Low Pressure Burning of Ammonium Perchlorate Composite Propellants-Reference-Cited by-同舟云学术

Low Pressure Burning of Ammonium Perchlorate Composite Propellants

Published:1986-05 Issue:1-2 Volume:47 Page:81-91
ISSN:0010-2202
Container-title:Combustion Science and Technology
language:en
Short-container-title:Combustion Science and Technology

Author:

KUWAHARA T.,KUBOTA N.

Publisher

Informa UK Limited

Subject

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

Link

http://www.tandfonline.com/doi/pdf/10.1080/00102208608923866

Reference13 articles.

1. A model of composite solid-propellant combustion based on multiple flames

2. A Model of Composite Propellant Combustion Including Surface Heterogeneity and Heat Generation

3. DISSOCIATION PRESSURE OF AMMONIUM PERCHLORATE1

4. Kubota , N. , Kuwahara , T. , Miyazaki , S. , Uchiyama . K. , and Hirata , N. ( 1984 ).Combustion wave structures of ammonium perchlorate composite propellants. AIAA Paper 84 – 1435 .

Cited by 17 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Survey of Low-Burn-Rate Solid Rocket Propellants;Innovative Energetic Materials: Properties, Combustion Performance and Application;2020

2. Combustion performance studies of aluminum and boron based composite solid propellants in sub-atmospheric pressure regimes;Propulsion and Power Research;2019-12

3. Environmentally safe (chlorine-free): new green propellant formulation based on 2,2,2-trinitroethyl-formate and HTPB;RSC Advances;2018

4. Combustion of Composite Propellants;Propellants and Explosives;2015-03-13

5. Effect of binders on the burning rate of AP composite propellants;PROPELL EXPLOS PYROT;2000