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

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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

candidate of technical science, associate professor

Russian Federation

A. V. Sulinov

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

Email: ke_src@ssau.ru

candidate of technical science, associate professor

Russian Federation

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