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Concentration of carbon dioxide in products of combustion of GTE NK-16ST and NK-16-18ST
Baklanov A.V.
Formation of the structure, mechanical and tribological properties of high chrome steel by electronic-ion-plasma nitrogen
Eresko S.P., Ivanov Y.F., Petrikova E.A., Teresov A.D., Klopotov A.A.
Development of the concept of a reusable liquid rocket engine with three-component fuel
Belyakov V.A., Vasilevsky D.O., Ermashkevich A.A., Kolomentsev A.I., Farizanov I.R.
Modeling and verification of working process parameters in gas generators for pressurizing fuel tanks of liquid propellant rocket propulsion systems
Sheludko M.L., Nazarov V.P., Zenyuk K.O., Nazarova L.P.
The possibility of using methane-hydrogen fuel in converted gas turbine engines for power plants
Baklanov A.V.
Local heat transfer parameters in the areas of the developing temperature boundary layer in the cavities of gas turbines local heat transfer parameters in the areas of the developing temperature boundary layer in the cavities of gas turbines
Zuev A.A., Arngol'd A.A., Falkova E.V., Tolstopyatov M.I., Dubynin P.A.
Structure of the surface layer of high-chrome steel nitridated in the elion regime in the plasma of a suspended arc discharge with a heated cathode
Eresko S.P., Ivanov Y.F., Lopatin I.V., Klopotov A.A., Nikonenko A.V.
TECHNOLOGICAL EQUIPMENT ANALYSIS OF AUTOMATED MONITORING SYSTEMS OF FLUE GASES AT POWER PLANTS
Kovalev I.V., Kovalev D.I., Kolesnik V.V., Losev V.V., Karaseva M.V.
MINING OF GAS-GASHYDRATE STRATUM DESORBTION METHOD A T PRESER V A TION OF TWO-PHASE AND THREE-PHASE EQUILIBRIUMS
Ivanov B.D.
THE DEVELOPMENT OF THE COATINGS TECHNOLOGY APPLICATION RADIOREFLECTIVE COATINGS
Miheev A.E., Girn A.V., Harlamov V.A., Chernyatina A.A., Homenko I.I.
Acceleration of the gas stream in the channelof the electrojet engine
Kraev V.M., Slavin V.S., Kraev M.V.
STUDY OF COMPOSITION OF RESIDUAL AND PLASMA-FORMING GASES IN THE VACUUM COATERS
Miheev A.E., Harlamov V.A., Kryuchek S.D., Chernyatina A.A., Homenko I.I.
HIGH-TEMPERATURE GAS-STATIC PROCESSING OF CAST CASE DETAILS OF TURBOPUMP SYSTEMS
Oborin L.A., Kolmykov V.A., Nazarov V.P.
HEAT TRANSFER IN THE CAVITY OF A GAS TURBINE LIQUID ROCKET ENGINE
Zuev A.A., Tolstopyatov M.I.
Evaluationof burning arc stability on small currents
Meyster R.A., Lubnin M.A., Gotovko S.A., Meyster A.R., Grigor'ev A.N., Meister R.A., Lubnin M.A., Gotovko S.A., Meister A.R., Grigoryew A.N.
AUTOMATIC CONTROL SYSTEM OF O2 AND H2 CONCENTRATIONS IN TECHNOLOGICAL GAS CIRCUITS OF BTLSS SPACE APPLICATION
Morozov Y.A., Trifonov S.V., Murygin A.V., Tikhomirov A.A.
MATHEMATICAL AND NUMERICAL MODELLING OF CURRENTS OF VISCOUS THERMALLY CONDUCTIVE GAS
Shchepanovskaya G.I.
INFLUENCE OF FILLING PROCESSES FOR MIXING HEAD OF GAS GENERATORS ON DYNAMICS OF LIQUID ROCKET ENGINE WITHOUT STARTER DEVICE
Belayev E.N., Vorobyev A.G.
Potential of detection range of borders of oil reservoir using logging tool with broadband electromagnetic pulse
Muzalevskiy K.V., Mironov V.L., Mikhailov M.I.
The prospects for improving the performance of Electromechanical Executive body of the spacecraft
Kholodilov S.V.
Thickness measuring of modeled oil-saturated rock with nanosecond bohole electromagnetic loging tool
Muzalevskiy K.V., Mironov V.L.
1 - 21 of 21 Items

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