Analysis of properties of inertia regulator of thrust control system of liquid rocket engine
The quality of the flight task of a space rocket system is determined among other things by the accuracy of maintaining and regulating the thrust of the rocket engine. Improving the accuracy and reducing errors in the engine mode control system will reduce the cost of space launches or allow you t...
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| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education
2021-06-01
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| Series: | Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение" |
| Subjects: | |
| Online Access: | https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2021/%D0%A2.%205,%20%E2%84%96%202%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/98-105%20%D0%94%D1%80%D0%BE%D0%BD%D1%8C%20%D0%9C.%20%D0%9C.,%20%D0%AF%D0%BA%D0%BE%D0%B2%D0%BB%D0%B5%D0%B2%20%20%D0%90.%20%D0%91..pdf |
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| Summary: | The quality of the flight task of a space rocket system is determined among other things by the accuracy
of maintaining and regulating the thrust of the rocket engine. Improving the accuracy and reducing
errors in the engine mode control system will reduce the cost of space launches or allow you to put
a large payload into orbit. The article presents a mathematical model of a controller with an inertial
booster of a liquid-propellant rocket engine, identifies parameters and values that affect its accuracy,
and considers measures to reduce static error |
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| ISSN: | 2588-0373 2587-764X |