Modeling of electro-hydraulic controlled propulsion system

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Abstract

Modern rocket propulsion system is a dynamic system with a set of inter- connected links Modern controlled propulsion system, ensuring in the pro- cess of its operation on the aircraft receiving the given basic characteristics. Main propulsion controlled variable serving as controlled object is second mass flow of gases through the nozzle. Regulating influence area is man- aged throttle hydraulic adjusting the surface area of solid fuel combustion by draining the channel charge. Currently achieved level of development of computer technology allows to simulate the behavior of the object and its management systems. This helps improve the design quality and reduce de- bugging time hydroelectric generators.

About the authors

A. B. Bachurin

Ufa State Aviation Technical University

Email: bachurinsasha@rambler.ru
Russian Federation

E. V. Strelnikov

Ufa State Aviation Technical University

Email: bachurinsasha@rambler.ru
Russian Federation

V. A. Tselischev

Ufa State Aviation Technical University

Author for correspondence.
Email: bachurinsasha@rambler.ru
Russian Federation

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Copyright (c) 2015 Journal of Dynamics and Vibroacoustics


Journal of Dynamics and Vibroacoustics

ISSN 2409-4579 (Online)

Publisher and Founder: Samara National Research University, 34, Moskovskoye shosse, Samara, 443086, Russian Federation.

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Editor-in-chief:  Academician of the RAS
E. V. Shakhmatov 

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