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On selection of automatic control system for crvogenic fuel gas turbine engine

Bukin V.A.

(Rus)

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

Cycle parameters of an internal combustion spark-ignition gas piston engine with an electronic control system

Shishkov V.A.

(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)

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

Modeling direct fuel injection by a multipin nozzle into the ice combustion chamber using CAE/CAD-systems

Biryuk V.V., Kayukov S.S., Gorshkalev A.A., Uglanov D.A., Lysenko Y.D., Zvyagintsev V.A.

(Rus)

Features of start-up the engine of internal combustion with spark ignition on gas fuel

Shishkov V.A.

(Rus)

Vol 18, No 2 (2019)

Technology of computational analysis of the working process parameters of low-thrust rocket engines running on gaseous oxygen-hydrogen fuel with the use of ANSYS CFD

Ryzhkov V.V., Morozov I.I.

(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 9, No 1 (2010)

Quality indices of an internal combustion engine controlled by the discharge current channel

1 1., 1 1., 1 1.

(Rus)

Investigation of the kinetic properties of gas products of liquid-phase interaction hypergolic liquid rocket fuel

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 11, No 2 (2012)

Determining the angle of advance of ignition when switching from petrol to gas depending on fuel mixture burning rate

Shishkov V.A.

(Rus)

Vol 9, No 1 (2010)

Optoelectronic device for the control of hydrocarbon fuel cavitation treatment

1 1.

(Rus)

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

Egorychev V.S.

(Rus)

Vol 15, No 4 (2016)

Analysis of low-thrust liquid rocket engines with a methane air pump unit

Ivanov A.I., Kositsin I.P., Borisov V.A.

(Rus)

Vol 11, No 2 (2012)

Model of sedimentation of solid particles of heterogeneous materials

Polyanskov Y.V., Evseev A.N., Poroykov V.A.

(Rus)

Vol 9, No 1 (2010)

Defining the specific impulse of mixed solid propellants

1 1., 1 1.

(Rus)

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

Egorychev V.S.

(Rus)

Vol 14, No 1 (2015)

Experimental study of free-convection flame propagation

Yevdokimov O.A., Guryanov A.I.

(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)

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

1 1.

(Rus)

Vol 19, No 3 (2020)

Improving the efficiency of the powerplant of an unmanned aerial vehicle through the use of cryogenic fuel

Kolesnikov A.S., Grasko T.V., Raznoschikov V.V.

(Rus)

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

Prospects and problems of movement and power plants in powder metal fuel

Egorov A.G., Tizilov A.S.

(Rus)

Vol 13, No 5-3 (2014): Special Issue

Estimation of mass-dimensional characteristics of a complex propulsion unit of earth remote sensing spacecraft

Kurenkov V.I., Kucherov A.S., Yakishik A.A.

(Rus)

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

Didenko A.A., Sokolov A.B.

(Rus)

Мethod of design calculation of centrifugal emulsive duplex fuel nozzle

1 1.

(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)

Possibility of use of passing gases in gasturbine engines created within the limits of conversion

Rosljakov A.D., Kocherov E.P., Tsibizov J.I.

(Rus)

Vol 13, No 5-3 (2014): Special Issue

Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel

Ageenko Y.I., Lapshin E.A., Morozov I.I., Pegin I.V., Ryzhkov V.V.

(Rus)

Vol 10, No 1 (2011)

Algorithm of adaptation of an electronic control system of internal combustion engines to various chemical compositions of gas fuel

Shishkov V.A.

(Rus)

Mixing parameters investigations and methods of approach to calculations and development of the thrusters with a spray-centrifugal scheme of NT and NDMH mixing on the confusion chamber wall in considered

1 1.

(Rus)

Vol 10, No 6 (2011)

Peculiarities of starting a spark-ignition gas fuel internal combustion engine

Shishkov V.A.

(Rus)

Experimental and numerical investigation of the combustion process in vortex gas burner

Yevdokimov O.A.

(Rus)

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

Investigation of transformation of intermediate products of liquid-phase interaction propellant at the onset of combustion for rocket engine

Nigodjuk V.E., Sulinov A.V.

(Rus)

Vol 10, No 1 (2011)

Using the energy of gas differential pressure in electromagnetic injectors for improved breathing of spark-ignition internal combustion engine cylinders

Shishkov V.A.

(Rus)