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Vol 22, No 2 (2021)

Design of the cooling system of a reasuble liquid rocket engine with three-component fuel

Belyakov V.A., Vasilevsky D.O., Ermashkevich A.A., Kolomentsev A.I., Farizanov I.R.

(Rus)

(Eng)

Vol 22, No 1 (2021)

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.

(Rus)

(Eng)

Vol 25, No 1 (2024)

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.A., Vasilevsky D.O., Maslov D.V., Kilyashov A.A., Romashko R.V.

(Rus)

(Eng)

Vol 23, No 4 (2022)

Increasing the specific impulse of an oxygen-hydrogen liquid rocket engine by increasing heat transfer in the combustion chamber

Vasilevsky D.O.

(Rus)

Vol 21, No 1 (2020)

Features and modernization methods of thrust measurement devices for liquid rocket engine test stands

Begishev A.M., Zhuravlev V.Y., Torgashin A.S.

(Eng)

Vol 21, No 3 (2020)

CFD methods for cavitation modeling in centrifugal and axial pumps of LRE

Torgashin A.S., Zhujkov D.A., Nazarov V.P., Begishev A.M., Vlasenko A.V.

(Eng)

Vol 24, No 2 (2023)

To the method of calculation of the main characteristics of promising booster electric pump units of liquid processor engines

Dubynin P.A., Tolstopyatov M.I., Zuev A.A., Chernenko V.V.

(Rus)

Vol 22, No 4 (2021)

Comparative analysis of verified numerical simulation of cavitation based on the Rayleigh – Plesset model for liquid propellant rocket engine pumps

Torgashin A.S., Zhujkov D.A., Nazarov V.P., Begishev A.M., Vlasenko A.V.

(Rus)

(Eng)

Vol 23, No 3 (2022)

The choice of the energy parameters of an oxygen-hydrogen propellant expander cycle rocket engine

Belyakov V.A.

(Rus)

Vol 23, No 1 (2022)

Analysis of the stress-deformed state of the prismatic support of the lever-grading device of test stands for liquid rocket engines

Begishev A.M., Zhuravlev V.Y., Nazarov V.P., Torgashin A.S.

(Rus)

Vol 12, No 4 (2011)

DEVELOPING LRE OF LOW THRUST USING PROPELLANTS : STRONG HYDROGEN PEROXIDE WITH KEROSENE

Vorobiev A.G., Borovik I.N., Ha S.U.

(Rus)

Vol 19, No 3 (2018)

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.

(Rus)

Vol 17, No 3 (2016)

ACCELERATED UNWINDING OF THE ROTOR BOOSTER PUMP OF LIQUID ROCKET ENGINES UNDER START-UP CONDITIONS

Belayev E.N., Vorobyev A.G.

1 - 13 of 13 Items

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