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Vol 24, No 4 (2023)

Characteristics research of a low thrust rocket engine manufactured using additive SLM technology

Akbulatov E.S., Nazarov V.P., Gerasimov E.V.

(Rus)

(Eng)

Vol 20, No 2 (2019)

Solar thermal propulsion systems with various high-temperature power sources

Finogenov S.L., Kolomentsev A.I.

(Eng)

Vol 20, No 2 (2019)

Modeling of the stress-strain state of rocket-space technology structural elements manufactured by using additive technologies

Ushakova E.S.

(Eng)

Vol 21, No 1 (2020)

To the question of forecasting the technical condition of low-thrust liquid rocket engines

Komlev G.V., Mitrofanova A.S.

(Eng)

Vol 23, No 3 (2022)

Method for processing the results of cavitation tests of TNA pumps in order to obtain an approximating function

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

(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.

(Rus)

Vol 21, No 2 (2020)

Modeling of the stress-strain state of rocket-space technology structural elements manufactured by using additive technologies

Ushakova E.S.

(Eng)

Vol 17, No 3 (2016)

IMPROVING THE EFFICIENCY OF MULTIFUNCTIONAL ELECTRIC ROCKET ENGINES

Trifanov I.V., Kaz’min B.N., Oborina L.I., Trifanov V.I., Savel’eva M.V.

Vol 14, No 4 (2013)

THE DESIGN OF THE EXPERIMENT AND CREATION OF THE REGRESSION MODEL OF THE SPECIFIC IMPULSE LIQUID ROCKET ENGINE THRUST FROM 10 TO 420 N

Kolomentsev A.I., Khokhlov A.N.

(Rus)

Vol 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.G., Vorobyeva S.S.

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 16, No 3 (2015)

USE OF DIFFERENT OXIDIZERS FOR AFTERBURNING OF HYDROGEN HEATED BY SOLAR ENERGY IN ROCKET ENGINE

Finogenov S.L., Kolomentsev A.I., Kudrin O.I.

Vol 18, No 3 (2017)

IMPLEMENTATION OF AUTOMATED SYSTEM FOR MANUFACTURING OF PIPELINES OF ROCKET ENGINES

Yartsev E.N., Nazarov V.P., Teryaev N.S.

(Rus)

Vol 12, No 3 (2011)

APPLICATION OF COMBINED POROUS-MESH MATERIALS IN CONSTRUCTIONOF INTRATANK DEVICES OF PROPULISION INSTALLATIONS OF SPACECRAFTS,FINAL STEPS OF CARRIER ROCKETS AND UPPER-STAGES

Sapozhnikov V.B., Grishko Y.P., Korol'kov A.V., Bol'shakov V.A., Novikov Y.M., Konstantinov S.B., Martynov M.B., Sapozhnikov V.B., Grischko Y.P., Korolkov А.V., Bolshakov V.A., Novikov Y.M., Konstantinov S.B., Martynov M.B.

(Rus)

Vol 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.I., Nazarov V.P., Tsarapkin R.A.

(Rus)

Vol 13, No 3 (2012)

HYDRODYNAMIC INSTABILITY AT CAVITATIONAL OPERATING MODES OF HIGH-SPEED PUMPS

Krayev M.V.

(Rus)

Vol 18, No 2 (2017)

INFLUENCE OF LAUNCH PARAMETERS OF LIQUID ROCKET ENGINE ON THE BALANCE OF AXIAL FORCES IN THE TURBOPUMP

Belayev E.N., Vorobyev A.G.

(Rus)

Vol 12, No 5 (2011)

TECHNICAL CHARACTERISTICS OF OXYGEN-HYDROGEN LIQUID ROCKET PROPULSION SYSTEM OF INTERORBITAL SPACE VEHICLE

Borovik I.N.

(Rus)

Vol 17, No 3 (2016)

SOLAR THERMAL PROPULSION WITH DIFFERENT TYPES OF CONCENTRATOR-ABSORBER SYSTEM

Finogenov S.L., Kolomentsev A.I., Nazarov V.P.

Vol 17, No 1 (2016)

THE CHOICE OF HEAT-ACCUMULATING MATERIALS FOR SOLAR THERMAL PROPULSION

Finogenov S.L., Kolomentsev A.I.

Vol 15, No 3 (2014)

Some units spacecraft balancing

Krushenko G.G., Golovanova V.V.

(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 - 22 of 22 Items

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