Dynamics of tank propellant head control system

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Abstract

In the paper the impact of the axial acceleration factor on dynamic characteristics of the pressure controls of the gas pillow of liquid-propellant rocket’s fuel tank is considered. Frequency responses are defined. Possible applications of the developed model are proposed.

 

Key words: pilot operated gas pressure controller, axial acceleration factor, control system dynamics, gain and phase frequency responses 

About the authors

D. M. Stadnik

Самарский государственный аэрокосмический университет имени академика С. П. Королёва

Email: sdm-63@bk.ru
Russian Federation

V. Y. Sverbilov

Самарский государственный аэрокосмический университет имени академика С. П. Королёва

Author for correspondence.
Email: pas@ssau.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.

Extract from the register of registered media

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

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Address for correspondence: 34, Moskovskoye shosse, Samara, 443086, Russian Federation, Samara National Research University (room 324, building 14)

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e-mail: dynvibro@ssau.ru

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