Preparation and Combustion Performance of B/PVDF/Al Composite Microspheres

Author:

Cheng Long1,Huang Chuan2,Yang Yue1,Li Yifan1,Meng Yingyi1,Li Yanchun1,Chen Houhe1,Song Dongming13,Artiaga Ramón4

Affiliation:

1. School of Chemical EngineeringNanjing University of Science and Technology Nanjing 210094, Jiangsu China

2. Institute of Chemical MaterialsChina Academy of Engineering Physics Mianyang 621000, Sichuan China

3. Science and Technology on Applied Physics and Chemistry Laboratory Xian 710000, Shaanxi China

4. Department of Naval and Industrial Engineering, EsteiroUniversity of A Coruna (UDC) Ferrol 15471 Spain

Funder

Key Laboratory of National Defense Science and Technology

Publisher

Wiley

Subject

General Chemical Engineering,General Chemistry

Reference48 articles.

1. Application research of boron powder in propellants;Wang G.;J. Solid Rocket Technol.,1998

2. Thermal reaction characteristics of the boron used in the fuel-rich propellant

3. An investigation on boron used as a component of solid propellant;Zang L.;J. Propul. Technol.,1990

4. Thermoanalytical investigation on some boron–fuelled binary pyrotechnic systems

5. Electrophoretic assembly of B–Ti nanoenergetic coating for micro-ignitor application

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