Full Papers
doi.org/10.1002/ejic.202001068
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Preparation of g-C N Nanosheets/CuO with Enhanced
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Catalytic Activity on the Thermal Decomposition of
[a]
[a]
[a]
[a]
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The thermal oxidation etching assisted g-C N nanosheets/CuO
metric analysis (TGA). As a result, in the case of 5 wt% TCN/CuO,
the high decomposition temperature of AP decreased by
120.6°C, which is much lower than that of UCN, TCN, CuO and
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was prepared through a facile co-precipitation strategy. In this
work, the structure, morphology, and composition of g-C N
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(
UCN, prepared by urea), g-C N nanosheets (TCN, prepared by
UCN/CuO. In addition, the exothermic heat released from the
decomposition of AP increased from 430.64 Jg
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À 1
thermal oxidation etching of UCN), g-C N /CuO (UCN/CuO), g-
to
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À 1
C N nanosheets/CuO (TCN/CuO) were characterized via X-ray
2856.08 Jg . This evident catalytic activity may be related to
the synergistic effect of CuO and TCN. This work provides a
novel strategy for the construction of composite catalyst for the
thermal decomposition of AP, which is supposed to possess
significant potential in the solid propellant field.
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diffraction (XRD), Fourier transform infrared spectroscopy (FT-
IR), X-ray photoelectron spectroscopy (XPS) and transmission
electron microscopy (TEM). Furthermore, the catalytic effect of
the obtained samples on the thermal decomposition of
ammonium perchlorate (AP) was examined by thermal gravi-
Introduction
exothermic heat, which is not beneficial to the operation of
[9]
propellant. Taking this into consideration, the introduction of
catalysts could decrease the high-temperature decomposition
temperature (HTD) of AP effectively. Furthermore, lower HTD
and more exothermic heat may result in a higher burning rate
to some extent.
Solid propellant is an important source of energy for the
propulsion systems of missiles and rockets, which is capable of
converting chemical energy into heat energy by combustion.
The combustion behavior, a main indicator to evaluate the
performance of propellants, determines the rate of energy
release, efficiency, and stability of propellants, which is closely
[
1–2]
To date, numerous catalysts have been developed and
employed in AP and AP-based propellants. Transition metal
[3–4]
[10–15]
[16–17]
related to the operational effectiveness of rocket weapons.
oxides (TMOs),
materials,
carbon materials (CNT and GO),
MOFs
[
18–19]
[20–21]
AP is the main constituent part of propellant formulation and
the most commonly used oxidant, and its thermal decomposi-
tion parameters, especially decomposition temperature and
exothermic heat, are directly connected with the combustion
characteristics of AP-based propellants.
The thermal decomposition mechanism of AP was put
ferrocene and its derivatives
are effective in
catalyzing AP. Based on numerous investigations, there is a
conclusion that various p-type metal oxides, including CuO,
Mn O , Fe O , Fe O , Ce O , MnO , etc, demonstrate consider-
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4
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[5–7]
able effect during decomposition of AP. CuO is one of the most
effective catalysts among multitudinous metal oxides, which
could reduce the HTD of AP magnificently. Nevertheless, pure
CuO particles, especially CuO nanoparticles, are extremely
inclined to agglomerate, which seems to have a negative effect
on the combustion of the propellant.
[8]
forward by Jacobs for the first time, AP is decomposed along
with proton transfer to form NH and HClO during the low
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temperature decomposition, and subsequently evaporated into
the gas phase. However, the reaction between the intermediate
NH and HClO is incomplete, and the residual NH may be
Among various two-dimensional materials, graphitic carbon
nitride (g-C N ) has aroused much concern on account of its
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adsorbed on the AP surface. The decomposition reaction of the
AP stops until the surface of the AP is entirely coated with NH3.
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[22–27]
high nitrogen content and peculiar structure,
whose
As the temperature continues to rise, the NH is adsorbed on
applications fields are mainly focused on photocatalytic, electro-
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[28–33]
the AP surface, reacts with HClO again and finally produces
catalytic and heterogeneous catalytic
fields. In addition, it
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volatile products such as N O, NO, H O, HCl, etc. However, pure
could be readily obtained from various nitrogen-rich precursors
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[
34–38]
AP usually has higher decomposition temperature and lower
including melamine, urea, thiourea, dicyanamide, etc.
Recently, apart from a promising metal-free catalyst, g-C N has
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also been considered as a carrier for loading nanoparticles that
tend to agglomerate.
For the first time, Peng and coworkers found that g-C N4
could be employed as a novel and effective catalyst for AP and
[
a] D. N. Ma, Prof. Dr. X. M. Li, Prof. Dr. X. Q. Wang, Prof. Dr. Y. J. Luo
School of materials science and engineering,
Beijing Institute of Technology,
Beijing 100081, China
E-mail: 13651278705@139.com
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a possible mechanism that g-C N is prone to meet the
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[
39]
requirement of thermal excitation was illustrated in detail. In
Eur. J. Inorg. Chem. 2021, 982–988
982
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