Polyurethane Based Inhibition for High Flame Temperature Nitramine Based Composite Modified Double Base propellant
Keywords: Inhibition systems, Propellant inhibition bond strength
AbstractThe findings for polypropylene glycol (PPG) and hydroxyl-terminated polybutadiene (HTPB)-based inhibition systems are reported. These findings established that the inhibition system comprising HTPB-IPDI-IDP binder and Sb/sub 2/O/sub 3/-C black filler is most suitable for advanced nitramine-based composite modified double-base propellants in terms of mechanical properties and processibility. The promising composition was characterised for glass-transition behaviour and propellant-inhibition bond strength. Propellant grains inhibited with selected formulations were subjected to static evaluation at extreme temperatures and limited aging studies to obtain data of practical value.
How to Cite
Kakade, S., Vaidya, M., Khangaonkar, D., Divekar, P., Kadam, U., & Asthana, S. (2013). Polyurethane Based Inhibition for High Flame Temperature Nitramine Based Composite Modified Double Base propellant. Defence Science Journal, 48(4), 371-377. https://doi.org/10.14429/dsj.48.3964
Chemical Science & Technology
Copyright (c) 2016 Defence Science Journal
where otherwise noted, the Articles on this site are licensed under Creative Commons License: CC Attribution-Noncommercial-No Derivative Works 2.5 India