The method of neutralization of propellant compartments of rockets and maneuvering spacecrafts after propellant damping out of tanks

机译：推进剂抑制罐中火箭射箭推进室和机动航天器的中和方法

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The paper is devoted to the method of neutralization of propellant compartments of rockets and spacecrafts and the mathematical model of rocket fuel combustion process in two-dimensional turbulent flow is presented. For closure of the equation system the k-/spl epsi/ turbulence model is used.

机译：本文讨论了火箭和航天器的推进剂隔室的中和的方法，并提出了二维湍流中火箭燃料燃烧过程的数学模型。为了关闭等式系统，使用K-/ SPL EPSI /湍流模型。

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《Korea-Russia International Symposium on Science and Technology》|2003年||共3页
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Rotova O.G.;
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中图分类自动化技术、计算机技术;
关键词
rocket engines; combustion; turbulence; flow simulation; aerospace propulsion; neutralization; propellant compartments; rockets; spacecraft; rocket fuel combustion process; two-dimensional turbulent flow;

机译：火箭发动机;燃烧;湍流;流动模拟;航空推进;中和;推进剂隔室;火箭;航天器;火箭燃料燃烧过程;二维湍流;

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专利

1. On spacecraft maneuvers control subject to propellant engine modes [J] . Mazinan A. H. ISA Transactions . 2015,第Null期

机译：在航天器操纵控制受推进剂发动机模式的控制
2. Multi-objective Optimization of Zero Propellant Spacecraft Attitude Maneuvers [J] . Zhang S., Tang G. J., Friswell M. I., Journal of Optimization Theory and Applications . 2014,第3期

机译：零推进器航天器姿态操纵的多目标优化
3. Damping device to reduce the risk of injection-coupled combustion instabilities in liquid propellant rocket engines [J] . Armbruster Wolfgang, Hardi Justin S., Miene Yannik, Acta astronautica . 2020,第Apra期

机译：阻尼装置可降低液体推进剂火箭发动机中喷射耦合燃烧不稳定性的风险
4. The method of neutralization of propellant compartments of rockets and maneuvering spacecrafts after propellant damping out of tanks [C] . Rotova, O.G. . 2003

机译：推进剂从舱内阻尼后中和火箭和机动航天器推进剂舱的方法
5. Spatio-temporal atmospheric density forecasting for drag-based propellant-less spacecraft maneuvering: Theory and mission design [D] . Guglielmo, David. 2015

机译：基于阻力的无推进剂航天器机动的时空大气密度预测：理论与任务设计
6. Examination of the liver in personnel working with liquid rocket propellant [O] . Palle Petersen, Erik Bredahl, Ove Lauritsen, 1970

机译：液体火箭推进剂工作人员的肝脏检查
7. Synthesis of calculational methods for the design and analysis of radiation shields for nuclear rocket systems. Volume I. Radiation measurements in a nuclear rocket propellant tank mockup using simulated liquid hydrogen [O] . H.C. Woodsum, J. Rowland 1968

机译：核火箭系统辐射屏蔽设计与分析的综合。体积I.使用模拟液体氢气的核火箭推进剂罐模型中的辐射测量
8. Synthesis of calculational methods for the design and analysis of radiation shields for nuclear rocket systems. Volume 1 - Radiation measurements in a nuclear rocket propellant tank mockup using simulated liquid hydrogen [R] . Rowland, J., Woodsum, H. C. 1968

机译：核火箭系统辐射防护设计与分析计算方法的综合。第1卷 - 使用模拟液态氢的核火箭推进剂罐模型中的辐射测量

The method of neutralization of propellant compartments of rockets and maneuvering spacecrafts after propellant damping out of tanks

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