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Combustion of Boron in Airbreathing Rockets: Effects of the Secondary Combustion Chamber

机译：空气呼吸火箭中硼的燃烧：二次燃烧室的影响

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A performance comparison was calculated for a solid propellant containing 50% by weight of boron, and a powder injection where the propellant contained between 50% and 90% by weight of boron. The efficiency of combustion in the secondary chamber of an airbreathing rocket having powder injection was investigated using pressure changes from 2.5 to 11 bar, while keeping the boron percentage constant. A variation keeps the pressure constant and varies the boron percentage in the propellant between 50.5% and 87% by weight of boron.

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作者
Boussios, A.;
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年度 1979
页码 p.1-44
总页数 44
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Air breathing engines; Boron; Combustion chambers; Combustion efficiency; Metal powder; Oxidation; Solid propellant combustion; Solid propellant rocket engines; Tables (Data);

机译：空气呼吸发动机;硼;燃烧室;燃烧效率;金属粉末;氧化;固体推进剂燃烧;固体推进剂火箭发动机;表（数据）;

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1. Improved combustion model of boron particles for ducted rocket combustion chambers [J] . Kalpakli Bora, Acar Emir Bedig, Ulas Abdullah Combustion and Flame . 2017,第maya期

机译：管式火箭燃烧室硼粒子燃烧模型的改进
2. Characteristics of the combustion chamber of a boron-based solid propellant ducted rocket with a chin-type inlet [J] . Chen Binbin, Xia Zhixun, Huang Liya, Aerospace science and technology . 2018,第NOVa期

机译：带有下巴式进气口的硼基固体推进剂管道火箭的燃烧室特性
3. Effect of distributed injection of air into the afterburning chamber of a ram-rocket engine on the efficiency of combustion of boron particles [J] . Rashkovskii S. A., Milekhin Yu M., Fedorychev A. V. Combustion, Explosion, and Shock Waves . 2017,第6期

机译：分布式注入空气进入拉力火箭发动机燃烧型硼粒颗粒效率的效果
4. Combustion Study of the Boron Particles in the Secondary Chamber of Ducted Rocket [C] . Z. Xia, J. Hu, D. Fang, AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit . 2006

机译：管道火箭副室中硼粒子的燃烧研究
5. BIPROPELLANT COMBUSTION IN A LIQUID ROCKET COMBUSTION CHAMBER. [D] . JIANG, TSUNG LEO. 1987

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6. Transformation of Combustion Nanocatalysts inside Solid Rocket Motor under Various Pressures [O] . Jun-Qiang Li, Linlin Liu, Xiaolong Fu, 2019

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7. The Effect of Fuel Grain Size on the Combustion Characteristics in the Primary Combustion Chamber of Staged Combustion Hybrid Rocket [O] . Harunori NAGATA, Kenta HASHIBA, Hiroya SAKAI, 2010

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8. Analyses for the Description of Rocket and Airbreathing Propulsion System Combustion Chamber and Nozzle Flows Annual Report [R] . Edelman, R. B., Fortune, O. F., Weilerstein, G. 1970

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Combustion of Boron in Airbreathing Rockets: Effects of the Secondary Combustion Chamber

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