The Study on a Triple-Base Propellant Preparation and Combustion Performance

Ming Lei Chen; Dan Dan Ji; Xin Liao

doi:10.4028/www.scientific.net/AMR.781-784.2452

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 781-784The Study on a Triple-Base Propellant Preparation...

The Study on a Triple-Base Propellant Preparation and Combustion Performance

Abstract:

In order to improve the combustion performance of the nitroguanidine triple-base propellant and optimize its preparation technology, 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 combustion performance and shrinkage rate. Results show that with the same formula but different solvent ratios, the internal structure and the shrinkage rate of the triple-base propellant were quite different, the solvent ratio 0.34 propellant’s combustion performance is quite good, and its formula was the best recipe.

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Periodical:

Advanced Materials Research (Volumes 781-784)

Pages:

2452-2457

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.781-784.2452

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Online since:

September 2013

Authors:

Ming Lei Chen*, Dan Dan Ji, Xin Liao

Keywords:

Formula, Shrinking Percentage, Solvent Ratio, Triple-Base Propellant

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* - Corresponding Author

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