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International Journal of Energetic Materials and Chemical Propulsion最新文献

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nanocomposite; nanothermite; polymeric binder; relative explosive force 纳米复合材料;nanothermite;聚合物粘结剂;相对爆发力
IF 0.7 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.1615/intjenergeticmaterialschemprop.2022046800
Vitaliy Popov, S. Sysolyatin, V. Malykhin, V. Komov
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引用次数: 0
Ignition and Combustion of TNT-Dispersed Aluminum Powder tnt分散铝粉的点火与燃烧
IF 0.7 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.1615/intjenergeticmaterialschemprop.2022038884
R. Houim, Jacob W. Posey, Swagnik Guhathakurta
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引用次数: 0
Nanoaluminum for Solid Rocket Propulsion: Illusions and Reality 用于固体火箭推进的纳米铝:幻想与现实
IF 0.7 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.1615/intjenergeticmaterialschemprop.2022039752
L. DeLuca
In a lecture at the California Institute of Technology, on 29 December 1959, Richard P. Feynman drew the attention to the “bottom scale”. That year, studies of nanosized metal (nMe) particles had started for the initiation of nuclear reactions in USA and for material science in the then-USSR. Nanosized energetic ingredients were first prepared at the Semenov Institute of Chemical Physics, Moscow, when Gen et al. produced nMe particles by vaporization and consequent condensation of metal vapors in argon. In rocket propulsion, because of its high combustion enthalpy and easy availability, Al is widely used to improve performance mainly of composite AP/HTPB formulations, the workhorse of space launcher solid motors.
1959年12月29日,理查德·费曼(Richard P. Feynman)在加州理工学院的一次演讲中提请人们注意“底标度”。那一年,纳米金属(nMe)粒子的研究已经开始,用于美国核反应的启动和当时苏联的材料科学。纳米级高能成分是在莫斯科谢苗诺夫化学物理研究所首次制备的,当时Gen等人通过在氩气中蒸发和随后的金属蒸气冷凝来生产nMe颗粒。在火箭推进中,由于其高燃烧焓和易于获得,铝被广泛用于提高性能,主要是复合AP/HTPB配方,这是航天发射固体发动机的主力。
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引用次数: 1
Thermal decomposition behaviors of 30% hydrogen peroxide over free noble metal-synthesized solid catalysts 30%过氧化氢在游离贵金属合成固体催化剂上的热分解行为
IF 0.7 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.1615/intjenergeticmaterialschemprop.2022043338
I. Remissa, Adil Souagh, Y. Hairch, A. Sahib-eddine, M. Atamanov, R. Amrousse
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引用次数: 0
Effect of Particle Loading on the Burning Characteristics of Boron Laden Gel Fuel Droplet 颗粒载荷对含硼凝胶燃料液滴燃烧特性的影响
IF 0.7 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.1615/intjenergeticmaterialschemprop.2022045054
M. R., Shaibya Kumari, S. Karmakar, P. K. Ojha
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引用次数: 2
RoseMortar-Equation – a universal equation to predict the strength of an explosive in a ballistic mortar test 罗斯莫塔尔方程-在弹道迫击炮试验中预测炸药强度的通用方程
IF 0.7 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.1615/intjenergeticmaterialschemprop.2022045724
T. Klapotke
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引用次数: 0
Determination of Steady State Mean Burning Rate of Composite Solid Propellant under Open loop and Closed loop with Servo-Mechanism by Laser Doppler Velocimetry 用激光多普勒测速法测定开环和闭环伺服机构下复合固体推进剂的稳态平均燃烧速率
IF 0.7 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.1615/intjenergeticmaterialschemprop.2022045053
Rajendra Rajak, S. Chakravarthy, B. S. Chandran
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引用次数: 0
HYDRIDE-DEHYDRIDE FINE ZIRCONIUM POWDERS FOR PYROTECHNICS 烟火用氢化-脱氢精细锆粉
IF 0.7 Q4 ENGINEERING, AEROSPACE Pub Date : 2021-01-01 DOI: 10.1615/intjenergeticmaterialschemprop.2020035408
I. Amelichkin, E. Knyazeva, R. Medvedev, A. V. Muslimova, R. Nefedov, V. Orlov, V. Sachkov, A. Sachkova, O. B. Stepanova, I. Zhukov
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引用次数: 0
THE EFFECT OF TEMPERATURE AND HUMIDITY ON THE THERMAL CHARACTERISTICS OF TETRAZOLE DERIVATIVES 温度和湿度对四氮唑衍生物热特性的影响
IF 0.7 Q4 ENGINEERING, AEROSPACE Pub Date : 2021-01-01 DOI: 10.1615/intjenergeticmaterialschemprop.2021035528
Satoru Yoshino, T. Komoriya, K. Sakamoto
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引用次数: 0
Catalytic potential of microsized additives in enhancing the linear burn rate of potassium nitrate-sucrose based composite solid propellant strands 微粒径添加剂对提高硝酸钾-蔗糖基复合固体推进剂线燃率的催化潜力
IF 0.7 Q4 ENGINEERING, AEROSPACE Pub Date : 2021-01-01 DOI: 10.1615/intjenergeticmaterialschemprop.2021038209
Manisha Bharti, Lakshay Bansal, Sonia Chalia
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引用次数: 2
期刊
International Journal of Energetic Materials and Chemical Propulsion
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