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卷 25, 编号 1 (2024)
Study of the payload extraction trajectory heavy class carrier rocket
Bordachev V., Kolga V.
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(Rus) PDF
(Eng)
卷 24, 编号 4 (2023)
Concentration of carbon dioxide in products of combustion of GTE NK-16ST and NK-16-18ST
Baklanov A.
PDF
(Rus) PDF
(Eng)
卷 21, 编号 2 (2020)
Mathematical model of a linear electrodynamic engine operation on impact with account for elastic deformation of the hardened surface
Shvaleva N., Fadeev A., Eresko T.
PDF
(Eng)
卷 24, 编号 4 (2023)
Characteristics research of a low thrust rocket engine manufactured using additive SLM technology
Akbulatov E., Nazarov V., Gerasimov E.
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(Rus) PDF
(Eng)
卷 22, 编号 3 (2021)
Application of the propulsion subsystem on the base of SPT-100b plasmic thruster to the Express-80 and Express-103 spacecraft’s orbit raising and orbit control
Ermoshkin Y., Vnukov A., Volkov D., Kochev Y., Simanov R., Yakimov E., Grikhin G.
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(Rus) PDF
(Eng)
卷 20, 编号 2 (2019)
Mathematical model of a linear electrodynamic engine operation on impact with account for elastic deformation of the hardened surface
Shvaleva N., Fadeev A., Eresko T.
PDF
(Eng)
卷 20, 编号 2 (2019)
Solar thermal propulsion systems with various high-temperature power sources
Finogenov S., Kolomentsev A.
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(Eng)
卷 20, 编号 2 (2019)
Modeling of the stress-strain state of rocket-space technology structural elements manufactured by using additive technologies
Ushakova E.
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(Eng)
卷 21, 编号 1 (2020)
To the question of forecasting the technical condition of low-thrust liquid rocket engines
Komlev G., Mitrofanova A.
PDF
(Eng)
卷 22, 编号 3 (2021)
Improvement of the control system of the installation of electrical processing of metals based on a linear electrodynamic motor
Shestakov I., Shestakov V., Fadeev A., Shvaleva N.
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(Rus)
卷 22, 编号 1 (2021)
Experimental investigations of a plasma thrusters and its power processing units performances like an electric load of a spacecraft’s power condition system
Ermoshkin Y., Kochev Y., Nikipelov A., Pervukhin A., Simanov R.
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(Rus) PDF
(Eng)
卷 21, 编号 2 (2020)
Modeling of the stress-strain state of rocket-space technology structural elements manufactured by using additive technologies
Ushakova E.
PDF
(Eng)
卷 23, 编号 3 (2022)
Method for processing the results of cavitation tests of TNA pumps in order to obtain an approximating function
Torgashin A., Zhujkov D., Nazarov V., Begishev A.
PDF
(Rus)
卷 22, 编号 1 (2021)
The possibility of using methane-hydrogen fuel in converted gas turbine engines for power plants
Baklanov A.
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(Rus) PDF
(Eng)
卷 23, 编号 4 (2022)
The feature of the “Express-AMU3”, “Express-AMU7” spacecrafts injecton to geostationary orbit
Ermoshkin Y., Vnukov A., Volkov D., Kochev Y., Simanov R., Yakimov E., Pridannikov S.
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(Rus)
卷 24, 编号 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)
卷 12, 编号 3 (2011)
INCREASE OF EFFICIENCY OF GAS DISTRIBUTION IN THE ACCELERATINGCHANNEL OF AN ELECTROJET ENGINE
Gopanchuk V., Zhasan V., Potapenko M., Gopanchuk V., Zhasan V., Potapenko M.
PDF
(Rus)
卷 15, 编号 4 (2014)
Backgrounds and trends of all-electric propulsion geostationary satellites creation
Vnukov A., Rvacheva E.
PDF
(Rus)
卷 17, 编号 3 (2016)
GEOSTATIONARY ORBITAL INJECTION OF A SPACECRAFT BY THE COMBINED METHOD
Yakovlev A., Vnukov A., Balandina T., Balandin E., Tarletskiy I.
卷 19, 编号 3 (2018)
ON THE CONCEPT OF ALL ELECTRIC PROPULSION SPACECRAFT
Yermoshkin Y., Volkov D., Yakimov E.
PDF
(Rus)
卷 17, 编号 3 (2016)
IMPROVING THE EFFICIENCY OF MULTIFUNCTIONAL ELECTRIC ROCKET ENGINES
Trifanov I., Kaz’min B., Oborina L., Trifanov V., Savel’eva M.
卷 10, 编号 1-1 (2009)
Acceleration of the gas stream in the channelof the electrojet engine
Kraev V., Slavin V., Kraev M.
PDF
(Rus)
卷 11, 编号 4 (2010)
GEOSTATIONARY SPACECRAFT ORBIT SLAVING AND MANEUVER: THRUSTERS ON DRIVES INSTALLATION SCHEME
Ermoshkin Y., Raevskiy V., Urusov V., Yermoshkin Y., Raevsky V., Urusov V.
PDF
(Rus)
卷 14, 编号 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., Khokhlov A.
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(Rus)
卷 18, 编号 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)
卷 16, 编号 3 (2015)
USE OF DIFFERENT OXIDIZERS FOR AFTERBURNING OF HYDROGEN HEATED BY SOLAR ENERGY IN ROCKET ENGINE
Finogenov S., Kolomentsev A., Kudrin O.
卷 10, 编号 1-1 (2009)
Equations of three dimension electromagnetic field modelof multiphase linear induction motor with transverse flux
Ivanchura V., Suhanov V., Nikulin N.
PDF
(Rus)
卷 17, 编号 1 (2016)
COMPONENTS OF HIGH-PRECISION ELECTROMECHANICAL ACTUATOR FOR SYSTEM OF ADAPTATION TRANSFORMABLE SPACE TELESCOPE FOR ULTRA-LOW TEMPERATURES (4.2 K)
Jusov A., Kozlov S., Arkhipov M., Kostrov E.
卷 14, 编号 3 (2013)
MICROELECTRONIC SYSTEMS FOR AUTOMATION OF PERSPECTIVE SPACE VEHICLES
Nepomnuashy O., Ohotkin K., Habarov V.
PDF
(Rus)
卷 13, 编号 1 (2012)
FEATURES OF EXPERIMENTAL DEFINITION OF COMPOSITE MATERIALS DURABILITY AGAINST EROSIVE IMPACT OF STATIONARY PLASMA THRUSTERS
Nadiradze A., Rachmatullin R., Kochura S., Maksimov I., Smirnov V.
PDF
(Rus)
卷 17, 编号 1 (2016)
THE CHOICE OF HEAT-ACCUMULATING MATERIALS FOR SOLAR THERMAL PROPULSION
Finogenov S., Kolomentsev A.
卷 17, 编号 3 (2016)
SOLAR THERMAL PROPULSION WITH DIFFERENT TYPES OF CONCENTRATOR-ABSORBER SYSTEM
Finogenov S., Kolomentsev A., Nazarov V.
卷 13, 编号 3 (2012)
HYDRODYNAMIC INSTABILITY AT CAVITATIONAL OPERATING MODES OF HIGH-SPEED PUMPS
Krayev M.
PDF
(Rus)
卷 16, 编号 2 (2015)
ELECTROSTATIC DISCHARGE PROBLEM IN GEOSTATIONARY SPACECRAFT ELECTROJET PROPULSION SUBSYSTEM
Ermoshkin Y., Kochev Y., Trofimchuk D., Yakimov E.
PDF
(Rus)
卷 19, 编号 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)
卷 12, 编号 2 (2011)
Electric propulsions rational application range on the applied spacecrafts
Ermoshkin Y., Yermoshkin Y.
PDF
(Rus)
卷 16, 编号 2 (2015)
LOW-POWER RADIO-FREQUENCY ION THRUSTER
Akhmetzhanov R., Bogatyi A., Dronov P., Dyakonov G., Ivanov A.
PDF
(Rus)
卷 20, 编号 1 (2019)
ESTIMATION OF THE EFFICIENCY OF SPACECRAFT TRANSPORTATION WITH MINIMAL RADIATION DEGRADATION OF SOLAR CELLS
Birukov V., Nazarov V., Kurguzov A.
PDF
(Rus)
卷 17, 编号 3 (2016)
ACCELERATED UNWINDING OF THE ROTOR BOOSTER PUMP OF LIQUID ROCKET ENGINES UNDER START-UP CONDITIONS
Belayev E., Vorobyev A.
卷 12, 编号 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., Grishko Y., Korol'kov A., Bol'shakov V., Novikov Y., Konstantinov S., Martynov M., Sapozhnikov V., Grischko Y., Korolkov А., Bolshakov V., Novikov Y., Konstantinov S., Martynov M.
PDF
(Rus)
卷 12, 编号 5 (2011)
TECHNICAL CHARACTERISTICS OF OXYGEN-HYDROGEN LIQUID ROCKET PROPULSION SYSTEM OF INTERORBITAL SPACE VEHICLE
Borovik I.
PDF
(Rus)
卷 15, 编号 3 (2014)
Some units spacecraft balancing
Krushenko G., Golovanova V.
PDF
(Rus)
卷 19, 编号 1 (2018)
THE INFLUENCE OF THE COMBINED PROPULSION SYSTEM PARAMETERS ON THE INTEGRAL DOSE OF RADIATION WHEN PUTTING A SPACECRAFT INTO A GEOSTATIONARY ORBIT
Birukov V., Nazarov V., Kurguzov A.
PDF
(Rus)
卷 17, 编号 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.
卷 12, 编号 1 (2011)
CRITERIAOF ORBITALCONTROLTHRUSTER OPTIMALALLOCATIONON BOARD OFGEOSTATIONARY SPACECRAFT
Ermoshkin Y., Urusov V., Yermoshkin Y., Urusov V.
PDF
(Rus)
卷 15, 编号 2 (2014)
Small-sized multi-motor-reducer
Nadaraia C., Shestakov I., Fadeev A.
PDF
(Rus)
卷 18, 编号 3 (2017)
IMPLEMENTATION OF AUTOMATED SYSTEM FOR MANUFACTURING OF PIPELINES OF ROCKET ENGINES
Yartsev E., Nazarov V., Teryaev N.
PDF
(Rus)
卷 16, 编号 1 (2015)
Electric power supply of heater elements of electric propulsion thruster by regulated alternating current
Moshnyakov A., Mikhaylov M.
PDF
(Rus)
卷 11, 编号 1 (2010)
Indicatrix account of materials dispersion at the estimations of erosion-contaminating influence of streams of plasma thrusters on space craft
Nadiradze A., Shaposhnikov V., Smirnov V., Maximov I., Kochura S.
PDF
(Rus)
卷 10, 编号 2 (2009)
INVESTIGATION DRIVE SYSTEM WITH THE MULTIPHASE TRANSVERSE FLUXLINEAR INDUCTION MOTOR
Ivanchura V., Suchanov V., Nikulin N.
PDF
(Rus)
卷 18, 编号 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)
卷 16, 编号 1 (2015)
AN ELECTROMECHANICAL EXECUTIVE BODY BASED ON THE CONTACTLESS DIRECT CURRENT MOTOR WITH A WINDING PRINTING DISK STATOR FOR SMALL SPACECRAFTS
Balandina T., Balandin E.
PDF
(Rus)
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