Investigation of properties of system of automatic control of liquid-propellant rocket propulsion system with integrating regulator

Investigation of properties of system of automatic control of liquid-propellant rocket propulsion system with integrating regulator

There are considered the dynamic properties of the system of automatic control of the unitary fuel supply to a singlecomponent gas generator of a liquid rocket engine. There are obtained differential equations describing the operation of the comparison element, the throttle valve, the hydraulic...

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Bibliographic Details
Main Authors: I. A. Kyzmenko, A. B. Yakovlev
Format: Article
Language:English
Published: Omsk State Technical University, Federal State Autonoumos Educational Institution of Higher Education 2019-03-01
Series:Омский научный вестник
Subjects:
liquid rocket engine
unitary fuel
liquid gas generator
control system
Online Access:https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2019/1%20(163)/17-21%20%D0%9A%D1%83%D0%B7%D1%8C%D0%BC%D0%B5%D0%BD%D0%BA%D0%BE%20%D0%98.%20%D0%90.,%20%D0%AF%D0%BA%D0%BE%D0%B2%D0%BB%D0%B5%D0%B2%20%D0%90.%20%D0%91..pdf
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https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2019/1%20(163)/17-21%20%D0%9A%D1%83%D0%B7%D1%8C%D0%BC%D0%B5%D0%BD%D0%BA%D0%BE%20%D0%98.%20%D0%90.,%20%D0%AF%D0%BA%D0%BE%D0%B2%D0%BB%D0%B5%D0%B2%20%D0%90.%20%D0%91..pdf

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