THE INVESTIGATION OF THE STABILITY OF THE PROPELLANT INTAKE IN CARRIER ROCKET WITH MONOPROPELLANT ROCKET ENGINE

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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 University
5/1, ul. Baumanskaya 2-ya, Moscow, 105005, Russia

Author for correspondence.
Email: morenov.sv@ssau.ru

A. N. Temnov

Bauman Moscow State Technical University
5/1, ul. Baumanskaya 2-ya, Moscow, 105005, Russia

Email: morenov.sv@ssau.ru

References

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  2. Gordeev, V.A., Zhukov, V.A., Zavadskiy, V.K., Ivanov, V.P, Kablova, E.B., Klenova, L.G. and Mozzhorina, M.Y. (2010), Princypy postroeniya i strukturnye skhemy upravleniya rashodovaniem topliva i nadduva bakov RN s gidravlicheskimi svyazyami mezhdu bokovymi I tsentralnym blokami , Mashinostroenie, Moscow, Russia, pp. 331-337.
  3. Kolesnikov, K.S, (2003). Dinamika raket , Mashinostroenie, Moscow, Russia, 520 p.
  4. Birkin, I.A. (2011), Ob effektivnosti pereliva topliva mezhdu raketnymi stupenyami Aktual‘nye problemy rossiyskoy kosmonavtiki. – Materialy XXXY akademicheskikh chteniy po kosmonavtike, Moscow, pp. 42-43.
  5. Kirillov, V.V. (1960), Issledovanie kolebaniy zhidkosti v nepodvizhnom sosude s uchetom ee vytekaniya , Trudy MFTI, Moscow, Russia, vol. 5, pp. 19-25.

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Copyright (c) 2017 М. И. Дьяченко, А. Н. Темнов

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Journal of Dynamics and Vibroacoustics

ISSN 2409-4579 (Online)

Publisher and Founder: Samara National Research University, 34, Moskovskoye shosse, Samara, 443086, Russian Federation.

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Editor-in-chief:  Academician of the RAS
E. V. Shakhmatov 

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