REDUCTION OF THE TEMPERATURE AND FORCE IMPACT OF SUPERSONIC JETS OF A ROCKET ENGINE ON OBJECTS OF GROUND TECHNOLOGICAL EQUIPMENT

  • R. Mochonov Yuzhnoye State Design Office
  • А. Sotnichenko Yuzhnoye State Design Office
  • H. Ivanytskyi Yuzhnoye State Design Office
  • М. Salo Yuzhnoye State Design Office
  • O. Brizhak Yuzhnoye State Design Office
Keywords: SUPPLY WATER SYSTEM, SUPERSONIC JET, FLAME DEFLECTOR, EVAPORATION, NUMERICAL SIMULATION, LAGRANGE APPROACH, ANSYS FLUENT.

Abstract

To prevent surfaces flowing under direct impact of high-temperature gas jets, the majority of up-to-date launch complexes of integrated launch vehicles (ILV) apply water feed systems. Nowadays the only feasible way of theoretical research of interaction of propulsion systems supersonic jets with water jets from water feed system headers is numerical simulation. To investigate thermal and force load on surfaces under impact of supersonic jets from propulsion system we carried out numerical simulation of gas-dynamic process in gas duct during integrated launch vehicle takeoff. We investigated the two options, with and without water feed. We took the Antares ILV gas duct as a prototype. Our mathematical model is based on the two-phase medium dynamics equations. At this, the gas flow is described by the three-dimensional Navier-Stokes equations, and at simulation of water drops we applied Lagrange trajectory approach. The research was done in commercial code ANSYS Fluent. As a result of the numerical experiment we got data on efficiency of reduction of thermal and force impact of propulsion system supersonic jets on gas duct structure at use of water feed system. Based on the research we worked out the key recommendations that might be of use at design and optimization of water feed systems of ILV ground complexes.

Author Biographies

R. Mochonov, Yuzhnoye State Design Office

Украина ГП «КБ «Южное» им. М.К. Янгеля», инженер-конструктор 1-й категории.

Сфера интересов - вычислительная гидродинамика и теплообмен при разработке космической техники.

А. Sotnichenko, Yuzhnoye State Design Office

Украина. ГП «КБ «Южное» им. М.К. Янгеля», начальник группы.

Сфера интересов - архитектура и размещение наземного технологического оборудования ракетно-космических комплексов.

H. Ivanytskyi, Yuzhnoye State Design Office

Украина. ГП «КБ «Южное» им. М.К. Янгеля», начальник лаборатории.

Сфера интересов - системы заправки и другие пневмогидравлические системы наземного технологического оборудования ракетно-космических комплексов.

М. Salo, Yuzhnoye State Design Office

Украина. ГП «КБ «Южное» им. М.К. Янгеля», начальник сектора.

Сфера интересов – исследование тепломссообменных процессов в наземном оборудовании ракет-носителей.

O. Brizhak, Yuzhnoye State Design Office

ГП «КБ «Южное» им. М.К. Янгеля», инженер-конструктор 1-й категории.

Сфера интересов - разработка 3D-моделей наземного технологического оборудования ракетно-космических комплексов.

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Published
2021-11-17
How to Cite
Mochonov, R., SotnichenkoА., Ivanytskyi, H., SaloМ., & BrizhakО. (2021). REDUCTION OF THE TEMPERATURE AND FORCE IMPACT OF SUPERSONIC JETS OF A ROCKET ENGINE ON OBJECTS OF GROUND TECHNOLOGICAL EQUIPMENT. Journal of Rocket-Space Technology, 29(4), 12-28. https://doi.org/10.15421/452102