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Title

Authors

Vol 8, No 3-2 (2009): Special Issue

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 22, No 3 (2023)

Study of the efficiency of the application of gas dynamic stabilization of the flame in a current engine

Belonozhkin V.V., Teslya D.N.

(Rus)

Vol 12, No 3-1 (2013): Vestnik SSAU

Limit values of the Brayton cycle with the use of reduced fuel characteristics

Mikheenkov E.L., Nekrasova S.O.

(Rus)

Vol 23, No 3 (2024)

Development and research testing of a low thrust on gaseous-propellant rocket engine chamber

Musteikis A.I., Levikhin A.A., Kolosenok S.V.

(Rus)

Vol 12, No 3-1 (2013): Vestnik SSAU

Method of reduced fuel characteristics and parameters of the operating cycles of heat engines

Anastaseev V.V., Belozertsev S.V., Mikheenkov E.L., Nekrasova S.O.

(Rus)

Vol 10, No 5 (2011)

Design and investigation of a pneumatic atomizer as applied to a low emission combustion chamber of a promising gas-turbine engine

Vasilyev A.Y., Chelebyan O.G., Yagodkin V.I.

(Rus)

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

Increasing the overall performance of a two-stroke engine with spark ignition by fuel injection

Dovgyallo A.I., Krasheninnikov S.V., Shchepetov D.A.

(Rus)

Vol 18, No 4 (2019)

Solving the problem of minimax closed-loop control of liquid-propellant launch vehicle fuel consumption control

Shorikov A.F., Kalev V.I.

(Rus)

Vol 18, No 2 (2019)

Disturbed motion of a hypersonic vehicle in climb

Balakin V.L., Krikunov M.M.

(Rus)

Vol 15, No 4 (2016)

Mathematical modelling of the working process of a hot gas pressure feed system

Salich V.L.

(Rus)

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

State of the art analysis in the automotive hybrid drives

Sinyiakov A.F., Gimadiev A.G., Ilukhin V.N., Sverbilov V.Y.

(Rus)

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

Quasi one-dimensional model and calculation of processes in gas turbineengine combustion chambers given the heterogeneity of the combustible mixture, changes in mass, composition, temperature and stirring efficiency of the working body

Didenko A.A., Sokolov A.B.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Research of laws of interaction of components in a liquid phase self-igniting liquid rocket fuel

1 1., 1 1.

(Rus)

Vol 18, No 3 (2019)

Disturbed motion of the hypersonic first stage of an aerospace system in climb

Balakin V.L., Krikunov M.M.

(Rus)

Vol 18, No 1 (2019)

Optimization of space vehicle combined orbital plane change maneuver on the basis of pontryagin’s maximum principle

Khramov A.A.

(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 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

Results of primary operation of NK-37 engine low emission combustion system

Bantikov D.Y., Yeliseev Y.S., Lavrov V.N., Pchelyakov A.A., Fedorchenko D.G., Tsybizov Y.I.

(Rus)

Vol 12, No 3-1 (2013): Vestnik SSAU

System of pressurization of the fuel tank of a launch vehicle using the heat of generator gas

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

(Rus)

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

Working process of gaseous fuel metallizator

Pervyshin A.N., Ryazanov A.I.

(Rus)

Vol 18, No 1 (2019)

Analysis of control programs and climb paths of the hypersonic first stage of an aerospace system

Balakin V.L., Krikunov M.M.

(Rus)

Vol 15, No 1 (2016)

Mathematical model of fuel sloshing in the measuring channel of the fuel expenditure control system

Kryukov Y.A.

(Rus)

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

Fluctuations of pressure in rail gas injection of engines with spark ignition

Shishkov V.A.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

Progressive thermodynamic cycle of internal combustion engine based on сrank a rod the mechanism with dual kinematic communications

Grabovskiy A.A.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Increasing efficiency of pressurization of the rocket tanks in the flight

1 1., 1 1.

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

Test bench for investigation of thrusters intra-chamber working processes

Pervyshin A.N., Ryazanov A.I.

(Rus)

Vol 17, No 4 (2018)

Optimization of fuel distribution in the afterburner of a gas turbine engine

Nelyubin V.R.

(Rus)

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

Test verification of flow stabilizer calculated parameters provided flow stabilization of propellant in wide range of input parameters

Beshenev Y.A., Volkov A.V., Kazankin F.A.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

Guaranteeing of ecological and economic indicators of internal combustion engine

Grabovskiy A.A., Mironov V.A.

(Rus)

Vol 7, No 3 (2008): Special Issue

Increasing efficiency of pressurization of the rocket tanks in the flight

Biryuk V.V., Kapitonov V.A., Smorodin A.V.

(Rus)

Vol 20, No 4 (2021)

Specific features of pressure pulsation control in combustion chambers of land based gas turbine units

Skiba D.V., Maksimov D.A., Kashapov R.S., Kharisov T.S.

(Rus)

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

Joint work of units and characteristics of elements gas the equipment for the engine of internal combustion with spark ignition

Shishkov V.A., Lesnih U.I.

(Rus)

Vol 17, No 4 (2018)

Analysis of control programs and flight paths of a hypersonic vehicle in climb

Balakin V.L., Krikunov M.M.

(Rus)

Vol 14, No 2 (2015)

Experience of operational development of starting characteristics of the APU combustion chamber

Chechulin A.Y.

(Rus)

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

On plasma support of fuel burning in a combustion chamber of a gas-turbine facility

Bulaeva M.N., Kravchenko I.V., Riaby V.A., Tkachenko D.P.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

The combined fuel draining control system for liquid oxygen and liquid hydrogen upper stage

Ivanov V.P., Partola I.S.

(Rus)

Vol 12, No 1 (2013)

Optimal control of the angle of attack of a hypersonic flight vehicle

Bebyakov A.A.

(Rus)

Vol 20, No 2 (2021)

Calculation of flow characteristics of liquid fuel supplied through pressure jet atomizers of small-sized gas turbine engines

Gurakov N.I., Zubrilin I.A., Hernandez Morales M., Yakushkin D.V., Didenko A.A., Matveev S.G., Komisar Y.V.

(Rus)

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

Heat engine cycle limitations imposed by fuel properties

Mikheyenkov E.L.

(Rus)

Vol 17, No 3 (2018)

Development of a procedure for the synthesis of a micro gas turbine engine neural controller with account for fuel consumption constraints

Kuznetsov A.V., Makaryants G.M.

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

Robust research of the fuzzy logic controllers using a fuel flow control loop of the gas-turbine engine as an example

Chicherova E.V.

(Rus)

Vol 9, No 1 (2010)

Defining the specific impulse of mixed solid propellants

1 1., 1 1.

(Rus)

Vol 12, No 2 (2013)

Chemical gas sources

Novikov A.A., Ershikhin N.A.

(Rus)

Vol 19, No 2 (2020)

Optimal command control of flight paths of aerospace system hypersonic first stage in conditions of atmospheric disturbances

Krikunov M.M.

(Rus)

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

Turboprofan jet modeling and equivalent specific fuel consumption optimization subsystem construction on the seminatural modelling stand

Pogorelov G.I., Krivosheev I.A., Godovanyuk A.G., Danilin O.E., Badamshin B.I.

(Rus)

Vol 17, No 2 (2018)

Optimization of space vehicle combined orbital plane change maneuver on the basis of the successive linearization method

Balakin V.L., Ishkov S.A., Khramov A.A.

(Rus)

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

Investigation of 11D428А-22 thruster operation dynamics with bellows flow stabilizer

Beshenev Y.A., Volkov A.V., Kazankin F.A.

(Rus)

Vol 11, No 1 (2012)

Command control of hypersonic cruising aircraft during climb

Balakin V.L., Kotchyan A.G.

(Rus)

Vol 8, No 3-3 (2009): Special Issue

Development of advanced low thrust rocket engines with ecologically friendly propellants

1 1., 1 1., 1 1.

(Rus)

Vol 12, No 2 (2013)

Experimental research of wall boundary flow formation in the combustion chamber of a small gas generator with self-igniting fuel components

Shustov S.A.

(Rus)

Vol 19, No 1 (2020)

Optimal command control of hypersonic aircraft flight path in conditions of atmospheric disturbances

Krikunov M.M.

(Rus)

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

Improving the efficiency of diesel engines by means of electroprocessing of fuel

Kozmenkov I.N., Nosyrev D.Y.

(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 11, No 7 (2012)

Measurement of hydrocarbon fuels quality factor precision increase

Borminsky S.A.

(Rus)

Vol 8, No 3-3 (2009): Special Issue

The simplification of heat engines thermodynamics calculation with using of idaeal gas’ model

1 1., 1 1.

(Rus)

Vol 12, No 3-1 (2013): Vestnik SSAU

Applying the possibilities of Microsoft Excel for solving problems of fuel burning thermodynamics

Mikheenkov E.L., Nekrasova S.O., Ramzaeva E.A.

(Rus)

1 - 58 of 58 Items

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