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Title
Authors
Vol 19, No 3 (2018)
ON THE CONCEPT OF ALL ELECTRIC PROPULSION SPACECRAFT
Yermoshkin Y.M., Volkov D.V., Yakimov E.N.
PDF
(Rus)
Vol 19, No 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.I., Nazarov V.P., Kurguzov A.V.
PDF
(Rus)
Vol 17, No 3 (2016)
GEOSTATIONARY ORBITAL INJECTION OF A SPACECRAFT BY THE COMBINED METHOD
Yakovlev A.V., Vnukov A.A., Balandina T.N., Balandin E.A., Tarletskiy I.S.
Vol 17, No 4 (2016)
STRUCTURE OPTIMIZATION AND PARAMETERS OF LARGE ENERGY PROPULSION SYSTEMS
Novikov Y.A., Ermolaev V.I.
Vol 25, No 1 (2024)
Issues of ensuring the resistance of high-voltage solar arrays of spacecraft to the effects of secondary arc discharges
Valiullin V.V., Kochura S.G., Maximov I.A., Nadiradze A.B.
PDF
(Rus) PDF
(Eng)
Vol 12, No 1 (2011)
CRITERIAOF ORBITALCONTROLTHRUSTER OPTIMALALLOCATIONON BOARD OFGEOSTATIONARY SPACECRAFT
Ermoshkin Y.M., Urusov V.M., Yermoshkin Y.M., Urusov V.M.
PDF
(Rus)
Vol 20, No 1 (2019)
ESTIMATION OF THE EFFICIENCY OF SPACECRAFT TRANSPORTATION WITH MINIMAL RADIATION DEGRADATION OF SOLAR CELLS
Birukov V.I., Nazarov V.P., Kurguzov A.V.
PDF
(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 20, No 3 (2019)
Development of the propulsion construction and the trajectory of the spacecrafts for the study of Martian planetary system
Platov I.V., Simonov A.V., Vorobyev A.L., Gordienko E.S.
PDF
(Eng)
Vol 11, No 4 (2010)
GEOSTATIONARY SPACECRAFT ORBIT SLAVING AND MANEUVER: THRUSTERS ON DRIVES INSTALLATION SCHEME
Ermoshkin Y.M., Raevskiy V.A., Urusov V.M., Yermoshkin Y.M., Raevsky V.A., Urusov V.M.
PDF
(Rus)
Vol 20, No 2 (2019)
Solar thermal propulsion systems with various high-temperature power sources
Finogenov S.L., Kolomentsev A.I.
PDF
(Eng)
Vol 17, No 1 (2016)
THE CHOICE OF HEAT-ACCUMULATING MATERIALS FOR SOLAR THERMAL PROPULSION
Finogenov S.L., Kolomentsev A.I.
Vol 22, No 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.M., Kochev Y.V., Nikipelov A.V., Pervukhin A.V., Simanov R.
PDF
(Rus) PDF
(Eng)
Vol 16, No 2 (2015)
ELECTROSTATIC DISCHARGE PROBLEM IN GEOSTATIONARY SPACECRAFT ELECTROJET PROPULSION SUBSYSTEM
Ermoshkin Y.M., Kochev Y.V., Trofimchuk D.A., Yakimov E.N.
PDF
(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 10, No 5 (2009)
Geo satellite attitude and orbit control: fixed orbit control thrasters
Ermoshkin Y.M., Raevsky V.A., Urusov V.M.
PDF
(Rus)
Vol 15, No 4 (2014)
Backgrounds and trends of all-electric propulsion geostationary satellites creation
Vnukov A.A., Rvacheva E.I.
PDF
(Rus)
Vol 17, No 3 (2016)
DEVELOPMENT OF THE PROPULSION CONSTRUCTION AND THE TRAJECTORY FOR THE SPACECRAFTS OF THE “LAPLACE-L” MISSION FOR THE STUDY OF THE JUPITER PLANETARY SYSTEM
Platov I.V., Simonov A.V.
Vol 10, No 4 (2009)
GEOSTATIONARY SPACECRAFT ATTITUDE AND ORBIT CONTROL BY MOTIONLESS ORBIT CONTROL THRUSTERS
Yermoshkin Y.M., Raevsky V.A., Urusov V.M.
PDF
(Rus)
Vol 14, No 3 (2013)
ELASTIC FEED SYSTEMS OF FUEL TANKS
Platov I.V.
PDF
(Rus)
Vol 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.Y., Nazarov V.P., Konstantinov R.I., Morozov V.I., Gainutdinov A.V.
Vol 13, No 3 (2012)
HYDRODYNAMIC INSTABILITY AT CAVITATIONAL OPERATING MODES OF HIGH-SPEED PUMPS
Krayev M.V.
PDF
(Rus)
Vol 19, No 3 (2018)
DESIGN OF A LOW THRAST PROPULSION SYSTEM AND THE TRAJECTORIES OF SPASECRAFT TO THE CENTRE OF THE SOLAR SYSTEM
Platov I.V., Simonov A.V.
PDF
(Rus)
Vol 12, No 2 (2011)
Electric propulsions rational application range on the applied spacecrafts
Ermoshkin Y.M., Yermoshkin Y.M.
PDF
(Rus)
Vol 16, No 1 (2015)
FEATURES OF DEVELOPMENT OF THE COMBINED IMPELLENT INSTALLATION AND THE CIRCUIT OF FLIGHT OF THE SPACECRAFT «INTERGELIO-PROBE»
Platov I.V., Simonov A.V., Konstantinov M.S.
PDF
(Rus)
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