Application and Properties of Nano‐sized RDX in CMDB Propellant with Low Solid Content

Author:

Liu Jie1,Ke Xiang1,Xiao Lei1,Hao Gazi1,Rong Yuanbo1,Jin Chengsu1,Jiang Wei1,Li Fengsheng1

Affiliation:

1. National Special Superfine Powder Engineering Research Center of China, School of Chemical EngineeringNanjing University of Science and Technology Nanjing 210094 P. R. China

Funder

National Natural Science Foundation of China

Publisher

Wiley

Subject

General Chemical Engineering,General Chemistry

Reference29 articles.

1. S. Chaturvedi P. N. Dave Solid Propellants: AP/HTPB Composite Propellants Arab. J. Chem.2015 DOI: https://doi.org./10.1016/j.arabjc.2014.12.033.

2. J. H. Yi F. Q. Zhao B. Z. Wang T. An Y. Wang H. X. Gao BTATz–HNIW–CMDB Propellants J. Therm. Anal. Calorim.2013 115 1227–1234.

3. J. Z. Li X. Z. Fan X. G. Liu Z. R. Liu Effects of Pranularity of Ammonium Perchlorate on Thermal Decomposition of AP-CMDB Propellant J. Propul. Tech.2009 30 380–384.

4. S. Elbasuney A. Fahd H. E. Mostafa Combustion Characteristics of Extruded Double Base Propellant Based on Ammonium Perchlorate/Aluminum Binary Mixture Fuel2017 208 296–304.

5. R. Damse H. Singh Nitramine-based high energy propellantcompositions for tank guns Def. Sci. J.2000 50 75–81.

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