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Aluminum hydride (AlH) is a promising fuel component of solid propellant, but its stabilization is still challenging. Herein, surface functionalization of hydrophobic perfluoropolyether (PFPE) followed by ammonium perchlorate (AP) coating has been implemented. In particular, AlH@PFPE@AP ( = 10, 30, 50, or 64.21%) composites (AHFPs) were prepared by a spray-drying technique. The PFPE-functionalized AlH with a hydrophobic surface shows an increased water contact angle (WCA) from 51.87° to 113.54°. Compared with pure AlH, the initial decomposition temperatures of AHFPs were increased by 17 °C, and the decomposition properties of AP in the AHFPs were also enhanced with significantly decreased peak temperature and fairly increased energy output. Moreover, the decomposition induction time of AHFPs-30% was improved by almost 1.82 times that of raw AlH, which indicates that the coatings of PFPE and AP could improve the stability of AlH. The maximum flame radiation intensity of AHFPs-30% was 21.6 × 10, which is almost 7.71 times that of pure AlH (2.8 × 10).
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http://dx.doi.org/10.1021/acs.langmuir.3c00711 | DOI Listing |
ACS Omega
August 2025
Institute of Chemistry and Materials, 17 Hoang Sam, Cau Giay, Hanoi 100000, Vietnam.
Graphene/FeO/CuO nanocomposites were successfully synthesized using an ultrasonic-assisted method, with FeO and CuO nanoparticles (10 to 20 nm in size) uniformly distributed on graphene sheets. The synthesis process was optimized through X-ray diffraction (XRD) analysis, and the nanocomposites were further characterized for morphology, elemental distribution, specific surface area, and bonding dynamics. Differential scanning calorimetry (DSC) revealed that adding 2 and 5 wt % of the composite reduced the thermal decomposition temperatures of ammonium perchlorate (AP) by 86.
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July 2025
School of Materials Science and Technology, Beijing Institute of Technology, Beijing 100081, China.
Al-based nanocomposite energetic materials have broad application prospects in explosives and propellants, owing to their excellent energy release efficiency. However, their insufficient reliability, poor stability, and difficulty of formation limit their practical application. This study employed self-assembly using a hydrophilic polymer polyvinylpyrrolidone (PVP) together with nano-aluminum powder (Al), copper oxide (CuO), and ammonium perchlorate (AP) to obtain high-strength and high-activity composite micrometer-sized microspheres.
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August 2025
College of Chemistry and Molecular Sciences, Wuhan University, Wuhan 430072, China.
Since ammonium perchlorate (AP) thermal decomposition catalysis is a typical heterogeneous catalytic process, developing catalysts with optimized interfacial properties has become an urgent priority. Catalysts featuring hierarchically porous structures demonstrate significant advantages in heterogeneous catalysis due to their abundant accessible active sites. In this study, a wrinkled hierarchically porous structure cerium-based metal-organic framework material (WHP-UiO-66-Ce) was synthesized by the soft template method, and its interaction with AP enabled efficient catalysis of AP decomposition.
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July 2025
Xi'an Modern Chemistry Research Institute, Xi an 710065, China.
The rheological properties of the propellant slurry and droplet dynamics during the casting process play a critical role in the manufacturing of propellants. This study systematically investigated the rheological characteristics of a hydroxyl-terminated polybutadiene (HTPB)-based composite solid propellant slurry and optimized the vacuum casting process through integrated experimental and numerical simulation approaches. Rheological tests revealed shear-thinning behavior, with the Herschel-Bulkley model parameters confirming non-Newtonian fluid characteristics.
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July 2025
Institute of Energetic Materials, Faculty of Chemical Technology, University of Pardubice, Pardubice CZ-532 10, Czech Republic.
The new combustion modifier cis-1,3,4,6-tetranitrooctahydroimidazo-[4,5-]-imidazole (BCHMX) was tested on an aluminum HMX/HTPB/AP propellant. Monitored were the changes in the propellant characteristics, when the 10, 20, and 30 wt % ammonium perchlorate (AP) were substituted by pure 1,3,5,7-tetranitro-1,3,5.7-tetrazocane (HMX), mechanical mixture HMX/BCHMX (PM), and coagglomerate of HMX/BCHMX (CACs), the latter two in a weight ratio of 8:1.
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