Effect of Nano‐Copper Chromite on the Thermal Decomposition and Combustion of AP‐Based Solid Propellants

Author:

Gou Bingwang1,Kou Yong2,Hu Yubing2,Zhang Guangpu2,Guo Hu2,Xiao Lei2ORCID,Zhao Fengqi1,Gao Hongxu1,Jiang Wei2ORCID,Hao Gazi2ORCID

Affiliation:

1. Xi'an Modern Chemistry Research Institute Xi'an 710065 China

2. National Special Superfine Powder Engineering Research Center of China School of Chemistry and Chemical Engineering Nanjing University of Science and Technology Nanjing 210094 China

Funder

National Natural Science Foundation of China

Publisher

Wiley

Subject

General Chemical Engineering,General Chemistry

Reference35 articles.

1. Estimation of ammonium perchlorate in HTPB based composite solid propellants using Kjeldahl method;Ajaz A. G.;J. Journal of Hazardous Materials,2010

2. Nano oxalates of Fe, Co, Ni: Burning rate modifiers for composite solid propellants

3. Effect of the dispersibility of nano-CuO catalyst on heat releasing of AP/HTPB propellant;Yang Y.;J. Journal of Nanomaterials,2011

4. Effect of Fe2O3 in Fe2O3/AP Composite Particles on Thermal Decomposition of AP and on Burning Rate of the Composite Propellant

5. A review on the preparation and application of nano-energetic materials;Wang S. W.;J. Chinese Journal of Explosives & Propellants,2021

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