Influence in a constructive and regime parameters antechamber by operation-in the combustion chamber liquid-propellant rocket engine thrusters on hypergolic liquid propellants

Abstract


The article presents the results of theoretical and experimental studies on intensification through antechamber major limiting stages of the flow of the working process in the combustion chamber: the gasification of liquid phase intermediates and evaporation of unreacted fuel components Comrade through the organization of effective secondary crushing and mixing of gas-phase and mouth-injuries of large-scale non-uniformity of the ratio of the fuel components in the cross section through heavy turbulence in gas-phase intermediates


About the authors

V. E. Nigodjuk

Samara State Aerospace University named after academician S.P. Korolyov (National Research University)

Author for correspondence.
Email: ke_src@ssau.ru

Russian Federation

candidate of technical science, associate professor

A. V. Sulinov

Samara State Aerospace University named after academician S.P. Korolyov (National Research University)

Email: ke_src@ssau.ru

Russian Federation

candidate of technical science, associate professor

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