Thrust Vector Control of Solid Propellant Operative-Tactical Rockets
Authors
-
Mykola Bondarenko
Oles Honchar Dnipro National University
Author
https://orcid.org/0009-0008-8421-8408
-
Volodymyr Habrinets
Oles Honchar Dnipro National University
Author
https://orcid.org/0000-0002-6115-7162
Abstract
In modern military conflicts, the role of operative-tactical rockets has significantly increased as they are an effective means of delivering strikes over long distances. However, to successfully accomplish missions, it is necessary to ensure the effective operation of the control systems of these rockets and protect them from enemy air defense systems. Among the various measures used to counter enemy air defense systems, thrust vector control of solid propellant rocket engines (TVC) plays an important role. This method allows changing the direction of the rocket's movement and increasing its maneuverability, making it less vulnerable to anti-missile systems. This article discusses the basic principles of thrust vector control of solid propellant operative-tactical rocket engines and their use in countering enemy systems. The possibilities and limitations of applying this method in different combat conditions are also analyzed.
Downloads
References
Габрінець В. О., Горбенко Г. О., Гумницький В. П. Основи теорії та проектування РДТП. Підручник, Дн-ськ, Арт-Пресс, 2005, 198 с.
ГП «Государственное Киевское конструкторское бюро «Луч», Каталог продукции, 2021, 44 с.
Шапошник В. І., Качер В. О., & Курдюков О. Ю. (2016). Аналіз методів керування вектором тяги при створенні зразків твердопаливних ракет. Науково-технічний журнал "Вісник Війсь-кової академії України", 1 (45), 148-155.
Liu, X., & Luo, Z. (2019). Control of solid rocket motors. Pro-gress in Aerospace Sciences, 74, 28-55 с.
Н. С. Голубенко, Б. И. Кушнир, В. А. Зензеров. Опыт отра-ботки органов управления вектором тяги РДТТ, Космическая тех-ника. Ракетное вооружение. 2016. Вып. 1 (111), 13-18 с.
Chen, C. F., & Lin, Y. F. (2018). A review of missile attitude control systems. Journal of Guidance, Control, and Dynamics, 34(3), 676-687 с.
Miller, D. W., & Volden, J. (2019). The Art of Missile Guid-ance. American Scientist, 102(6), 416-423 с.
Downloads
Published
Issue
Section
License
Copyright (c) 2024 Challenges and Issues of Modern Science
This work is licensed under a Creative Commons Attribution 4.0 International License.
All articles published in the journal Challenges and Issues of Modern Science are licensed under the Creative Commons Attribution 4.0 International (CC BY) license. This means that you are free to:
- Share, copy, and redistribute the article in any medium or format
- Adapt, remix, transform, and build upon the article
as long as you provide appropriate credit to the original work, include the authors' names, article title, journal name, and indicate that the work is licensed under CC BY. Any use of the material should not imply endorsement by the authors or the journal.
