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Radiation conditions in medium circular orbit during the extreme magnetic storm in May 2024
Shelepov M.D., Ivanov V.V., Kochura S.G., Maksimov I.A., Molchanov K.V., Prokopyev V.Y.
Parametric analysis of the anisogrid body of the spacecraft for cleaning the orbit of space debris
Belonovskaya I.D., Kolga V.V., Yarkov I.S., Yarkova E.A.
INVESTIGATION OF CHARGE-DISCHARGE PROCESSES IN THE SPACECRAFT DETACHABLE CONNECTOR
Tikhomirov R.E., Maximov I.A., Trofimchuk D.A., Ivanov V.V., Balashov S.V.
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.
Formation of an approach to modeling orbital operations assembly of a reconfigurable spacecraft on geostationary orbit
Koroleva Y.L., Hohlov A.I., Nikolaev D.A., Borisova N.V., Mathynenko M.G.
Formation of an approach to modeling orbital operations assembly of a reconfigurable spacecraft on geostationary orbit
Koroleva Y.L., Hohlov A.I., Nikolaev D.A., Borisova N.V., Mathynenko M.G.
The method of Haar sums for numerical solution of kinematic Poisson equations system that determine an evolution of a spacecraft position
Kirillov K.A., Ovchinnikova E.V., Safonov K.V., Titov G.P., Khokhlov A.I., Gashin A.A.
Results of monitoring the radiation environment in medium circular orbit
Eliseev D.V., Grafodatsky O.S., Ivanov V.V., Maksimov I.A., Molchanov K.V., Prokopyev V.Y.
Development of interface module emulator architecture for spacecraft life support systems
Komarov V.A., Semkin P.V.
Applying software-mathematical models of onboard equipment to develop onboard software
Lomaev Y.S., Ivanov I.A., Tolstykh A.V., Islentev E.V.
Problematic issues of application of methods of accelerated radiation testing of ECB
Avdyushkin S.A., Maximov I.A., Kochura S.G.
THE DETERMINATION OF RELATIVE COORDINATES BASEDON THE RETRANSMISSION OF NAVIGATION SIGNALSOF THE GLONASS AND GPS SYSTEMS
Garin Е.N.
BUNDLED SOFTWARE TO COMPUTE TEMPERATURE FIELDS OF SPACE VEHICLES PANELS WITH LEAKY CONSTRUCTION
Vasiljev E.N., Derevyanko V.V.
THE INFLUENCE OF CONDITIONS FOR PASSING GLONASS AND GPS SATELLITE RADIO NAVIGATION SIGNALS ON THE ERRORS OF DEFINING RELATIVE COORDINATES
Garin E.N.
DISTRIBUTED PARAMETERS ENERGY-HEAT MODEL OF SPACE NICKEL-HYDROGEN STORAGE BATTERY
Sakhnov M.Y., Lelekov A.T., Galochkin S.A., Sahnov M.Y., Lelekov A.T., Galochkin S.A.
SYSTEM FOR MONITORING THE LEVELS OF SPACE ENVIRONMENT EXPOSURE EXPERIENCED BY SATELLITES DEVELOPED BY “INFORMATION SATELLITE SYSTEMS” COMPANY
Testoedov N.A., Kochura S.G., Maximov I.A.
A construction algorithm of the peripheral cord of the frontal network for the space reflector with the cable-mesh deployable structure
Goldobin N.N., Testoedov N.A.
SOME ASPECTS OF ALTERNATE DESIGN, PRODUCTION TECHNOLOGY, TESTS AND OPERATION OF AMORTIZATION PLATFORM FOR FIXATION OF AUTOMATIC SPACECRAFT IN TRANSPORT CONTAINER
Testoedov N.A., Lozovenko S.N., Golovenkin E.N., Antipiev A.I., Tsaytler A.V.
RESULTS AND PROSPECTS OF JOINT HEAT PHYSICAL RESEARCHES OF ICM OF THE SB RAS AND JSC “ACADEMICIAN M.F. RESHETNEV “INFORMATION SATELLITE SYSTEMS”
Shaidurov V.V., Derevyanko V.A., Vasilyev E.N., Kosenko V.E., Zvonar V.D., Chebotarev V.E.
ORGANIZATION OF COMPLEX TESTING OF THE SPACECRAFT COMMAND AND MEASURING SYSTEM
Nozhenkova L.F., Isaeva O.S., Koldyrev A.Y.
THE ANALYSIS OF THE IMPACT OF THE METHOD OF FASTENING ON STRAIN-STRESS BEHAVIOR OF COMPOSITE OVERWRAPPED PRESSURE VESSEL
Mironenko E.D., Miheev A.E.
THE ANALYSIS OF COMPLETED, ONGOING AND POTENTIAL MISSIONS TO THE JUPITER SYSTEM
Gordienko E.S., Platov I.V., Simonov A.V.
DESIGNING THE PROBLEM-ORIENTED INFRASTRUCTURE FOR SIMULATION MODELING OF SPACECRAFT ONBOARD EQUIPMENT
Nozhenkova L.F., Isaeva O.S.
AUTOMATED SIMULATION SYSTEM OF ELECTRICAL CHARACTERISTICS OF SPACECRAFT POWER SYSTEM
Mizrah E.A., Poymanov D.N., Balakirev R.V., Tkachev S.B.
SATELLITE-BORNE MICROPROCESSOR CONTROL SYSTEM WITH IMPROVE UPSET TOLERANCE
Udalov D.V.
Study of the payload extraction trajectory heavy class carrier rocket
Bordachev V.A., Kolga V.V.
Inter-satellite optical communication link
Aleksandrov A.V., Vasilenko A.V., Korolev D.O.
On remote sensing of the earth by spacecraft
Shlepkin A.A., Shiryaeva T.A., Shlepkin A.K., Filippov K.A., Pashkovskaya O.V.
Multiversion model of software control systems for space vehicles with range of decision-making
Kartsan I.N., Efremova S.V.
Development concept of inter-satellite laser communication
Kartsan I.N.
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.
MA THEMA TICHAL PROVIDING OF THE PLANNING METHODOF SUPERVISORY EQUIPMENT SYSTEM PREP ARA TION FOR ELECTRONICAND RADIOTESTING OF SPACECRAFTS
Voronkovich V.Z., Iosifov P.A.
Automated control system of heat fluxes at thermovacuum testing of spacecrafts
Shevlyakov A.V., Vykhristyuk I.A., Verkhoglyad A.G., Khalimanovich V.I., Hristich V.V.
Backgrounds and trends of all-electric propulsion geostationary satellites creation
Vnukov A.A., Rvacheva E.I.
ELASTIC FEED SYSTEMS OF FUEL TANKS
Platov I.V.
Dynamical workbench for signature analysis and operating conditions of flywheel engine group of pointing and attitude control systems of spacecrafts
Synitskiy D.E., Murygin A.V.
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.
Calculation of the coupling loss factors for the angle connected beams
Kravchunovky A.P.
Applying software-mathematical models of onboard equipment to develop onboard software
Lomaev Y.S., Ivanov I.A., Tolstykh A.V., Islentev E.V.
Study of impeller design parameters effect on the axial thrust of a centrifugal electric pump assembly
Kuznetsova Z.A., Sinichenko M.I., Kuznetsov A.D., Kleshnina I.A., Sin'kovskiy F.K.
Pressure measurement inside non-sealed equipment bay of the geostationary spacecraft
Mordovskiy S.A., Maximov I.A., Ivanov V.V., Sitnikova N.N., Trofimchuk D.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.
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.
Ensuring the thermal regime of spacecraft structures
Shatrov A.K., Rabetskaya O.I., Fisenko E.N.
Additional screening tests at the testing technical center for ground power equipment
Aliseenko Y.V., Nesterishin M.V., Vorontsova E.O., Fedosov V.V., Panteleev V.I.
Development of the heat panel of the small space apparatus for navigation support
Kolga V.V., Yarkov I.S., Yarkova E.A.
Small satellites for sea surface sounding
Kartsan I.N., Zhukov A.O.
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.
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.
FREQUENCY ANALYSIS OF THE LONGITUDINAL AND TRANSVERSE VIBRATIONS OF LATTICE CYLINDRICAL SHELL WITH OPENINGS
Shatov A.V., Khakhlenkova A.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.
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.
Alternative method of solar simulation for thermal vacuum tests of spacecraft
Shevchuk A.A.
Methodological principles of space vehicle design for the maximum energy sup-ply of the payload
Chebotarev V.E., Fatkulin R.F., Vorontsova E.O., Balandina T.N., Shangina E.A.
Design of a thermal control system with a two-phase coolant for a spacecraft with a capacity of 7 kW
Shilkin O.V., Kolesnikov A.P., Delkov A.V., Kishkin A.A., Shevchenko Y.N.
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.
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.
ASSESSMENT OF SPACECRAFT SOLAR ARRAY RELIABILITY DURING GROUND EXPERIMENTAL DEVELOPMENT TEST
Zakharov S.A.
REDUCTION OF SPACECRAFT HARNESS MASS
Dvirnyi V.V., Eremenko N.V., Dvirnyi G.V.
Innovative technical solutions developed under the leadership of M. F. Reshetnev in the creation of the first Siberian launcher “Cosmos-3M”
Nazarov V.P., Golovenkin E.N., Piunov V.Y.
Control and regulation equipment of electric power system for a prospective piloted transport system
Savenkov V.V., Tishchenko A.K., Volokitin V.N.
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