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Concentration of carbon dioxide in products of combustion of GTE NK-16ST and NK-16-18ST
Baklanov A.
Modeling of the stress-strain state of rocket-space technology structural elements manufactured by using additive technologies
Ushakova E.
The influence of the method of fuel supply into the combustion chamber on the quality of mixing and on the carbon oxide formation
Baklanov A.
Modeling of the stress-strain state of rocket-space technology structural elements manufactured by using additive technologies
Ushakova E.
The possibility of using methane-hydrogen fuel in converted gas turbine engines for power plants
Baklanov A.
The choice of the energy parameters of an oxygen-hydrogen propellant expander cycle rocket engine
Belyakov V.
INCREASE OF EFFICIENCY OF GAS DISTRIBUTION IN THE ACCELERATINGCHANNEL OF AN ELECTROJET ENGINE
Gopanchuk V., Zhasan V., Potapenko M., Gopanchuk V., Zhasan V., Potapenko M.
SPACECRAFT THERMAL VACUUM OPTIMIZATION: DEVELOPMENT OF NEW TENDENCIES
Krat S., Khristich V., Krat S., Hristkh V.
INFLUENCE OF FILLING PROCESSES FOR MIXING HEAD OF GAS GENERATORS ON DYNAMICS OF LIQUID ROCKET ENGINE WITHOUT STARTER DEVICE
Belayev E., Vorobyev A.
CAMERA-TO-TOUCHSCREEN DESIGN
Likhonina R., Kohout L., Kadlec J.
The Method of CALCULATION OF THERMAL STATE OF CHAMBER FOR steady state IMPULSE operation OF LIQUID ROCKET ENGINE OF SMALL THRUST
Vorobyev A., Vorobyeva S.
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