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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.
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(Rus) PDF
(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.
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(Rus)
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.
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(Rus) PDF
(Eng)
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.
PDF
(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.
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(Eng)
Vol 23, No 3 (2022)
The choice of the energy parameters of an oxygen-hydrogen propellant expander cycle rocket engine
Belyakov V.A.
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(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.
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(Rus)
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.
PDF
(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.
PDF
(Rus) PDF
(Eng)
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.
PDF
(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.
PDF
(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 - 12 of 12 Items

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