Journal of Dynamics and VibroacousticsJournal of Dynamics and Vibroacoustics2409-4579Samara National Research University293910.18287/2409-4579-2015-2-2-6-15UnknownPROCESS MODELING ELECTRO-HYDRAULIC CONTROL SYSTEM CANCELED OR RE-LAUNCH ROCKET ENGINE SOLID FUELBachurinA. B.bachurinsasha1987@mail.ruStrelnikovE. V.e_strelnikov@mail.ruTselischevV. A.pgl.ugatu@mail.ruUfa State Aviation Technical University
Ufa, Ul. K. Marksa, 12 Russia, 45000020112015226152501201626012016Copyright © 2017,2017<p><em>Within the framework of the contemporary problem solving serial use of solid propulsion in space industry related disabilities deep traction control module and multiple on-off setting, proposed the introduction of a combined system of governance. The article provides a diagram of a controlled rocket propulsion system, equipped with a dual-circuit electrohydraulic control system, and describes how to control laid down in its foundation.The analysis of transients in a rocket engine solid fuel in separate and combined use of control subsystems responsible for the extinction of the engine and preparing to re-launch.</em></p>Solid rocket motorrefrigerantcombined management systemdynamic modelsteering gearРакетный двигатель твёрдого топливахладагенткомбинированная система управления гашениемдинамическая модельрулевая машинарегулятор расходатяга[[1] Petrenko, V.I., Sokolowsky, M.I., Zykov, A., Lyanguzov, S.V., Todoschenko, A.I., Popov, V.L., Potapov, B.F., Sevastiyanov, V.V. and Yarushin S.G. (2003), Upravliyemie energeticheskie ustanovki na tverdom toplive [Managed power plants for solid propellants], in Sokolowsky, M.I.(ed.) and Petrenko, V.I. (ed.), Mechanical Engineering, Moscow, Russia.][[2] Krivosheev, I.A., Tselischev, V.A., Bachurin, A.B. and Strel'nikov, E.V. (2012), Opyt razrabotki kombinirovannogo RDTT mnogokratnogo vkljuchenija [Experience development combined SRM inclusion of multiple], (in Russian), Vestnik UGATU, vol. 16, no. 2 (47), pp. 174-188.][[3] Akhmetov, Y.A., Bachurin, A.B., Strelnikov, E.V. and Tselichev, V.A., Ufa State Aviation Technical University (2012), Reguliruemyj raketnyj dvigatel' tverdogo topliva [Adjustable solid propellant motor], Russia, Pat. 2443895 MPK F02K9/92 F02K9/86.][[4] Prisnyakov, V.F. (1984), Dinamika racketnih dvigatelei tverdogo topliva [Dynamics of solid rocket motor fuel]. Textbook for universities, Mechanical Engineering, Moscow, Russia.][[5] Zezin, V.G., Petrenko, V.I., Popov, V.L., Rusak, A.M., Savchenko, V.I., Simonov, E.A. and Feofilaktov V.I. (1996), Reguliruemye tverdotoplivnye dvigatel'nye ustanovki [Adjustable solid propulsion systems], Miass: SRC.][[6] Mesropyan, A.V. and Tselishev, V.A. (2008), Modelirovanie gidravlicheskih rulevyh mashin [Modeling of hydraulic steering gears], Ufa: USATU.]