Central European Journal of Energetic Materials

Papers
(The TQCC of Central European Journal of Energetic Materials is 1. The table below lists those papers that are above that threshold based on CrossRef citation counts [max. 250 papers]. The publications cover those that have been published in the past four years, i.e., from 2021-05-01 to 2025-05-01.)
ArticleCitations
A Comparative Numerical and Experimental Study of Light Weight Materials for Neutralizing Explosive Reactive Armour6
A Pressure-Dependent Plasticity Model for Polymer Bonded Explosives under Confined Conditions6
Prediction of Ignition Delay Times for Amine-based Liquid Propellants through a QSPR Approach6
Comparison of the Implemented Detonation Velocity Predictions in the Research Output Software for Energetic Materials Based on Observational Modelling (RoseBoom©) with 31 Experimental Values4
Experimental Insight into the Catalytic Mechanism of MFe2O4 (M = Ni, Zn and Co) on the Thermal Decomposition of TKX-504
Experimental Study and Numerical Simulation of Explosive Welding of Nickel Foil with Q235 Steel4
Study of the Progress of Reaction in the Preparation of tetra-Functional GAP using FTIR Spectroscopy3
Influence of Temperature on the Thermal Expansion and Other Physical Properties of Pressed RDX–Wax Explosive Pellets3
Catalytic Debenzylation of 2,4,6,8,10,12-Hexabenzyl-2,4,6,8,10,12-hexaazatetracyclo [5.5.0.0.3,1105,9] Dodecane with Pd(OH)2/Al2O3 in a Batch Suspension Reactor and Optimization of the Reaction Parame3
Modern Highly Energetic Materials for the Production of Gun Powders and Rocket Propellants in Poland3
Efficiency of Using Explosive Foam Compositions for Compacting Structurally Unstable Soil2
Green Fabrication of Nanoscale Energetic Molecular Perovskite (H<sub>2</sub>dabco)[Na(ClO<sub>4</sub>)<sub>3</sub>] with Reduced Mechanical Sensitivity2
Studies on Curing of an Aluminized Ammonium Perchlorate Composite Propellant Based on Nitrile Butadiene Rubber Using a Quinol Ether of 1,4-Benzoquinone Dioxime2
Explosively Formed Penetrators Inflight Heating Compared to Hemispherical Copper Shaped Charge Jet2
Preparation and Characterization of a Novel Energetic Cocrystal RDX:TNT (1:2)2
Integrating Moisture Isotherms, Compatibility Assessment, and Model Propellant with ADN as an Eco-Friendly Oxidizer2
Study of the Influence of Sensitizer Content on the Density of a Bulk Emulsion Explosive Used in Underground Operations2
Finite Volume Method for the Combustion Reaction of Energetic Materials2
Synthesis of a New Random Copolymer Based on Glycidyl Nitrate and Tetrahydrofuran: A Thermal, Kinetic, and Theoretical Study2
Study of Molecular Perovskite (H2dabco)[NH4(ClO4)3]/Carbon Nanotubes Energetic Composite2
Preparation and Characterization of a Novel Coordination Compound [K(18-crown-6)][N(NO2)2]2
Experimental Study of the Effectiveness of a Model Reactive Armour without Metal Plates1
Effect of Natural Ageing on the Safety Parameters and Performance of TNT-based Melt Cast RDX/TNT Compositions1
A Literature Review of the Influence of Water on the Properties of Mining Explosives1
Theoretical Analysis and Numerical Study for Spin Jet Formation Performance1
Photo-thermal Decomposition of HNS Surface by 532nm Laser Irradiation: Spectral and Quantitative Analysis using In-Situ XPS- Quadrupole MS Technique1
Experimental Study on the Diverse Output Performance of a Firearm Firing-Ignition System1
Studies on the High Performance Characteristics of an Aluminized Ammonium Perchlorate Composite Solid Propellant Based on Nitrile Butadiene Rubber1
Computational Determination of the Specific Impulse of Solid Rocket Propellant Compositions of closo-Dodecaborate ([B12H12]2‒) Salts with HTPB Binder and Ammonium Perchlorate as an Oxidizer1
Effects of Metal Oxides on the Thermal Decomposition Kinetics and Mechanisms of HAN/PVA Based Propellants1
Comparative Study of the Penetration Characteristics of Ni-Al and Pure Cu Shaped Charge Liners1
Statistical Approach in Determining Energy Ballistic Parameters of Gunpowder Contained in the 7.62×39 mm Ammunition Based on Measuring the Development of Pressure in a Manometric Bomb1
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