Influence of iron oxide on thermal decomposition behavior and burning characteristics of ammonium nitrate/ammonium perchlorate-based composite propellants-Reference-Cited by-同舟云学术

Influence of iron oxide on thermal decomposition behavior and burning characteristics of ammonium nitrate/ammonium perchlorate-based composite propellants

Published:2018-06 Issue: Volume:192 Page:10-24
ISSN:0010-2180
Container-title:Combustion and Flame
language:en
Short-container-title:Combustion and Flame

Author:

Kohga Makoto^ORCID,Togo Shimpei

Publisher

Elsevier BV

Subject

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

Reference46 articles.

1. Oxidizer coarse-to-fine ratio effect on microscale flame structure in a bimodal composite propellant;Isert;Combust. Flame,2016

2. Near-surface flame structure characterization of simplified ammonium perchlorate/hydroxyl-terminated polybutadiene compositions;Isert;Combust. Flame,2016

3. Burning rate of AP/HTPB base-bleed composite propellant under free ambient pressure;Zhang;Aerosp. Sci. Technol.,2017

4. Combustion mechanism of composite solid propellant sandwiches containing nano-aluminium;Gnanaprakash;Combust. Flame,2017

5. The effect of decorated graphene addition on the burning rate of ammonium perchlorate composite propellants;Isert;Combust. Flame,2017

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