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Assessment of the Shelf Life of Composite Solid Propellants in Air and Nitrogen Atmospheres through Thermal Ageing 复合固体推进剂在空气和氮气环境中热老化的保质期评估
IF 0.8 4区 工程技术 Q4 CHEMISTRY, APPLIED Pub Date : 2021-03-30 DOI: 10.22211/CEJEM/134663
M. Keshavarz, Seyyed Mohammad Hossein Hosseini, M. Karimi
This work introduces dynamic mechanical thermal analysis (DMTA) as an efficient method for the assessment of the shelf life of solid composite solid propellants in air and nitrogen atmospheres. The samples were aged at three temperatures 323.15, 333.15, and 343.15 K for 60, 120, and 180 days. The two different methods of Arrhenius and Berthelot were used to compare the effects of air and nitrogen atmospheres on the ageing of composite solid propellants. Damping (Tan δ) of composite solid propellants was used to determine the shelf life of the samples based on the loss of half of the physical property Tan δ (50% drop in damping). For the air atmosphere, the calculated activation energy for the degradation reactions of the samples was 86.26 kJ·mol–1. Both models, Arrhenius and Berthelot, confirmed that the shelf lives of the samples under the nitrogen atmosphere are more than four times those in an air atmosphere.
本文介绍了动态机械热分析(DMTA)作为一种评估固体复合固体推进剂在空气和氮气环境中保质期的有效方法。样品在323.15、333.15和343.15 K三个温度下老化60、120和180天。采用Arrhenius和Bertherot两种不同的方法比较了空气和氮气环境对复合固体推进剂老化的影响。复合固体推进剂的阻尼(Tanδ)用于根据物理性能Tanδ的一半损失(阻尼下降50%)来确定样品的保质期。对于空气气氛,样品降解反应的计算活化能为86.26 kJ·mol–1。Arrhenius和Bertherot这两个模型都证实,样本在氮气环境下的保质期是空气环境下的四倍多。
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引用次数: 1
Novel Composite Solid Propellant with High Resistance to Thermo-oxidative Degradation Reactions, Extended Shelf Life, and Superior Combustion Characteristics 新型复合固体推进剂具有高抗热氧化降解反应,延长保质期和优越的燃烧特性
IF 0.8 4区 工程技术 Q4 CHEMISTRY, APPLIED Pub Date : 2021-03-30 DOI: 10.22211/CEJEM/135119
Sherif Elbasuney, Eslam Elsaka, A. Elbeih, H. Mostafa
Hydroxy-terminated polybutadiene (HTPB) pre-polymer is the main constituent that is responsible for conferring high mechanical properties on composite solid propellants. However, HTPB pre-polymer suffers from oxidative degradation reactions that diminish its mechanical properties and shelf life. Composite solid propellant formulations based on an advanced stabilizing agent (anti-oxidant), Flexzone 6-H, with different curing ratios, 0.7 and 1.1, were developed via mixing and casting under vacuum. The developed formulations were subjected to artificial ageing using Vant Hoff,s formula by isothermal heating at 80 °C for up to 35 days. The change in strain with ageing was evaluated using a uni-axial tensile test. The propellant formulation based on a curing ratio of 0.7 demonstrated a high ageing resistance coefficient and an extended service life of up to 15 years, compared with 5 years for higher curing ratio. A propellant grain is considered to be ‘aged out’ at 30% reduction in its maximum strain value. The propellant formulation based on the 0.7 curing ratio exhibited superior thermal stability as it offered a minimum decrease in heat released after ageing using DSC. Additionally, the 0.7 curing ratio formulations exhibited a minimum change in burning rate and pressure exponent with ageing time. It can be concluded that the propellant with 0.7 curing ratio can maintain its mechanical, thermal, and ballistic properties with ageing. Central European Journal of Energetic Materials ISSN 1733-7178; e-ISSN 2353-1843 Copyright © 2021 Łukasiewicz Research Network – Institute of Industrial Organic Chemistry, Poland 144 S. Elbasuney, E. Elsaka, A. Elbeih, H.E. Mostafa Copyright © 2021 Łukasiewicz Research Network – Institute of Industrial Organic Chemistry, Poland
端羟基聚丁二烯(HTPB)预聚物是赋予复合固体推进剂高机械性能的主要成分。然而,HTPB预聚物受到氧化降解反应的影响,降低了其机械性能和保质期。以先进的稳定剂(抗氧化剂)Flexzone 6-H为基础,通过混合和真空铸造,研制了固化比为0.7和1.1的复合固体推进剂配方。所开发的配方使用万特霍夫公式在80°C等温加热长达35天进行人工老化。应变随老化的变化是用单轴拉伸试验来评估的。基于固化比为0.7的推进剂配方显示出高的抗老化系数和延长的使用寿命长达15年,相比之下,更高的固化比为5年。推进剂颗粒在其最大应变值降低30%时被认为是“时效”的。基于0.7固化比的推进剂配方表现出优异的热稳定性,因为它在使用DSC老化后提供了最小的热释放减少。此外,0.7固化比配方的燃烧速率和压力指数随老化时间的变化最小。结果表明,0.7固化比的推进剂在老化后仍能保持其力学、热、弹道性能。中欧含能材料学报,ISSN 1733-7178;e-ISSN 2353-1843版权所有©2021 Łukasiewicz波兰工业有机化学研究所研究网络144 S. Elbasuney, E. Elsaka, A. Elbeih, H.E. Mostafa版权所有©2021 Łukasiewicz波兰工业有机化学研究所研究网络
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引用次数: 0
Theoretical Simulations on Physicochemical Performance of Novel High-energy BHDBT-based Propellants 新型高能BHDBT基推进剂物理化学性能的理论模拟
IF 0.8 4区 工程技术 Q4 CHEMISTRY, APPLIED Pub Date : 2021-03-30 DOI: 10.22211/CEJEM/134652
Ke Wang, Hai-tao Huang, Huixiang Xu, Huan Li, Jun-qiang Li, X. Fan, W. Pang
Based on Energy Calculation Star program and molecular dynamic method, three designed 2,3-bis(hydroxymethyl)-2,3-dinitro-1,4-butanediol tetranitrate-based (BHDBT) propellants are firstly reported and their physicochemical performance are investigated. Results suggest that compared with HMX-based and CL-20-based propellants, the specific impulses of all BHDBT-based propellants surpass or approximate 280 s, which indicates the latter have the potential to be high-energy propellants. The diffusion coefficient of plasticizers in BHDBT-based propellant decrease as the temperature reduces, and reduce in the order: Bu-NENA > TMETN > BTTN. The densities of all BHDBT-based propellants surpass or approximate 1.7 g/cm3. The comparison of elastic constants, Poisson’s ratios and K/G values indicates that the mechanical properties of three BHDBT-based propellants increase in the order (by plasticizer): Bu-NENA < TMETN < BTTN. The bond length analysis of C–NO2 and O–NO2 bond in BHDBT suggests that the former is the trigger bond in the BHDBT-based propellants, and the safety of BHDBT-based propellants and BHDBT crystal decreases in the order: GAP/BTTN/Al/BHDBT > GAP/Bu-NENA/Al/BHDBT ≈ GAP/TMETN/Al/BHDBT > BHDBT. In conclusion, GAP/BTTN/Al/BHDBT propellant has the potential to be a novel high-energy propellant.
基于能量计算星程序和分子动力学方法,首次报道了三种设计的2,3-双(羟甲基)-2,3-二硝基-1,4-丁二醇四硝酸酯基(BHDBT)推进剂,并对其物理化学性能进行了研究。结果表明,与HMX基和CL-20基推进剂相比,所有BHDBT基推进剂的比冲都超过或接近280s,这表明后者具有成为高能推进剂的潜力。增塑剂在BHDBT基推进剂中的扩散系数随着温度的降低而降低,其降低顺序为:Bu-NENA>TMETN>BTTN。所有BHDBT基推进剂的密度都超过或接近1.7 g/cm3。弹性常数、泊松比和K/G值的比较表明,三种BHDBT基推进剂的力学性能按增塑剂的顺序增加:Bu-NENAGAP/Bu-NENA/Al/BHDBT≈GAP/TMETN/Al/BHDBT>BHDBT。总之,GAP/BTTN/Al/BHDBT推进剂具有成为一种新型高能推进剂的潜力。
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引用次数: 0
Shear Flow of Guncotton Pulp 贡棉浆剪切流动
IF 0.8 4区 工程技术 Q4 CHEMISTRY, APPLIED Pub Date : 2021-03-30 DOI: 10.22211/CEJEM/134904
V. Banishevsky, R. Zakusylo, D. Zakusylo
This article considers aspects of the flow, rheology, and viscometry of guncotton pulp. It is substantiated that during production guncotton pulp is subjected to shear deformation, taking into account sliding over smooth surfaces, in the input zones of the dies, in the barrel, and on the crimped finned tube of the screw extruder. At the same time, the presence of shear stress in guncotton pulp has not been established. A rotational viscometer with a torque meter, which was developed during this research, enabled the presence of shear stress in guncotton pulp to be demonstrated. The values of the flow stress depend on the solvent content in the guncotton pulp; as this is decreased, the τ0 value increases. When the flow curve for the section from τ0 to τRmax was constructed, the flow curves of the guncotton pulp were described by the Herschel-Bulkley equation. The flow curves of guncotton pulp obtained on corrugated capillaries of different sizes are non-invariant and depend on the magnitude of the deformation of the guncotton pulp in the capillaries. Guncotton pulp flows in a narrow range of pressures and deformations.
本文从浆料的流动性、流变性和粘度等方面进行了研究。事实证明,在生产过程中,考虑到在光滑表面上、模具的输入区、筒体和螺杆挤出机的卷曲翅片管上的滑动,浆棉浆会发生剪切变形。同时,粘棉浆中剪切应力的存在尚未确定。在这项研究中开发了一种带扭矩计的旋转粘度计,使粘棉浆中剪切应力的存在得以证明。流动应力的值取决于浆粕中溶剂的含量;随着时间的减少,τ0值增加。当构造τ0至τRmax截面的流动曲线时,炮棉浆的流动曲线由Herschel-Bulkley方程描述。在不同尺寸的波纹毛细管上获得的粘棉浆的流动曲线是非不变的,并且取决于粘棉浆在毛细管中的变形幅度。贡棉浆在狭窄的压力和变形范围内流动。
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引用次数: 0
The Shooting Tests of Target Perforating Ability, Performed on Cast Concrete Cylinders 现浇混凝土筒靶射孔能力射击试验
IF 0.8 4区 工程技术 Q4 CHEMISTRY, APPLIED Pub Date : 2020-12-31 DOI: 10.22211/cejem/132066
Ł. Habera, Kamil Hebda, P. Koślik, T. Sałaciński
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引用次数: 1
Composite Propellant Formulation of Poly (16-, 32- and 64-) Azido Dendritic Esters as Energetic Plasticizer and Evaluation of Properties 聚(16-、32-和64-)叠氮树突状酯作为高能增塑剂的复合推进剂配方及性能评价
IF 0.8 4区 工程技术 Q4 CHEMISTRY, APPLIED Pub Date : 2020-12-28 DOI: 10.22211/cejem/131235
K. D. B. Yamajala, Hema Singh, Ramesh Kurva, M. Maurya, Shaibal Banerjee
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引用次数: 0
The Effect of Detonator Shell Materials on Detonation Calorimetry Results 雷管壳体材料对爆轰量热结果的影响
IF 0.8 4区 工程技术 Q4 CHEMISTRY, APPLIED Pub Date : 2020-12-28 DOI: 10.22211/cejem/131804
O. Němec, Tomáš Musil, M. Künzel
Detonation calorimetry is a method for the determination of the heat released by the detonation of an explosive charge. Compared to classical combustion calorimetry, detonation calorimetry requires an inert atmosphere, a large sample mass and a detonator for its initiation. This detonator releases some energy for which the results must be corrected. Four types of detonator have been tested in the calorimeter alone and also in combination with explosive charges of PETN. It was found that the aluminium shell of the detonator considerably increases the apparent heat of detonation of the PETN samples in a vacuum, while the presence of combustible (polymeric) components has the opposite effect. Pressurization of the calorimetric vessel with nitrogen gas only partially suppresses these effects. The preferred technique is to use copper or glass confinement in a high pressure inert atmosphere.
爆震量热法是一种测定炸药爆炸释放热量的方法。与经典的燃烧量热法相比,爆震量热法需要惰性气氛、大的样品质量和引爆剂。这种雷管释放出一些能量,必须对其结果进行校正。四种类型的雷管已经单独在量热计中进行了测试,也与PETN炸药组合进行了测试。研究发现,雷管的铝壳显著增加了PETN样品在真空中的表观爆热,而可燃(聚合物)组分的存在具有相反的效果。用氮气对量热容器加压只能部分抑制这些影响。优选的技术是在高压惰性气氛中使用铜或玻璃限制。
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引用次数: 1
Regularities of Spheroidization of HMX Extracted from Solid Propellant Disposal Products 固体推进剂处理产物中HMX的球化规律
IF 0.8 4区 工程技术 Q4 CHEMISTRY, APPLIED Pub Date : 2020-12-28 DOI: 10.22211/cejem/131782
Maksym Cheltonov, R. Zakusylo, I. Ustymenko
Nitramines of high quality for manufacturing high-energy composites, such as oсtogen (HMX) and hexogen, have received much attention by researchers worldwide. Mixed formulations containing fillers in the form of spheroidal dispersed particles of explosives are homogenized at lower energy consumption. They are characterized by stable rheological characteristics, which guarantee the quality of the products obtained on the basis thereof. Methods for obtaining spherical nitramine particles by means of ultrasonic and hydromechanical rounding using commercial HMX were evaluated. It was found that under similar conditions, rounding by the hydromechanical process in a vortex device is more efficient and less energy-consuming than that of the ultrasonic method. It was confirmed that spheroidization of commercial HMX in an aqueous dimethyl sulfoxide (DMSO) medium by hydromechanical rounding occurs due to erosion of crystals of large size (70 μm or more). Based on the experimental results with spheroidization of commercial nitramine, the mass fraction content below 50 μm versus time was plotted for hydromechanical rounding. The method of hydromechanical rounding in aqueous DMSO to obtain spheroidized HMX, extracted from solid propellant using DMSO, was found to be the most suitable. Spheroidized modified HMX with specific characteristics (density and crystals of near-spherical shape) was obtained, which could be used for the manufacture of high-energy composites.
用于制造高能复合材料的高质量硝胺,如邻苯二甲酸酯(HMX)和己烯,受到了世界各地研究人员的广泛关注。含有球形分散炸药颗粒形式填料的混合制剂以较低的能耗进行均质化。它们具有稳定的流变特性,保证了在此基础上获得的产品的质量。评价了使用商用HMX通过超声和流体力学成圆获得球形硝胺颗粒的方法。研究发现,在类似的条件下,涡流装置中的流体力学过程比超声波方法更有效,能耗更低。已经证实,商业HMX在二甲基亚砜(DMSO)水性介质中通过流体力学成圆发生的球化是由于大尺寸(70μm或更大)晶体的侵蚀。基于商业硝胺球化的实验结果,绘制了低于50μm的质量分数含量与时间的关系图,用于流体力学圆角。在二甲基亚砜水溶液中进行流体力学成圆以获得球化HMX的方法被认为是最合适的,该方法使用二甲基亚磺酸从固体推进剂中提取。获得了具有特定特性(密度和近球形晶体)的球化改性HMX,可用于制造高能复合材料。
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引用次数: 0
Study of the Synthesis of GAP-HTPB-GAP Liquid Copolymer GAP-HTPB-GAP液体共聚物的合成研究
IF 0.8 4区 工程技术 Q4 CHEMISTRY, APPLIED Pub Date : 2020-12-28 DOI: 10.22211/cejem/131803
M. Chmielarek, Paweł Maksimowski, Katarzyna Cieślak, T. Gołofit, Hanna Drozd
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引用次数: 2
Estimation of the Detonation Pressure of Co-crystal Explosives through a Novel, Simple and Reliable Model 用一种新的、简单可靠的模型估算共晶炸药的爆压
IF 0.8 4区 工程技术 Q4 CHEMISTRY, APPLIED Pub Date : 2020-12-28 DOI: 10.22211/cejem/131687
N. Zohari, M. Montazeri, S. G. Hosseini
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引用次数: 1
期刊
Central European Journal of Energetic Materials
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