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Authors
MINIATURE ANTENNAS FOR CUBERSAT
Generalov A.G., Gadzhiev E.V.
IMPROVEMENT OF INSULATION RESISTANCE MEASUREMENT ACCURACY DURING SPACECRAFT POWER SYSTEM TESTS
Shtabel N.V., Samotik L.A., Mizrah E.A.
TO GEOSTATIONARY COLLOCATION PROBLEM
Kuprin A.G., Medvedev A.V.
SOFTWARE SUPPORT FOR TESTING COMMAND RECEPTION AND TRANSMISSION AND TELEMETRY ANALYSIS IN THE COMMAND-AND-MEASURING SYSTEM
Nozhenkova L.F., Isaeva O.S., Vogorovskiy R.V., Gruzenko E.A.
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.
The influence of conditions for passing GLONASSand GPS satellite radio navigation signals on the errors of defining relative coordinates
Garin E.N.
The problems of telemetric data processingin the loop of spacecrafts computer-aided control system
Pakman D.N., Nekrasov M.V., Antamoshkin A.N.
Dual-use spacecraft conception
Kislitskiy M.I., Kislitsky M.I.
MODERN SPACECRAFTS OPERATIONAL RELIABILITY AND QUALITY ANALYSIS
Patraev V.E., Trifanov I.V., Patraev V.E., Trifanov I.V.
Rational photovoltaic batteries mounting on the earth remote sensing microsatellite
Gubin S.V., Shepetov Y.A., Dolzhukova K.O.
Mathematical methods used to assess the position and form accuracy of a large-sized spacecraft reflector
Goldobin N.N.
PROBLEMS OF DEVELOPMENT OF LOW-ORBIT MULTIFUNCTIONAL PERSONAL SATELLITE COMMUNICATION SYSTEM «GONETS-D1M»
Kuzovnikov A.V., Testoedov N.A., Agureev V.A.
ONBOARD COMPUTER COMPLEX FOR UNPRESSURISED LONG-RESOURCED SPACECRAFTS
Kozlov I.V.
THE REVIEW OF MODERN SOLAR CELLS FOR SPACE APPLICATION BASED ON AIIIBV MATERIALS
Slyshchenko E.V., Naumova A.A., Lebedev A.A., Genali M.A., Vagapova N.T., Zhalnin B.V.
ANALYSIS OF SPACECRAFT ORBITAL MOTION STABILITY OF GONETS-M NO 37152
Kolovsky I.K., Shmakov D.N., Podolyakin V.N.
THE EVOLUTION OF THE PROJECT “SEA LAUNCH” OF SPACECRAFT
Testoedov N.A., Dvirnyi V.V., Krushenko G.G., Dvirnyi G.V.
DETERMINATION OF THE FUNDAMENTAL FREQUENCY OF A SANDWICH PANEL AS CONSTRUCTIONAL PART OF SPACECRAFT BODY
Deev P.O., Sinkovskiy F.K.
APPLICATION OF THE METHOD OF LOAD TESTING WITH GROUND experimental METHOD of CONTROL UNITS OF antenna GUIDANCE system
Kudryashova G.V., Babanov D.A., Galimzyanov A.T.
The shock-absorber for executive powers of system of stabilisation of a spaceCRAFT
Vasiltsov A.A., Lipovtsev A.A.
ADAPTIVE MULTI BEAM ANTENNA JSC «ISS»
Pershin A.S., Uzolin E.Y., Pershin A.S., Uzolin E.Y.
Geo satellite attitude and orbit control: fixed orbit control thrasters
Ermoshkin Y.M., Raevsky V.A., Urusov V.M.
METHODS FOR HIGH-ACCURACY MEASUREMENTS OF PRECISION STRUCTURES FOR MOBILE AUTOMATIC SPACECRAFT IN THERMAL VACUUM CONDITIONS
Dvirniy G.V.
Electric propulsions rational application range on the applied spacecrafts
Ermoshkin Y.M., Yermoshkin Y.M.
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.
Mobile system weightlessness simulation for a large spacecraft
Kovalev I.V., Kikot J.O.
Unification methods of present telemetry processing systems in satellite control centers
Nekrasov M.V., Packman D.N., Antamoshkin A.N.
MICROELECTRONIC SYSTEMS FOR AUTOMATION OF PERSPECTIVE SPACE VEHICLES
Nepomnuashy O.V., Ohotkin K.G., Habarov V.A.
DEVELOPMENT OF COMPOSITE PRECISION SATELLITE REFLECTOR: FINITE ELEMENT CONSTRUCTION MODELING
Lopatin A.V., Pasechnik K.A., Vlasov A.Y., Shatov A.V.
ON THE CONCEPT OF ALL ELECTRIC PROPULSION SPACECRAFT
Yermoshkin Y.M., Volkov D.V., Yakimov E.N.
THE METHOD OF AUTOMATED DEVELOPMENT OF AN ASSEMBLY DRAWING OF A CABLE NETWORK
Butin A.M., Dubrovskiy E.U., Dobyshev E.V., Efremov S.V., Suntsov S.B.
SIMULATION MEANS OF ELECTROSTATIC DISCHARGES IN THE SYSTEM “STATIONARY PLASMA THRUSTER - TRANSFORMATION AND CONTROL SYSTEM”
Trofimchuk D.A., Bezhayev Y.A., Ivanov V.V., Kochura S.G., Maximov I.A.
ASSESSMENT OF SPACECRAFT SOLAR ARRAY RELIABILITY DURING GROUND EXPERIMENTAL DEVELOPMENT TEST
Zakharov S.A.
AN ELECTROMECHANICAL EXECUTIVE BODY BASED ON THE CONTACTLESS DIRECT CURRENT MOTOR WITH A WINDING PRINTING DISK STATOR FOR SMALL SPACECRAFTS
Balandina T.N., Balandin E.A.
SOLAR BATTERIES EXPERIMENTALUNIT WITH CONCENTRATOR:IDEA, CONSTRUCTION, METHODOLOGY OF FLIGHT TESTS
Mel'nikov P.I., Kudryashov V.S., Kuzoro V.I., Shangina E.A., Melnikov P.I., Kudryashov V.S., Kuzoro V.I., Shangina E.A.
GEOSTATIONARY SPACECRAFT ATTITUDE AND ORBIT CONTROL BY MOTIONLESS ORBIT CONTROL THRUSTERS
Yermoshkin Y.M., Raevsky V.A., Urusov V.M.
METHODOLOGICAL BASES OF ESTIMATION OF SYSTEMIC ACTION OF ADDITIONAL PAYLOAD ON SPACECRAFT FUNCTIONING
Kislitskiy M.I.
CRITERIAOF ORBITALCONTROLTHRUSTER OPTIMALALLOCATIONON BOARD OFGEOSTATIONARY SPACECRAFT
Ermoshkin Y.M., Urusov V.M., Yermoshkin Y.M., Urusov V.M.
TOP-DOWN APPROACH FOR SPACECRAFT DEVELOPMENT
Lihachev M.V.
Designing and constructing of the program-mathematical model for the spacecraft command and measuring system
Nozhenkova L.F., Isaeva O.S., Gruzenko E.A.
The research of effective thermal conductivity coefficient effect on the temperature field of reflector
Burova O.V., Romankov E.V., Tsivilev I.N., Minakov A.V.
SEPARATION DEVICE FOR SPACECRAFT UNPRESSURIZED PLATFORMS BASED ON ISOGRID STRUCTURES
Vehov A.S.
PROGRAM COMPLEX FOR MODELING OF STABILIZED MOTION OF SPACECRAFT WITH TRANSFORMABLE FLEXIBLE PARTS
Ignatyev M.G., Kopylov V.M., Kulakov A.J., Sotnikov M.V.
MATHEMATICAL MODEL FOR GEOSTATIONARY SPACECRAFT DISTURBING TORQUES DETERMINATION
Latyntsev S.V., Murygin A.V.
TWO-DIMENSIONAL THERMAL MODEL OF THE THERMAL CONTROL SYSTEM FOR NONHERMETIC FORMATION SPACECRAFT
Tanasienko F.V., Shevchenko Y.N., Delkov A.V., Kishkin A.A.
SOFTWARE SUPPORT FOR TESTING of large spacecraft REFLECTOR AND EVALUATION OF THE OPERATION PARAMETERS OF COMPONENT WEIGHT COMPENSATION SYSTEM
Kovalev I.V., Badanina J.O.
DOUBLE-CONIC ADAPTER FOR LAUNCHING THE BLOCK OF THREE SPACECRAFTS
Khakhlenkova A.A.
FREQUENCY ANALYSIS OF THE LONGITUDINAL AND TRANSVERSE VIBRATIONS OF LATTICE CYLINDRICAL SHELL WITH OPENINGS
Shatov A.V., Khakhlenkova A.A.
REDUCTION OF SPACECRAFT HARNESS MASS
Dvirnyi V.V., Eremenko N.V., Dvirnyi G.V.
Development of mechanical test procedure for the fuel bellows tanks
Ermoshkin Y.M., Orlov S.A., Usanov A.Y.
DEVELOPMENT AND THERMAL VACUUM TESTS OF HEAT SHIELDS FOR PROTECTION OF MECHANICAL ELECTRIC DRIVE UNIT FROM EFFECT OF “SOLAR TRAP”
Vshivkov A.Y., Tanasienko F.V., Golovenkin E.N., Yurtaev E.V.
UPGRADING OF PHOTOVOLTAICARRAY SIMULATORWITH TWO-CIRCUIT CONTROL ELEMENT
Tkachev S.B., Mizrakh E.A., Tkachev S.B., Mizrakh E.A.
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