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Solid propellants burning enhancement using foil embedding method

Published online by Cambridge University Press:  03 February 2016

H. G. Darabkhanid  and
N. S. Mehdizadeh
H. G. Darabkhanid
Affiliation:
Aerospace Engineering Department, Amirkabir University of Technology, Centre of Excellence in Computational Aerospace Engineering, Tehran, Iran
N. S. Mehdizadeh
Affiliation:
Aerospace Engineering Department, Amirkabir University of Technology, Centre of Excellence in Computational Aerospace Engineering, Tehran, Iran
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Abstract

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The method of metal embedding is widely employed in solid propellant motors with end-burning configuration, thereby significantly improving the burning rate of the propellants. In this study, the cylindrical foil embedding method is applied to double-base solid propellant, as a new method, and the effects of the type and thickness of the foil on the burning surface, as well as the burning rate, are experimentally investigated. It is shown that by using the foil embedding method, the burning characteristics of solid propellants can be improved. Results have been compared to some available data. To the best of the author’s knowledge there are no published data available on this method.

Information

Type
Research Article
Information
The Aeronautical Journal , Volume 112 , Issue 1138 , December 2008 , pp. 725 - 732
Copyright
Copyright © Royal Aeronautical Society 2008 

References

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