Experimental Study on a Triple-base Propellant Formulation
Ming-Lei Chen, Xiao Ma, Kai-Lun Xiang, Ruo-Ting Xing, Wen-Bin Liu, Bo Zhang, Na Wang, Dan-Dan Ji
Available Online April 2016.
- https://doi.org/10.2991/icmit-16.2016.140How to use a DOI?
- triple-base propellant, solvent ratio, formula, shrinking percentage
- 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.
- Open Access
- This is an open access article distributed under the CC BY-NC license.
Cite this article
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 - 2016 3rd International Conference on Mechatronics and Information Technology PB - Atlantis Press SN - 2352-538X UR - https://doi.org/10.2991/icmit-16.2016.140 DO - https://doi.org/10.2991/icmit-16.2016.140 ID - Chen2016/04 ER -