Email this article THE INVESTIGATION OF THE STABILITY OF THE PROPELLANT INTAKE IN CARRIER ROCKET WITH MONOPROPELLANT ROCKET ENGINE
- Authors: Diachenko M.I.1, Temnov A.N.1
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Affiliations:
- Bauman Moscow State Technical University 5/1, ul. Baumanskaya 2-ya, Moscow, 105005, Russia
- Issue: Vol 2, No 2 (2015)
- Pages: 27-33
- Section: Articles
- URL: https://dynvibro.ru/dynvibro/article/view/4272
- DOI: https://doi.org/10.18287/2409-4579-2015-2-2-27-33
- ID: 4272
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Abstract
The problem of propellant free oscillations in cylindrical and conical tanks is considered and solutions presented with boundary conditions on a free surface and the surface of intake which if speak figuratively provides a resistance to the fluid descent; the special attention was given to research influences the propellant intake on appearance Pogo effect. Such problems have come from the purpose to increase efficiency and output performance of the multistage cluster rockets by a central stage fueling from the side stages of a cluster.
About the authors
M. I. Diachenko
Bauman Moscow State Technical University5/1, ul. Baumanskaya 2-ya, Moscow, 105005, Russia
Author for correspondence.
Email: morenov.sv@ssau.ru
A. N. Temnov
Bauman Moscow State Technical University5/1, ul. Baumanskaya 2-ya, Moscow, 105005, Russia
Email: morenov.sv@ssau.ru
References
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