4.7 Article

Graphene oxide-(ferrocenylmethyl) dimethylammonium 3-nitro-1,2,4-triazol-5-one composites as catalysts on the combustion of HTPB propellant

Journal

COMBUSTION AND FLAME
Volume 249, Issue -, Pages -

Publisher

ELSEVIER SCIENCE INC
DOI: 10.1016/j.combustflame.2023.112620

Keywords

Energetic compound; Graphene oxide; Functional material; Solid propellant; Combustion catalyst

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Graphene-based combustion catalysts have attracted much attention due to their excellent catalytic performance. In this study, graphene oxide-(ferrocenylmethyl) dimethylamine-3-nitro-1,2,4-triazol-5-one (GO@MAFcNTO) composites with different GO contents were prepared and systematically characterized. The catalytic effect of GO@MAFcNTO on AP and the combustion performance of HTPB propellant containing GO@MAFcNTO were investigated. The results demonstrated that GO@MAFcNTO effectively reduces the activation energy and decomposition temperature of AP and significantly improves the combustion performance of HTPB propellant.
Graphene-based combustion catalysts have attracted much attention from propellant chemists due to their excellent catalytic performance. To investigate the synergistic effect of graphene oxide and ferrocene derivatives, graphene oxide-(ferrocenylmethyl) dimethylamine-3-nitro-1,2,4-triazol-5-one (GO@MAFcNTO) composites with different GO contents were prepared by vacuum freeze-drying method. It was system-atically characterized by SEM, EDS, FT-IR, XRD, Raman, and XPS. The catalytic action of GO@MAFcNTO on AP was detected by DSC, and the corresponding kinetic parameters were calculated and analyzed by thermal decomposition kinetics. In addition, the strand burning rate, pressure index, flame structure, and condensed combustion products of HTPB propellants with or without GO@MAFcNTO were analyzed. The results show that the as-synthesized GO@MAFcNTO can effectively reduce the activation energy and decomposition temperature of AP. In addition, the combustion performance of HTPB propellant contain-ing GO@MAFcNTO has been greatly improved, and the combustion efficiency of aluminum powder has been improved. At 2.0 MPa, the burning rate of HTPB propellant containing GO@MAFcNTO increases from 2.19 mm center dot s -1 to 4.43 mm center dot s -1. The excellent catalytic performance of GO@MAFcNTO comes not only from the uniform dispersion of iron in the GO lamellar of ferrocene derivatives, but also from the excellent conductivity of GO and the synergistic effect of GO and MAFcNTO. Among them, GO can mainly reduce the activation energy in the reaction process, while ferrocene derivatives provide a large number of active sites in the reaction process, and the synergistic effect of the two promotes the complex to have a good catalytic activity.(c) 2023 The Combustion Institute. Published by Elsevier Inc. All rights reserved.

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