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A liquid stratification model to predict failure in thermally damaged EBW detonators Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-08-08 Michael Hobbs, Stephanie Coronel
In previous work, commercially available downward facing exploding bridgewire detonators (EBWs) were exposed to elevated temperatures. These detonators were then initiated using a firing set which discharged a high amplitude short duration electrical pulse into a thin gold bridgewire. Responses of the detonators were measured using photonic doppler velocimetry (PDV) and high-speed photography. A time
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Propiolate-Terminated Polybutadiene-Based Network Binders for Solid Propellants via Catalyst-Free Azide-Alkyne Cycloaddition Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-08-05 ByoungSun Min, Jinhyuk Lee, Sung June Kim, Hong-Min Shim
We developed the new preparation method of polubutadiene-based binders, which has been widely used in solid composite propellants, under the triazole curing system formed by the Huisgen azide-alkyne cycloaddition(AAC) without any promotors. Firstly, polybutadiene terminated propiolate, alkyne adjecent to electron-withdrawing group -C(=O)O-, PKPB(propiolate-terminated polybutadiene), was prepared followed
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Amorphization and Crystallization of Hexanitroazobenzene (HNAB) Using Conventional DSC and Flash DSC Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-08-03 Yung P. Koh, Zachary T. Fondren, Aric A. Denton, Sindee L. Simon, Gregory B. McKenna
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Phase Contrast X-Ray Imaging of the Collapse of an Engineered Void in Single-Crystal HMX Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-08-02 Christian J. Blum-Sorensen, Camilo A. Duarte, Jonathan D. Drake, Nicholas E. Kerschen, Kamel Fezzaa, Marisol Koslowski, Weinong W. Chen, Steven F. Son
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Experimental investigation of Zr-based amorphous alloy as a shaped charge liner Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-29 Jin Shi, Zheng-xiang Huang, Xu-dong Zu, Q. Q. Xiao
This study aimed to investigate the mechanical properties of Zr-based amorphous alloy at high strain rates and its use as a shaped charge liner. A split Hopkinson pressure bar (SHPB) was used to carry out dynamic mechanical performance tests, and a scanning electron microscope (SEM) was used to observe the fracture morphology of the test piece. The X-ray test of the jet formation and the static penetration
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Novel Segregated Solid Propulsion System with Separately Stored Fuel and Oxidizer Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-29 Joseph Lichthardt, Bryce C Tappan, Narendra De, Alan Novak, Eva Baca, David Oschwald, Grant Risha
The development and experimentation of a solid propulsion concept consisting of separate hydrogen-rich solid propellant and solid oxidizer grains is presented. This system consists of an extremely fuel-rich solid propellant, which, once ignited, undergoes a self-sustaining decomposition to release fuel-rich product gases, which are particularly rich in hydrogen gas. These relatively high-temperature
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Characterization and Testing of Unstable Oxidizers: Ammonium Chlorate and Nitrite Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-27 Athina Kominia, Justin Hunter, James Smith, Jimmie Oxley
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Effect of Nano-Copper Chromite on the Thermal Decomposition and Combustion of AP-Based Solid Propellants Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-21 Bingwang Gou, Yong Kou, Yubing Hu, Guangpu Zhang, Hu Guo, Lei Xiao, Fengqi Zhao, Hongxu Gao, Wei Jiang, Gazi Hao
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Identification of 2,2-dinitropropanol, a hydrolyzed product of aged eutectic Bis(2,2-dinitropropyl) acetal - Bis(2,2-dinitropropyl) formal mixture Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-19 Alexander Edgar, Camille Wong, Kitmin Chen, David Langlois, Dali Yang
Eutectic bis(2,2-dinitropropyl) acetal - bis(2,2-dinitropropyl) formal mixture, nitroplasticizer (herein called NP) has historically been produced by either the ter Meer or oxidative nitration synthesis process, wherein 2,2-dinitropropanol (DNPOH) is produced as an intermediate step in the both processes. Therefore that DNPOH, could be present in NP either as a production or hydrolysis degradation
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Detonation Characteristics of an Aluminized DNAN-based Melt-cast Explosive Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-18 Yang Yang, Zhuoping Duan, Shurui Li, Yong Han, Hui Huang, Liansheng Zhang, Fenglei Huang
Investigations of the detonation characteristics of a new aluminized DNAN-based melt-cast explosive RMA-2X (containing 30 wt.% DNAN (2,4-dinitroanisole), 30 wt.% NTO (3-nitro-1,2,4-triazol-5-one), 10 wt.% HMX (1,3,5,7-tetranitro-1,3,5,7-tetraazacyclooctane) and 30 wt.% aluminum) were undertaken, as well as a lithium fluoride (LiF) substituted explosive RMF-2X (containing 30 wt.% DNAN, 30 wt.% NTO,
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The Influence of AP Addition on the Combustion Characteristics of TKX-50 with Concentrated Ignition Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-15 Zhiyu Yan, Xun Cao, Jun Tao, kun zhang, Qianqian Li, Jinhua Wang, Zuohua Huang
In order to study the influence of ammonium perchlorate (AP) addition on the combustion reaction process of dihydroxylammonium 5,5´-bistetrazole-1,1´- diolate (TKX-50), a concentrated ignition system was used to evaluate the ignition and combustion characteristics of the samples. The self-luminescence characteristics and the OH concentration distribution in the flame of TKX-50 and TKX-50/AP composites
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In Memoriam: Professor h.c. Dr. Hiltmar Schubert Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-13
Professor h.c. Dr. Hiltmar Schubert, founder of Propellants, Explosives, Pyrotechnics and longtime director of Fraunhofer ICT passed away on December 27th, 2020. With this special issue on the occasion of Professor Schubert's 95th anniversary this year, Fraunhofer ICT, the PEP board and the international Energetic Material community want to take the opportunity to remember him as an outstanding personality
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Micromechanical Behavior of HTPB Propellant Bonding Interface under Uniaxial Tensile Loading Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-18 Shu-di Pei, Hong-fu Qiang, Xue-ren Wang, Jia-xiang Wang, Shi-qi Li
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Are All Solid Propellant Burning Rate Modifiers Catalysts? Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-18 Joseph Kalman
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Molding Fabrication of High-Energy Nanoparticles of Lead Azide Encapsulated by Graphene-Doped Porous Carbon Matrix with Excellent Ignition Ability Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-13 Zhenzhan Yan, Shuang Wang, Li Yang, Jimin Han, Wenchao Tong
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Preparation and Characterization of PANI Surface Modified HMX/F2602 Microcapsule Composites Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-12 Yuexin Li, Wenzheng Xu, Fengwei Guo, Tianlun Yan, Xin Zheng, Yamei Wei, Xianpeng Tan, Jingyu Wang
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Agglomeration in Composite Propellants Containing Different Nano-Aluminum Powders Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-12 Ortal Cohen, Dan Michaels, Yinon Yavor
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Shock Initiation and Detonation Parameters of Hexanitrohexaazaisowurtzitane (CL-20) Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-12 Alexander Utkin, Valentina Mochalova, Alla Zubareva, Viktoriya Rykova, Vasilii Sosikov, Vladislav Yakushev
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Synthesis of a new 1,2,4-triazine derived Azidoxime Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-10 Alexander Cleveland, Christopher Snyder, Gregory Imler, David Chavez, Damon Parrish
A 1,2,4-triazine based azidoxime was formed via the substitution of a chloroxime (3) with sodium azide in ethanol. This compound was characterized via single-crystal X-ray diffraction. This material has a calculated density of 1.746 g•cm–1 and is less sensitive to impact, spark, and friction, as compared to PETN and RDX. The dehydrated material has a calculated density of 1.823 g•cm–1 and the detonation
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Study on Tensile Mechanical Properties of GAP/CL-20/HMX Propellant Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-11 Guanglong Zhang, Xiangyang Liu, Jinshang Zhang, Muchen Li, Xu Zhang, Ningfei Wang, Xiao Hou
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Modelling of Ratchet Growth in TATB-Based Charge under Thermal Cycling Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-10 Shuo Wang, Xilin Yan, Fangyun Lu, Siyang Lei, Rong Chen
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Strain Rate and Temperature Effects of the JOXL-1 Explosive Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-08 Xintao Zhu, Xiaojing Zhang, Wenbin Li, Wenjin Yao
To determine the influence of temperature and strain rate on the mechanical behavior of JOXL-1 explosive, the stress-strain curves of JOXL-1 explosive at different temperatures (233 K-473 K) and different strain rates (110 s−1-400 s−1) were measured using a split Hopkinson pressure bar (SHPB) experimental system with a temperature control device. The results show that the dynamic mechanical properties
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Effects of Glycerol Tribenzoate on the Mechanical Properties and Reaction Characteristics of Al/THV Reactive Materials Prepared by Extrusion-Injection Molding Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-05 Shupeng Xu, Yinjie Wang, Xiuchen Zhao, Zenglin Yang, Xianjin Ning, Chengwen Tan
The metal/fluoropolymer reactive material, Al/THV composites, can be prepared effectively into different shapes by extrusion injection molding. In this study, glycerol tribenzoate (GTB) plasticizer was introduced into Al/THV (35/65 wt%) prepared by extrusion and injection molding. The addition of GTB significantly affected certain properties of the matrix (THV), which consequently affected the mechanical
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Theoretical Study on the Gas-Phase Oxidation Mechanism of Ethylene by Nitrous Oxide Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-01 Yuyan Li, Rongpei Jiang, Sen Xu, Xuedong Gong
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Self-Healing of HTPB Based Polyurethane Binder via Ring Opening Metathesis Polymerization Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-06 Akash M Dhas, Kavita Ghosh, Shaibal Banerjee
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Effect of Ingredients Ratio on the Friction Sensitivity and Burning Performances of Mg/Ba(NO3)2/Novolac Resin Pyrotechnic Compositions Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-06 Akbar Zare, Mohammad Zhiani
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Experimental and Numerical Analysis of Single Screw Extrusion Process for Thermoplastic PBX Based on PVT Properties Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-05 Yufan Bu, Chunyan Chen, Fan Jiang, Xiaofeng Wang, Defu Che, Hai Nan
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A Nonlinear Ultrasonic Method for Detection and Characterization of Dewetting Damage in Solid Propellant Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-04 Yu Pan, Wen-Zhong Qu, Shou-Cheng Zhang, Li Xiao, Xi-Hua Chu
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Towards a deep insight into thermal and moisture aging of silicon-based pyrotechnic delay composition through a combination of spectroscopy– Principal component analysis approaches Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-01 Amir Abdelaziz, Slimane Bekhouche, Ahmed Fouzi Tarchoun, Abderahmane Mezroua, Djalal Trache
The aging of pyrotechnics is heavily influenced by temperature and humidity during their long-term storage. The investigation of the aging mechanisms of such composites is of great interest for their safe storage and use in weapon systems, hence avoiding any unexpected phenomenon or decrease in performance. This study is aimed at understanding the aging effects related to temperature and moisture on
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Prevention of Self Decomposition in Pyrotechnic Wet Mixtures by Replacing Aluminium with Boron Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-01 Lakshmana Pandian Prakash, Arumugachamy Azhagurajan, Kadarkaraithangam Jeyasubramanian
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Detonation Performance Experiments, Modeling, and Scaling Analysis for Pentaerythritol Tetranitrate (PETN) High Explosive Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-01 Eric K. Anderson, Carlos Chiquete, Ritchie I. Chicas, Scott I. Jackson
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An analysis and calculation method for one-dimensional balanced Interior ballistics of a recoilless gun Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-06-30 zhonghui jiang, Gang Tao, Peng Wen, Zhiyu Li, Hongmin Yan
The balancing force of the interior ballistics is an important issue in the design of the recoilless gun. It has been found in practice that the balancing force design method for recoilless guns based on the traditional classical interior ballistic theory cannot guide the balance from the physical mechanism and process. In order to study the unbalanced force experienced by the recoilless gun during
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Monitoring of aging of solid-rocket-motor propellant grains using an electromechanical impedance method Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-06-30 Duan Lei-Guang, Xueren Wang, Hongfu Qiang, Zhejun Wang
It is of great significance to monitor the aging state and evaluate the useful life of stored solid-rocket-motor ( SRM ) propellant grains. In this work, the aging state of hydroxyl terminated polybutadiene(HTPB) propellant grains was studied based on the electromechanical impedance (EMI) method. The relationship between the complex modulus and the mechanical impedance of viscoelastic material was
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Preparation of LLM-105-Based Explosive Ink and Its Detonating Transfer Performance in Explosive Network Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-06-30 Jialin Cai, Guan Luo, Hui Huang, Yousong Liu, Xin Di, Han Gao
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Detonation Reaction Zone and Acceleration Ability of a TKX-50 Based Polymer Bonded Explosive Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-01 Kaiyuan Tan, Yong Han, Jiahui Liu, Xiaojun Lu, Guijuan Fan, Zhijian Yang, Fenglei Huang
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Using Wavy Fuel Surface to Improve the Performance of the Solid Fuel Ramjets Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-01 Alireza Reyhani, Amir Mahdi Tahsini
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Extended JCZ3 Equation of State and JAGUAR Implementation for High Explosives Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-01 Leonard Stiel, Ernest Baker, Philip Samuels, Rodger Cornell, David Rydzewski
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Impact and Friction Sensitivities of PETN: I. Sensitivities of the Pure and Wetted Material Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-07-01 Thomas M. Klapötke, Guillaume Lemarchand, Tobias Lenz, Moritz Mühlemann, Jörg Stierstorfer, Ralf Weber
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Preparation and Performance of ANPyO/Emulsion Explosive Composite Energetic System Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-06-30 Zhiwei He, Yuanyuan Li, Yikang Yu, Chuanhao Xu, Wenyu Zhu, Yuqiang Ge, Wei Cheng
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A New High Order Virial Equation of State and Its Application in the Chapman-Jouguet Parameters Calculation of Explosives Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-06-30 Yue Peng, Xinping Long, Xiaohua Jiang, Zhiming Zhang
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Initial Temperature Effects on the Combustion Characteristics of Al Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-06-29 Hui Liu, Jianzhong Liu, Jifei Yuan, Xiaolin Chen, Yu Zhao, Wuxi Xie
The combustion of aluminium in propellants plays an important role in the energy release of propellants, and investigations of the combustion mechanism of aluminium can help to further improve the energy release characteristics of propellants. The changes in reaction temperature and product content over time during the reaction of Al(l)/O2 and Al(l)/AP systems at different initial temperatures were
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DRAGON – The German Thermo-Chemical Code Based on the Becker-Kistiakowsky-Wilson Equation of State Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-06-23 Werner Arnold, Ernst Rottenkolber, Thomas Hartmann
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Electronegativity at the Shock Front Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-06-23 Martin Rahm
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Developing Reaction Chemistry Models from Reactive Molecular Dynamics: TATB Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-06-15 Edward M. Kober
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Integration of Complex Geometry Gun Propellant Form Function Calculation and Geometry Optimization Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-06-15 Moru Wang, Guorui Jin, Yongrong Zhou, Fengqiang Nan, Xiangyang Lin, Weidong He
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Elastic Anisotropy of 1,3,5-Triamino-2,4,6-Trinitrobenzene as a Function of Temperature and Pressure: A Molecular Dynamics Study Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-06-15 Paul Lafourcade, Jean-Bernard Maillet, Nicolas Bruzy, Christophe Denoual
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ADN Solid Propellants with High Burning Rates as Booster Material for Hypersonic Applications Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-06-15 Stefan Sims, Sebastian Fischer, Claudio Tagliabue
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Copper Oxide Nano-Catalyst Incorporated TEGDN/NC/DAG Propellants: Thermal Behaviors and Kinetics Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-06-13 Vahid Mirzajani, Hamed Nazarpour-Fard, Khalil Farhadi, Ali Ghobadian
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Long-Term and Short-Term Creep Characteristic Analysis for HTPB Propellant Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-06-13 Kuangwei Deng, Haiyang Li, Jie Xu, Huiru Cui, Zhibin Shen
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Critical Evaluation of Reactive Force Fields for Vibrational Spectra: Case Study of Crystalline Cellulose Iβ Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-06-08 Zhiyu Liu, Peter W. Chung
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Systematic Builder for All-Atom Simulations of Plastically Bonded Explosives Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-06-08 Chunyu Li, Brenden W Hamilton, Tongtong Shen, Lorena Alzate, Alejandro Strachan
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Interaction-Enhanced Coating of Energetic Material: A Generally Applicable Method for the Desensitization Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-06-03 Yulan Song, Qi Huang, Jinhao Zhang, Yujia Zhang, Bo Jin, Rufang Peng
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Laser Ignition Process of Energetic Particles Under Consideration of Non-Fourier Effect Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-06-01 Tianyi Li, Xiaobing Zhang
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The Crystal Transformation of α-HNIW Coated with Different Coatings Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-05-31 Shengwei Li, Xueyong Guo, Qi Pan, Chengcheng Wu, Honglei Zhang
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Trace Analysis Model of Muzzle Smoke Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-05-31 Chen-guang Yan, Ming-xing Zhang, Yan Li, Chen-guang Zhu, Zi-hao Zhang
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Oxidizability Enhancement of Hydroxyl Terminated Polyether Polyurethane Elastomers via Fluoroalcohols Grafting Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-05-31 Chen Shen, Shi Yan, Xiaole Sun, Yanwei Tan, Yapeng Ou, Qingjie Jiao
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Simulation of the Loading Density for Gun Propellants with Arbitrary Shapes Using a Discrete Element Method Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-05-31 Sebastian Wurster, Martin Lietz, David Sprengel
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Experimental Investigation on Fracture Properties of HTPB Propellant with Circumferentially Notched Cylinder Sample Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-05-27 Zhejun Wang, Hongfu Qiang, Jiaxiang Wang, Leiguang Duan
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Theoretical Research on the Combustion Mechanism and Kinetics for Aluminum and Carbon Dioxide Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-05-26 Siyi Zhang, Yunlan Sun, Baozhong Zhu, Tao Sun
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Review of the Effects of Polymer Binder Properties on Microstructure and Irreversible Volume Growth of Plastic Bonded Explosives Formulations Propellants Explos. Pyrotech. (IF 2.134) Pub Date : 2022-05-26 Jeremy J. Pietron, Paul B. Mirkarimi