Comparison of burn rate and thermal decomposition of AP as oxidizer and PVC and HTPB as fuel binder based composite solid propellants-Reference-Cited by-同舟云学术

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Comparison of burn rate and thermal decomposition of AP as oxidizer and PVC and HTPB as fuel binder based composite solid propellants

Published:2019-04 Issue:2 Volume:15 Page:227-232
ISSN:2214-9147
Container-title:Defence Technology
language:en
Short-container-title:Defence Technology

Author:

Manash A.,Kumar P.

Publisher

Elsevier BV

Subject

Metals and Alloys,Mechanical Engineering,Ceramics and Composites,Computational Mechanics

Reference13 articles.

1. Effect of transition metal oxides on decomposition and deflagration of composite solid propellant systems;Kishore;AIAA J,1986

2. Chemistry and kinetics of HTPB and Diisocyanate-HTPB polymers during slow decomposition and combustion - like conditions;Brill;Combust Flame,1991

3. The effect of pressure and additives on the kinetics of decomposition of AP;Weashe,1967

4. A review on the decomposition/deflagration of oxidizer and binder in composite solid propellant;Kishore;Defence Sci J,1978

5. The mechanism of burning rate catalysis in composite HTPB- AP propellant combustion;Fong;Combust Flame,1986

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