Development of mathematical model of processes in gas generator with unitary fuel for powering turbine of liquid rocket engine

Authors

DOI:

https://doi.org/10.25206/2588-0373-2023-7-3-82-88

Keywords:

dynamic processes, automatic control system, single-component gas generator, throttle valve, liquid rocket fuel

Abstract

The article considers the dynamic model of a gas generator with control throttle of liquid rocket engine with pumping supply system and unitary fuel for powering the turbine. The system of dynamic equations describing the processes occurring in a single-component gas generator and a throttle valve is obtained. The mathematical model makes it possible to analyze and identify the main patterns of the influence of input quantities on the controlled quantity.

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Author Biography

Yakovlev Aleksey Borisovich, Omsk State Technical University, Omsk, Russia

Candidate of Technical Sciences, Associate Professor, Head of Aircraft and Rocket Building Department, Omsk State Technical University, Omsk.

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Abstract views: 30

Published

2023-10-27

How to Cite

Yakovlev А. Б. (2023). Development of mathematical model of processes in gas generator with unitary fuel for powering turbine of liquid rocket engine. Omsk Scientific Bulletin. Series «Aviation-Rocket and Power Engineering», 7(3), 82–88. https://doi.org/10.25206/2588-0373-2023-7-3-82-88

Issue

Vol. 7 No. 3 (2023)

Section

Aviation and rocket-space engineering

License

Non-exclusive rights to the article are transferred to the journal in full accordance with the Creative Commons License BY-NC-SA 4.0 «Attribution-NonCommercial-ShareAlike 4.0 Worldwide License (CC BY-NC-SA 4.0»)

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