Numerical Study of Intrachamber Processes Dynamics at Nozzleless Solid Propellant Rocket Engine Actuation

M. Yu. Egorov; D. M. Egorov

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Numerical Study of Intrachamber Processes Dynamics at Nozzleless Solid Propellant Rocket Engine Actuation

机译：无喷嘴固体推进剂火箭发动机启动室内过程动力学的数值研究

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The results of the comprehensive numerical analysis for dynamics of intrachamber processes that appear at nozzleless solid propellant rocket engine (SPRE) actuation are presented. A complete cycle of rocket engine operation is analyzed. We solve a conjugate problem involving the igniter actuation; heating, ignition and following combustion of a solid propellant charge; a combustion product flow in the combustion chamber; depressurization of the combustion chamber, and the subsequent motion of the rocket engine blank; variation of the combustion surface geometry at the expense of the gradual and nonuniform burnout of solid propellant web.

机译：提出了对无喷嘴固体推进剂火箭发动机（SPRE）驱动时出现的腔内过程动力学进行综合数值分析的结果。分析了火箭发动机操作的完整循环。我们解决了涉及点火器驱动的共轭问题。固体推进剂装料的加热，点火和燃烧;燃烧产物在燃烧室内的流动;燃烧室降压，随后火箭发动机坯料运动;改变燃烧表面的几何形状，以牺牲固体推进剂纤维网的逐渐和不均匀的燃尽为代价。

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《Russian Aeronautics》 |2013年第1期|共5页
作者
M. Yu. Egorov; D. M. Egorov;
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正文语种 eng
中图分类航空;
关键词
Comprehensive numerical analysis; Intrachamber processes; Propellant web burnout; Nozzleless solid propellant rocket engine;

机译：综合数值分析;舱内工艺;推进剂燃尽;无喷嘴固体推进剂火箭发动机;

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1. Numerical Study of Intrachamber Processes Dynamics at Nozzleless Solid Propellant Rocket Engine Actuation [J] . M. Yu. Egorov, D. M. Egorov Russian Aeronautics . 2013,第1期

机译：无喷嘴固体推进剂火箭发动机启动室内过程动力学的数值研究
2. Numerical Modeling of the Processes within the Combustion Chamber of a Solid Propellant Rocket Engine during the Stabilization of the Design Operation Mode [J] . G. N. Amarantov, M. Yu. Egorov, S. M. Egorov, Fluid Dynamics . 2011,第3期

机译：设计运行模式稳定过程中固体推进剂火箭发动机燃烧室内过程的数值模拟
3. Study of Interchamber Processes when Starting Water-Filled Solid Propellant Rocket Engines [J] . V.D.Barsukov, S.V.Goldaev Известия　Высших　учебных　заведений: Авиационная　техника . 2000,第2期

机译：启动充水固体推进剂火箭发动机的舱间过程的研究
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机译：固体火箭推进剂燃烧过程中加热层物理和化学过程的数值模拟
5. Experimental study of mixing and combustion processes in a solid propellant ducted rocket motor. [D] . Chuang, Chin-Lung. 1989

机译：固体推进剂管道火箭发动机混合与燃烧过程的实验研究。
6. Studies in the Meaning and Relationships of Birth and Death Rates: IV. On the Range of Instances in which Geometrical Progressions describe numerically processes of life i.e. those processes which might be explained by a monomolecular reaction [O] . John Brownlee 1915

机译：出生率和死亡率的意义及其关系的研究：IV。在几何级数描述生命过程的实例范围内即那些可能由单分子反应解释的过程
7. NUMERICAL STUDY OF DYNAMICS INTRACHAMBER PROCESSES IN SOLID PROPELLANT SUSTAINER TAKING INTO ACCOUNT FLIGHT OVERLOADS. PART 2. CALCULATION RESULTS [O] . Mikhail Egorov, Dmitry Egorov, Sergey Egorov 2021

机译：实体推进剂持续载于考虑飞行超负荷的动力学内夹层过程的数值研究。第2.计算结果
8. Gas Dynamics of Solid-Propellant Rocket Engines [R] . Shishkov, A. A. 1969

机译：固体推进剂火箭发动机的气体动力学

Numerical Study of Intrachamber Processes Dynamics at Nozzleless Solid Propellant Rocket Engine Actuation

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