Investigations into the copper chromite particle size effect on the combustion characteristics of poly(vinyl-chloride) plastisol propellants

Author:

Benmahammed Mohamed Amine,Mouloud Abdelrazak

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials

Reference37 articles.

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2. M. T. Vernacchia, Development, modeling and testing of a slow–burning solid rocket propulsion system, Master of Science in Aeronautics and Astronautics, Massachusetts institute of technology “MIT”, Cambridge, USA (2017).

3. M. Rodriguez–Pesina, J. Garcia–Dominguez, F. Garcia–Hernandez, L. M. Flores–Vélez and O. Dominguez, The thermal decomposition of ammonium perchlorate–aluminum propellants in presence of metallic zinc particles, Materials Sciences and Applications, 8 (2017) 436–447.

4. A. Dey, A. K. Sikder, M. B. Talawar and S. Chottopadhyay, Towards new directions in oxidizers/energetic fillers for composite propellants: an overview, Cent. Eur. J. Energ. Mater., 12 (2) (2015) 377–399.

5. M. A. Benmahammed and A. Mouloud, Effects of some physical parameters on burning rate of PVC–plasticized propellants, Proc. 28th Int. Annual Conference ICT on Combustion and Detonation, Karlsruhe, Germany (1997).

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