Experimental Study on a Triple-base Propellant Formulation

DOI

10.2991/icmit-16.2016.140How to use a DOI?

Keywords

triple-base propellant, solvent ratio, formula, shrinking percentage

Abstract

In order to optimize the triple-base propellant's preparation technology and improve the combustion performance, used the half solvent method to prepare a series of propellant samples with different solvent ratios, and used the close bomb experiment and scanning electron microscope (SEM) and other experiments to study the microstructure, shrinkage rate and combustion performance. Results show that with the same formula but different solvent ratios, the shrinkage rate and the internal structure of the triple-base propellant were quite different, the solvent ratio 0.34~0.35 propellant's combustion performance is quite good and its formula was the best recipe.

Copyright

© 2016, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Ming-Lei Chen
AU  - Xiao Ma
AU  - Kai-Lun Xiang
AU  - Ruo-Ting Xing
AU  - Wen-Bin Liu
AU  - Bo Zhang
AU  - Na Wang
AU  - Dan-Dan Ji
PY  - 2016/04
DA  - 2016/04
TI  - Experimental Study on a Triple-base Propellant Formulation
BT  - Proceedings of the 2016 3rd International Conference on Mechatronics and Information Technology
PB  - Atlantis Press
SP  - 775
EP  - 780
SN  - 2352-538X
UR  - https://doi.org/10.2991/icmit-16.2016.140
DO  - 10.2991/icmit-16.2016.140
ID  - Chen2016/04
ER  -