Author:
Liu Lin-lin,He Guo-qiang,Wang Ying-hong,Liu Pei-jin
Publisher
Springer Science and Business Media LLC
Reference16 articles.
1. Kuo KK, Summerfield M. Fundamentals of solid-propellant combustion. New York: American Institute of Aeronautics and Astronautics; 1984.
2. Menke K, Eisele S. Rocket propellants with reduced smoke and high burning rates. Propellant Explos Pyrotech. 1997;22(3):112–9. doi: 10.1002/prep.19970220304 .
3. Yang V, Brill TB, Ren WZ, Zarchan P. Solid propellant chemistry, combustion, and motor interior ballistics, vol. 185. New York: American Institute of Aeronautics and Astronautics; 2000.
4. Saravanakumar D, Sengottuvelan N, Narayanan V, Kandaswamy M, Varghese TL. Burning-rate enhancement of a high-energy rocket composite solid propellant based on ferrocene-grafted hydroxyl-terminated polybutadiene binder. J Appl Polym Sci. 2011;119(5):2517–24. doi: 10.1002/App.32859 .
5. Guo XD, Li FS, Song HC, Liu GP, Kong LR, Li MN, et al. Combustion characteristics of a novel grain-binding high burning rate propellant. Propellant Explos Pyrotech. 2008;33(4):255–60. doi: 10.1002/prep.200800223 .
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