An alternative approach to improve burning rate characteristics and processing parameters of composite propellant-Reference-Cited by-同舟云学术

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An alternative approach to improve burning rate characteristics and processing parameters of composite propellant

Published:2019-11 Issue: Volume:209 Page:357-362
ISSN:0010-2180
Container-title:Combustion and Flame
language:en
Short-container-title:Combustion and Flame

Author:

Sangtyani Rekha,Saha Himadri S.,Kumar Amit,Kumar Arvind,Gupta Manoj,Chavan Prakash V.

Publisher

Elsevier BV

Subject

General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry

Reference32 articles.

1. Propellant and Explosives;Kubota,2002

2. Effect of transition metal oxides on decomposition and deflagration of composite solid propellant systems: a survey;Kishore;AIAA J.,1979

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

4. Combutsion characteristics of AP/CTPB propellant with burning rate modifiers;Krishnan;J. Propuls. Power,1992

5. Action of transition metal oxides on composite solid propellant;Kishore;AIAA J.,1980

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