Science, Bangalore
  • S. Sankaralingam Indian Institute of Science, Bangalore
  • A. Sameena Begum Indian Institute of Science, Bangalore
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.

Author Biographies

K. Kishore, Indian Institute of Science, Bangalore
Indian Institute of Science, Baogalore-560 012
S. Sankaralingam, Indian Institute of Science, Bangalore
Indian Institute of Science, Bangalore-560 012
A. Sameena Begum, Indian Institute of Science, Bangalore
Indian Institute of Science, Bangalore-560-012
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
Section
General Papers

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