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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.
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.
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.
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.
Development of workspace and algorithms for testing SpaceWire onboard equipment
Maksyutin A.S., Murygin A.V., Ivlenkov D.V., Dymov D.V.
Testing of spacecraft orientation and stabilization systems sing starry sky simulators
Gorelko M.G., Murygin A.V.
Development of the CYCLOPS CubeSat payload
Sotnikova N.V., Kadadova A.V., Utkin V.V., Kadochnikov D.M.
Implementation error of relative measurements
Garin E.N.
Ground control system for distant space vehicles
Zhukov A.O., Ivanov K.A., Bondareva M.K., Bondarev M.N., Gorovoy D.S.
THE INFLUENCE OF CONDITIONS FOR PASSING GLONASS AND GPS SATELLITE RADIO NAVIGATION SIGNALS ON THE ERRORS OF DEFINING RELATIVE COORDINATES
Garin E.N.
PLATFORM OF AUTOMATION OF COMPONENT WEIGHT COMPENSATION SYSTEM FOR LARGE SPACECRAFT REFLECTOR
Kovalev I.V., Badanina J.O.
Review of technical solutions for developing of a control and data handling as a system on a chip for ultra small spacecraft
Khanov V.K., Borodina T.V., Antamoshkin A.N.
SOME RESULTS OF “PLASMA-PROGRESS” AND “RADAR-PROGRESS” ACTIVE SPACE EXPERIMENTS
Khakhinov V.V., Potekhin A.P., Lebedev V.P., Kushnarev D.S., Alsatkin S.S.
DEPLOYMENT DYNAMICS MATHEMATICAL MODELS USED FOR THE OVERSIZED TRANSFORMABLE MECHANICAL SYSTEMS DURING ON-GROUND COMPLEX FUNCTIONAL TESTS
Romanenko I.V., Dvirnyy V.V., Kuklin V.A., Perminov M.D.
SIMULATION MODELING OF THE MAIN COMPONENTS OF MOTION CONTROL SYSTEM OF THE SATELLITE
Yelubayev S.A., Jamalov N.K., Alipbayev K.A., Sukhenko A.S., Bopeyev T.M.
METHOD FOR CALCULATING THE ENERGY CHARACTERISTICS AND SOLAR BATTERY PARAMETERS OF HIGH-VOLTAGE POWER SUPPLY SYSTEMS
Chernaya M.M.
VERIFICATION OF FINITE-ELEMENT MODEL SPACECRAFT VIA TEST RESULTS
Balyakov D.F.
STUDENT PICOSATELLITE PLATFORM SIBQUBE: DEVELOPMENT OF PROTOTYPE STRUCTURE OF POCKETQUB CLASS PICOSATELLITE
Kravchunovsky A.P., Draganyuk M.N., Zuev D.M., Skorobogatov S.A., Movchan P.V.
LATTICE CYLINDRICAL SHELL WITH A ROUND TRANSVERSE PROFILE AND VARIABLE STIFFNESS
Khakhlenkova A.A.
GEOMETRICAL AND FINITE-ELEMENT MODELING OF LATTICE CONICAL SHELL WITH GEODESIC PATH OF SPIRAL RIBS
Khakhlenkova A.A., Shatov A.V.
Using the principle of gravitational stabilization and orientation in the design of small spacecraft
Еsina P.A., Kornev V.M.
Development of interface module emulator architecture for spacecraft life support systems
Komarov V.A., Semkin P.V.
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.M., Vnukov A.A., Volkov D.D., Kochev Y.V., Simanov R.S., Yakimov E.N., Grikhin G.S.
Features of defining the damping function in spacecraft finite-element models
Kravchunovky A.P.
Possibility of unification of requirements for radiation resistance for spacecraft with different operating conditions
Nazarenko A.A., Maximov I.A., Kochura S.G.
The problems of the transform antennas manufacture and development
Dvirny G.V.
TECHNIQUE FOR CALCULATION AND SELECTION OF SPACECRAFT ELECTRIC HEATERS PARAMETERS UNDER UNCERTAINTY CONDITIONS
Chebotarev V.E., Zvonar V.D., Fatkulin R.F., Dmitriev G.B.
COMBINED METHOD OF GONETS-M SPACECRAFT CONTROL MUL TIVERSION SOFTW ARE DESIGN
Antamoshkin O.
ADVANCED UNIFIED MICRO SERIES PLATFORMS
Zimin I.I., Valov M.V., Yakovlev A.V.
Comparison of direct and reverse cycle of the thermal control system for the non-hermetic spacecrafts
Delkov A.V., Hodenkov A.A., Shevchenko Y.N.
INVESTIGATION OF THE SPACE VEHICLES COATINGS FEATURES
Miheev A.E., Girn A.V., Ivasev S.S., Evkin I.V.
SATELLITE MASS CRITERIA OPTIMIZATION WITH THE USE OF CAD “ACAB”
Kochev Y.V., Efremov S.V., Ovchinnikov A.V.
PROCEDURE FOR EVALUATING THE EFFECTIVE USE RANGE OF THE UNIFIED SPACE PLATFORMS
Chebotarev V.E., Zimin I.I.
ANALYSIS OF LED-BASED SOLAR SIMULATOR DEVELOPMENT CAPABILITY FOR SPACECRAFT GROUND TESTING APPLICATIONS
Dvirniy G.V., Shevchuk A.A., Dvirniy V.V., Elfimova M.V., Krushenko G.G.
THE ALGORITHM FOR ESTIMATING ANGULAR RATE OF SPACECRAFT IN SURVIVABILITY MODE
Latyntsev S.V., Meus S.V., Оvсhinniкоv А.V.
AUTOMATED WEIGHT COMPENSATION SYSTEM FOR GROUND-BASED TRYOUT OF SPACE VEHICLE SOLAR PANELS
Verhoglyad A.G., Kuklin V.A., Makarov S.N., Mihalkin V.M., Halimanovich V.I.
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.
THERMAL STORAGE TO THE TEMPERATURE CONTROL SYSTEM OF POWERFUL BLOCKS OF ELECTRONIC EQUIPMENT WITH A SHORT ACTION TIME
Vasil’ev E.N., Derevyanko V.A., Chebotarev V.E.
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.
Control and regulation equipment of electric power system for a prospective piloted transport system
Savenkov V.V., Tishchenko A.K., Volokitin V.N.
Inter-satellite optical communication link
Aleksandrov A.V., Vasilenko A.V., Korolev D.O.
Methodology for calculating the de-weighting system of large-sized transformable elements of space vehicles for ground tests
Belyaev A.S., Filipas A.A., Tsavnin A.V., Tyryshkin A.V.
Implementation of “digital twin” technology within the thermo-elastic distortion testing of a precision carbon fiber reflector for the spacecraft antenna subsystem
Ivanov A.V.
CREATION OF THE FUEL SILPHON TANKS MECHANICAL TEST MODES
Yermoshkin Y.M., Orlov S.A., Usanov A.Y.
The main provisions of the methodology for ensuring the resistance of the onboard equipment of spacecraft to the effects of the radiation effects of outer space
Maximov I.A., Kochura S.G., Avdyushkin S.A.
About domestic system of space monitoring of emergencies
Testoedov N.A., Dvirnyj V.V., Nosenkov A.A., Elfimova M.V.
ELECTRONIC EQUIPMENT OF SPACECRAFT AND THERMOANALYSIS OF PRINTED-CIRCUIT -BOARDS
Yutkin A.V., Klimkin O.A., Dzyuvina A.
TESTING ELECTRONIC PARTS FROM FLIGHT LOTS ON DOSE EFFECTS FOR THE HARDNESS GUARANTEE OF SPACECRAFT ONBOARD EQUIPMENT
Zykov V.M., Maximov Y.V., Maximov I.A., Kochura S.G., Ivanov V.V., Patskov A.V.
Dynamics forecasting for electrical characteristics of spacecraft solar arrays by means of computational intelligence
Semenkina M.E., Semenkin E.S., Ryzhikov I.S.
PROPULSION OF A SPACECRAFT WITH THE ROTATING BATTERIES
Nadaraia C.G., Chestakov I.Y., Fadejev A.A., Nadaraia K.V.
Estimation of the form of a large-sized transformed reflector surface for a spacecraft
Goldobin N.N.
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.
THE METHOD OF SYNTHESIS OF THE DIGITAL CONTROLLER FOR A SOLAR ENERGY CONVERSION CHANNEL OF THE SOLAR BATTERY IN THE POWER SUPPLY SYSTEM OF A SPACECRAFT
Shkolnyi V.N., Semenov V.D., Kabirov V.A., Sukhorukov M.P., Torgaeva D.S.
SYSTEM APPROACH OF SELECTION TO PURPOSE DESIGNED EQUIPMENT OF SMALL SPACECRAFT
Kaloshin I.B., Kharlamov A.G., Skripachev V.O., Surovceva I.V., Ivanov V.K.
ANALYSIS OF CLEANING CONCEPTS OF NEAR-EARTH SPACE
Kirillov V.A., Bagateev I.R., Tarleckiy I.S., Balandina T.N., Balandin E.A.
INVESTIGATION OF CHARACTERISTICS OF ELECTRIC FIELD ARISING FROM ELECTROSTATIC DISCHARGE
Tikhomirov R.E., Maximov I.A., Trofimchuk D.A., Ivanov V.V., Maslov E.P.
Thermo-mechanical behavior of FORM-BUILDING EQUIPMENT FROM composite MATERIAL for reflector OF spacecraft antenna
Berdnikova N.A., Belov O.A., Babkin A.V., Belov D.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.
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