Search

Development of advanced low thrust rocket engines with ecologically friendly propellants

1 1., 1 1., 1 1.

(Rus)

Research of methods for protection the surface of cryogenic tanks from ice formation

1 1., 1 1., 1 1.

(Rus)

Vol 12, No 2 (2013)

Investigation of energy parameters of small-thrust liquid rocket engines with the geometric expansion ratio of the nozzle F=200

Ageenko Y.I., Nigodyuk V.E., Ryzhkov V.V., Sulinov A.V., Shustov S.A.

(Rus)

Vol 19, No 4 (2020)

Development of improved performance electromagnetic valve for liquid rocket engine

Igolkin A.A., Chubenko T.A., Maksimov A.D.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

Aspects of the numerical method calculating thermogazodynamic lrest based on not perfect passing of workflows in the combustion chamber

Silyutin M.V., Shustov S.A.

(Rus)

Vol 17, No 4 (2018)

Numerical simulation of low liquid flow in a mixer consisting of two centrifugal swirlers

Semkin E.V.

(Rus)

Vol 15, No 4 (2016)

Method of transient simulation of combustion processes in a low-thrust rocket engine operating on gaseous hydrogen and oxygen

Zubanov V.M., Shabliy L.S., Stepanov D.V.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

11D58MF combined propulsion unit operating on oxygen-hydrogen fuel for an average-sized booster

Lupyak D.S., Smolentsev A.A., Sokolov B.A., Tumanin E.N., Tupitsin N.N.

(Rus)

Vol 11, No 3-3 (2012): Special Issue

Research of influence of the thermal stream from the mid-flight liquid rocket engine on parameters of operating liquid rocket engines of small draught in the conditions of perspective razgonnogo's propulsion system of the block

Ageenko Y.I., Galperin R.N., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.

(Rus)

Vol 11, No 2 (2012)

Principles of constructing systems and objects of a middle-class space rocket complex with increased load-carrying capacity

Baranov D.A., Yelenev V.D., Smorodin A.V.

(Rus)

Vol 10, No 1 (2011)

Definition of directions of developing methods, technical decisions and means of decreasing the technogenic influence on the environment for the omplementation on board of space launch vehicles

Shatrov Y.T., Baranov D.A., Trushlyakov V.I., Kudentsov V.Y.

(Rus)

Oxyhydrogen propulsion device base on water electrolysis and lrest on component H2 + O2 for control system SS

1 1., 1 1., 1 1., 1 1., 1 1.

(Rus)

Vol 8, No 2 (2009)

Developing an electronic reference book on thermogasodynamic properties of rocket engine fuel combustion products taking into account non-ideal character of the working process

Silyutin M.V.

(Rus)

Vol 12, No 4 (2013)

The usage of high power supply capacity transport spacecraft

Ivanovich S.N.

(Rus)

Vol 19, No 1 (2020)

Bringing spacecraft into solar-oriented attitude by the measurements of a single-axis angular-rate sensor and an optical solar sensor

Shipov M.G., Steklova A.A., Davydov A.A.

(Rus)

Research of the possibility of thermal conditions LREST using an infrared thermal imaging system

Ryzhkov V.V., Silyutin M.V.

(Rus)

Vol 17, No 4 (2018)

Propulsion systems and low-thrust rocket engines based on various physical principles for control systems of small and micro-spacecraft

Ryzhkov V.V., Sulinov A.V.

(Rus)

Vol 15, No 4 (2016)

Efficiency of aft diffusers in vacuum systems of test benches for high-altitude firing tests of low-thrust liquid rocket engines

Galperin R.N., Gulyaev Y.I., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.

(Rus)

Vol 11, No 3-3 (2012): Special Issue

On a method of practical training fulfillment for course of studies “Design of Main Units and Systems of Engine”

Borisov V.A., Zhizhkin A.M.

(Rus)

Vol 12, No 3-2 (2013): Vestnik SSAU

Approaches to the evaluation of fuels for hypersonic engines

Sergeev S.M., Petrukhin N.V.

(Rus)

Vol 9, No 4 (2010)

Providing carrier rocket motion controllability on the basis of design smoothed wind profile application

Yendutkina Y.A., Titov B.A.

(Rus)

About the centre of science-educational of laser systems and technologies at faculty DLA SSAU

1 1., 1 1., 1 1.

(Rus)

Vol 8, No 1 (2009)

Reputation of enterprises competing in the market from the point of view of consumers

Ivanov D.Y., Kirilina Y.V.

(Rus)

Vol 19, No 1 (2020)

Mathematical model of the “tank – nozzle” cooling system

Shalay V.V., Shcherban K.V.

(Rus)

Influence in a constructive and regime parameters antechamber by operation-in the combustion chamber liquid-propellant rocket engine thrusters on hypergolic liquid propellants

Nigodjuk V.E., Sulinov A.V.

(Rus)

Vol 17, No 4 (2018)

Proposals for improving the efficiency and service life of the turbines of turbo-pump assemblies in liquid-propellant rocket engines by using double-sided crest-type radial labyrinth seals

Levochkin P.S., Chvanov V.K., Vasiliev V.S., Timushev S.F.

(Rus)

Vol 10, No 6 (2011)

Motion of an upper stage rocket with a toroidal tank around the mass center in parameters of Cayley-Klein

Alekseev A.V., Krasnikov V.S.

(Rus)

Vol 13, No 5-2 (2014): Special Issue

Automated thermovacuum firing test facility for testing and research of workflow in low-thrust rocket engine on hypergolic propellants

Galperin R.N., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.

(Rus)

Vol 11, No 3-3 (2012): Special Issue

Ways to improve the workflow of liquid rocket thrusters on hypergolic propellants

Nigodjuk V.E., Sulinov A.V.

(Rus)

Vol 12, No 3-2 (2013): Vestnik SSAU

Forecasting the individual performance capabilities of the rocket engine powerplant units at the maintanance stage

Biryuk V.V., Bronshtein V.M., Presnyakova A.S., Shatilova M.Y., Dostovalova S.S.

(Rus)

The flowing reactor as the tool of an experimental research of processes of transformation self-igniting liquid rocket fuel

1 1., 1 1.

(Rus)

Vol 8, No 1 (2009)

Experimental analysis of flow separation in low thrust rocket engine nozzles with a profiled supersonic part of the nozzle

Shustov S.A.

(Rus)

Vol 21, No 3 (2022)

Gas-dynamic losses in the flow part of the channel charge of a solid-propellant rocket engine

A. N. Sabirzyanov A.N., Khamatnurova C.B., Kuzmin V.V.

(Rus)

Vol 19, No 1 (2020)

Method of calculating dynamic designs of space launch vehicles for designing systems of stabilization of their motion

Lobanov V.A.

(Rus)

Increasing the energy efficiency of liquid rocket engine of small thrust (0,1-1,0) N with jet scheme of mixing

Nigodjuk V.E., Sulinov A.V.

(Rus)

Vol 17, No 3 (2018)

Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines

Ryzhkov V.V., Morozov I.I.

(Rus)

Vol 14, No 3-2 (2015): Special Issue

Procedure of validated CFD-modeling of a two-stage screw-centrifugal pump

Zubanov V.M., Shabliy L.S., Krivtsov A.V., Ivanov A.I., Kositsin I.P., Baturin N.V.

(Rus)

Vol 13, No 5-1 (2014): Special Issue

CFD-modeling of processes in a high-pressure oxidizer pump for the turbopump assembly of a liquid rocket engine

Zubanov V.M., Shabliy L.S.

(Rus)

Vol 11, No 3-2 (2012): Special Issue

Oxygen-hidrogen liquid rocket engine using turbo-pump developed for aviation hidrogen liquid two-spool turbo-jet

Ivanov A.I., Borisov V.A.

(Rus)

Vol 13, No 1 (2014)

Constructive actions for decreasing the acoustic pressure inside space-rocket products

Popov P.A., Sindyukov A.A.

(Rus)

Vol 9, No 1 (2010)

Assessment of technicaland economical efficiency of developing carrier rockets with first-stage reusable units

1 1., 1 1.

(Rus)

Mathematical model of small-thrust rocket engine with gaseous oxygen and hydrogen in pulse operation

1 1.

(Rus)

Vol 8, No 1 (2009)

Determining flow regimes around rocket boosters on a part of the launch orbit

Kharitonova A.N.

(Rus)

Vol 18, No 4 (2019)

Computer-aided design of low-thust rocket engines using the domain-specific knowledge database and CAE / CAD systems

Ryzhkov V.V., Morozov I.I., Lapshin E.A.

(Rus)

Physical workflow model in the combustion chamber LREST with a jet-centrifugal jets on hypergolic propellants

Silyutin M.V., Shustov S.A.

(Rus)

Vol 16, No 2 (2017)

Assessment of a liquid rocket engine concept based on innovative technologies

Solodovnikov A.V., Akinshin I.A., Golubyatnik V.V., Krivonogov A.V.

(Rus)

Vol 10, No 4 (2011)

Development of the method of valuating the level of competitiveness of industrial enterprises working in the sphere of space-rocket engineering

Kirilina E.V.

(Rus)

Vol 13, No 5-1 (2014): Special Issue

Research of the influence of design parameters of a 400 N-thrust low-thrust liquid rocket engine on its energy efficiency

Ageenko Y.I., Ilyin R.V., Pegin I.V.

(Rus)

Vol 11, No 3-1 (2012): Special Issue

Influence of high technologies on production technological prototypes of missile engines

Kodencev S.N., Suhochev G.A.

(Rus)

Vol 13, No 1 (2014)

Analysis of nonstationary thermal state of a low-thrust liquid rocket engine taking into account injection, evaporation and combustion of liquid fuel droplets

Vorobiev A.G., Borovik I.N., Ha S.

(Rus)

Мethod of design calculation of centrifugal emulsive duplex fuel nozzle

1 1.

(Rus)

Vol 7, No 3 (2008): Special Issue

A model of motion of monodispersible gas-liquid stream is in transzvukovoy of part of rocket chamber

Еpishchenko S.V., Pervishin A.N.

(Rus)

Vol 21, No 1 (2022)

On the efficiency of using the Navier-Stokes approximation in thermogasdynamic calculation of low-thrust liquid-propellant rocket engines at low Reynolds numbers

Maksimov A.D., Shustov S.A.

(Rus)

Vol 18, No 3 (2019)

Сalculated analysis of the influence of operation and design factors on the parameters of oxygen-hydrogen low-thrust rocket engines

Ryzhkov V.V., Morozov I.I.

(Rus)

Method of design calculation gas-liquid jet duplex fuel nozzle with internal mixing

Egorychev V.S.

(Rus)

Vol 16, No 2 (2017)

Multi-purpose high-precision thermal vacuum testing bench and someresults of firing tests of non-hypergolic low-thrust rocket engines

Ryzhkov V.V., Verjasov Y.N., Galperin R.N., Gulyaev Y.I., Ivashin Y.S.

(Rus)

Vol 14, No 1 (2015)

Vortex cleaning of fuel tank pressurant gas

Biryuk V.V., Shimanov A.A., Onoprienko D.A., Smorodin A.V., Shepelev A.I.

(Rus)

Vol 13, No 5-1 (2014): Special Issue

Experimental verification of the possibility of improving the liquid propelant rocket engine performance for the “Vega” launcher upper stage

Kovalenko A.N., Pereverzev V.G., Marchan R.A., Blishun Y.V.

(Rus)

Vol 11, No 3-1 (2012): Special Issue

Development liquid roket engine on component fuel liquefied natural gas and oxygen for reusable space launching systems

Efimochkin A.F., Khrisanfov S.P., Golubyatnik V.V., Kafarena P.V., Yeliseyev A.V.

(Rus)

Vol 13, No 1 (2014)

Analysis of nonstationary thermal state of low-thrust liquid rocket engine with high-concentration hydrogen peroxide and kerosene propellant with film cooling

Vorobiev A.G., Borovik I.N., Ha S.

(Rus)

Experimental determination of the side forces acting on the combustion chamber in the altitude chamber at startup

, , , ,

(Rus)

Features of calculation of hydraulic characteristics of capillary spray jets of is liquid-stnyh rocket engines of small pull-rod

1 1., 1 1., 1 1.

(Rus)

Vol 12, No 1 (2013)

Unit impulse input tests of a system of the «Frigate» upper-stage rocket

Mikhalenkov N.A., Yermakov V.Y., Utkina Y.I.

(Rus)

Vol 20, No 4 (2021)

The structure of knowledge base to support the development of low-thrust liquid-propellant rocket engines based on computer technologies

Ryzhkov V.V.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

Working process of gaseous fuel metallizator

Pervyshin A.N., Ryazanov A.I.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

The numerical modelling of processes in combustion chambers of low thrust rocket engines

Salich V.L.

(Rus)

Vol 15, No 4 (2016)

Peculiarities of the working process of low-thrust hypergolic-propellant liquid rocket engines with a thrust of less than 1 N

Nigodjuk V.E., Sulinov A.V.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

Experience in the development of 11Д58MФ liquid rocket engines

Smolentsev A.A.

(Rus)

Vol 11, No 4 (2012)

Mathematical model of investigating normal acoustic modes of launch vehicle modules

Popov P.A., Belov A.S., Kryuchkov A.N.

(Rus)

Vol 10, No 2 (2011)

Promising technologies for solving boundary problems regarding the delivery of separating parts of carrier rockets with terminal targeting

Benevolsky S.V., Goncharenko V.I.

(Rus)

Experimental development of the LRE with CCCM nozzle’s extension

(Rus)