Email this article Dynamics of tank propellant head control system
- Authors: Stadnik D.M.1, Sverbilov V.Y.1
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Affiliations:
- Самарский государственный аэрокосмический университет имени академика С. П. Королёва
- Issue: Vol 1, No 1 (2014)
- Pages: 24-27
- Section: Articles
- Published: 22.06.2014
- URL: https://dynvibro.ru/dynvibro/article/view/1650
- DOI: https://doi.org/10.18287/2409-4579-2014-1-1-24-27
- ID: 1650
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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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