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Design of the cooling system of a reasuble liquid rocket engine with three-component fuel
Belyakov V., Vasilevsky D., Ermashkevich A., Kolomentsev A., Farizanov I.
Development of the concept of a reusable liquid rocket engine with three-component fuel
Belyakov V., Vasilevsky D., Ermashkevich A., Kolomentsev A., Farizanov I.
Verification of thermodynamic parameters of a mixture of generator gas on oxygen-hydrogen fuel with an excess of one of the fuel components
Belyakov V., Vasilevsky D., Maslov D., Kilyashov A., Romashko R.
Increasing the specific impulse of an oxygen-hydrogen liquid rocket engine by increasing heat transfer in the combustion chamber
Vasilevsky D.
Features and modernization methods of thrust measurement devices for liquid rocket engine test stands
Begishev A., Zhuravlev V., Torgashin A.
CFD methods for cavitation modeling in centrifugal and axial pumps of LRE
Torgashin A., Zhujkov D., Nazarov V., Begishev A., Vlasenko A.
To the method of calculation of the main characteristics of promising booster electric pump units of liquid processor engines
Dubynin P., Tolstopyatov M., Zuev A., Chernenko V.
Comparative analysis of verified numerical simulation of cavitation based on the Rayleigh – Plesset model for liquid propellant rocket engine pumps
Torgashin A., Zhujkov D., Nazarov V., Begishev A., Vlasenko A.
The choice of the energy parameters of an oxygen-hydrogen propellant expander cycle rocket engine
Belyakov V.
Analysis of the stress-deformed state of the prismatic support of the lever-grading device of test stands for liquid rocket engines
Begishev A., Zhuravlev V., Nazarov V., Torgashin A.
DEVELOPING LRE OF LOW THRUST USING PROPELLANTS : STRONG HYDROGEN PEROXIDE WITH KEROSENE
Vorobiev A., Borovik I., Ha S.
INFLUENCE OF FILLING PROCESSES FOR MIXING HEAD OF GAS GENERATORS ON DYNAMICS OF LIQUID ROCKET ENGINE WITHOUT STARTER DEVICE
Belayev E., Vorobyev A.
ACCELERATED UNWINDING OF THE ROTOR BOOSTER PUMP OF LIQUID ROCKET ENGINES UNDER START-UP CONDITIONS
Belayev E., Vorobyev A.
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