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

Authors

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

DOI:

https://doi.org/10.14429/dsj.36.5991

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

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Published

2014-01-21

How to Cite

Kishore, K., Sankaralingam, S., & Begum, A. S. (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

Vol. 36 No. 4

Section

General Papers

License

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