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Volume 17, Nº 3 (2016)
IMPROVING THE EFFICIENCY OF MULTIFUNCTIONAL ELECTRIC ROCKET ENGINES
Trifanov I., Kaz’min B., Oborina L., Trifanov V., Savel’eva M.
Volume 26, Nº 1 (2025)
Design and testing of injectors manufactured using additive technologies for a low-thrust liquid rocket engine
Zhuravlev V., Manokhina E., Tolstopiatov M.
PDF
(Rus) PDF
(Eng)
Volume 23, Nº 3 (2022)
The choice of the energy parameters of an oxygen-hydrogen propellant expander cycle rocket engine
Belyakov V.
PDF
(Rus)
Volume 18, Nº 2 (2017)
INFLUENCE OF LAUNCH PARAMETERS OF LIQUID ROCKET ENGINE ON THE BALANCE OF AXIAL FORCES IN THE TURBOPUMP
Belayev E., Vorobyev A.
PDF
(Rus)
Volume 17, Nº 4 (2016)
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.
Volume 20, Nº 2 (2019)
Modeling of the stress-strain state of rocket-space technology structural elements manufactured by using additive technologies
Ushakova E.
PDF
(Eng)
Volume 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., Vorobyev A.
PDF
(Rus)
Volume 17, Nº 3 (2016)
ACCELERATED UNWINDING OF THE ROTOR BOOSTER PUMP OF LIQUID ROCKET ENGINES UNDER START-UP CONDITIONS
Belayev E., Vorobyev A.
Volume 21, Nº 1 (2020)
To the question of forecasting the technical condition of low-thrust liquid rocket engines
Komlev G., Mitrofanova A.
PDF
(Eng)
Volume 25, Nº 3 (2024)
Implementation of additive 3D printing technology in the development of an experimental oxygen-hydrogen low thrust rocket engine
Koshlakov V., Mosolov S., Klimenko A., Akbulatov E., Nazarov V., Gerasimov E.
PDF
(Rus) PDF
(Eng)
Volume 13, Nº 3 (2012)
HYDRODYNAMIC INSTABILITY AT CAVITATIONAL OPERATING MODES OF HIGH-SPEED PUMPS
Krayev M.
PDF
(Rus)
Volume 12, Nº 5 (2011)
TECHNICAL CHARACTERISTICS OF OXYGEN-HYDROGEN LIQUID ROCKET PROPULSION SYSTEM OF INTERORBITAL SPACE VEHICLE
Borovik I.
PDF
(Rus)
Volume 18, Nº 3 (2017)
IMPLEMENTATION OF AUTOMATED SYSTEM FOR MANUFACTURING OF PIPELINES OF ROCKET ENGINES
Yartsev E., Nazarov V., Teryaev N.
PDF
(Rus)
Volume 25, Nº 1 (2024)
Study of the payload extraction trajectory heavy class carrier rocket
Bordachev V., Kolga V.
PDF
(Rus) PDF
(Eng)
Volume 15, Nº 3 (2014)
Some units spacecraft balancing
Krushenko G., Golovanova V.
PDF
(Rus)
Volume 18, Nº 3 (2017)
THE ALGORITHM FOR ESTIMATING RESERVES OF THE WORKING PROCESS STABILITY IN COMBUSTION CHAMBERS AND GAS GENERATORS OF LIQUID ROCKET ENGINES
Biryukov V., Nazarov V., Tsarapkin R.
PDF
(Rus)
Volume 24, Nº 4 (2023)
Characteristics research of a low thrust rocket engine manufactured using additive SLM technology
Akbulatov E., Nazarov V., Gerasimov E.
PDF
(Rus) PDF
(Eng)
Volume 21, Nº 2 (2020)
Modeling of the stress-strain state of rocket-space technology structural elements manufactured by using additive technologies
Ushakova E.
PDF
(Eng)
Volume 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., Tolstopyatov M., Zuev A., Chernenko V.
PDF
(Rus)
Volume 17, Nº 2 (2016)
Modernization of fuel submission systems of liquid rocket engines OF UPPER STAGES on the basis of innovative technical decisions
Piunov V., Nazarov V., Konstantinov R., Morozov V., Gainutdinov A.
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