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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.
THE ANALYSIS OF COMPLETED, ONGOING AND POTENTIAL MISSIONS TO THE JUPITER SYSTEM
Gordienko E.S., Platov I.V., Simonov A.V.
The shock-absorber for executive powers of system of stabilisation of a spaceCRAFT
Vasiltsov A.A., Lipovtsev A.A.
ANALYSIS OF CLEANING CONCEPTS OF NEAR-EARTH SPACE
Kirillov V.A., Bagateev I.R., Tarleckiy I.S., Balandina T.N., Balandin E.A.
About domestic system of space monitoring of emergencies
Testoedov N.A., Dvirnyj V.V., Nosenkov A.A., Elfimova M.V.
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.
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.
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.
The influence of conditions for passing GLONASSand GPS satellite radio navigation signals on the errors of defining relative coordinates
Garin E.N.
Instrumental error of relative measurements
Garin E.N.
FEATURES OF EXPERIMENTAL DEFINITION OF COMPOSITE MATERIALS DURABILITY AGAINST EROSIVE IMPACT OF STATIONARY PLASMA THRUSTERS
Nadiradze A.B., Rachmatullin R.R., Kochura S.G., Maksimov I.A., Smirnov V.А.
ELECTRONIC EQUIPMENT OF SPACECRAFT AND THERMOANALYSIS OF PRINTED-CIRCUIT -BOARDS
Yutkin A.V., Klimkin O.A., Dzyuvina A.
TOP-DOWN APPROACH FOR SPACECRAFT DEVELOPMENT
Lihachev M.V.
Mobile system weightlessness simulation for a large spacecraft
Kovalev I.V., Kikot J.O.
THE QUESTIONS OF TECHNICAL REALIZATION OF THE DYNAMIC BENCH FOR THE RESEARCH OF THE ACTIVITY OF THE ENGINE-FLYWHEEL OF THE ATTITUDE CONTROL SYSTEM AND SPACE VEHICLE STABILIZATION
Sinitskiy D.E., Murigin A.V.
Estimation of the form of a large-sized transformed reflector surface for a spacecraft
Goldobin N.N.
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.
STRESS ANALYSIS OF SOLAR ARRAY DRIVER MECHANISM ACTUATOR OF THE SPACECRAFT “LUNA-RESURS-1”
Tambasova E.V., Tokarev A.V., Pavelko S.V., Таmbаsоv I.А.
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.
AUTOMATED SIMULATION SYSTEM OF ELECTRICAL CHARACTERISTICS OF SPACECRAFT POWER SYSTEM
Mizrah E.A., Poymanov D.N., Balakirev R.V., Tkachev S.B.
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 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.
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.
UNTIGHTENED PLATFORM OF SPACE VEHICLE FOR REMOTESOUNDING OFTHE EARTH
Shangina E.A., Rybakov A.S., Pasechnik K.A., Zaytsev P.A., Vlasov A., Shangina E.A., Ribakov А.С., Pasechnik К.А., Zaytsev P.A., Vlasov A.Y.
GEOSTATIONARY SPACECRAFT ATTITUDE AND ORBIT CONTROL BY MOTIONLESS ORBIT CONTROL THRUSTERS
Yermoshkin Y.M., Raevsky V.A., Urusov V.M.
BUNDLED SOFTWARE TO COMPUTE TEMPERATURE FIELDS OF SPACE VEHICLES PANELS WITH LEAKY CONSTRUCTION
Vasiljev E.N., Derevyanko V.V.
Ground control system for distant space vehicles
Zhukov A.O., Ivanov K.A., Bondareva M.K., Bondarev M.N., Gorovoy D.S.
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.
PLATFORM OF AUTOMATION OF COMPONENT WEIGHT COMPENSATION SYSTEM FOR LARGE SPACECRAFT REFLECTOR
Kovalev I.V., Badanina J.O.
Designing and constructing of the program-mathematical model for the spacecraft command and measuring system
Nozhenkova L.F., Isaeva O.S., Gruzenko E.A.
RESULTS OF 347K STATIC SUN SENSOR LABORATORY TESTING
Pirogov M.G., Varlamov V.I., Tsymbal G.L., Strizhova N.M., Demeshko S.A., Galchinskiy D.N., Safronov K.P., Polkunov B.A., Gebgart A.Y.
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.
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.
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.
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.
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.
The feature of the “Express-AMU3”, “Express-AMU7” spacecrafts injecton to geostationary orbit
Ermoshkin Y.M., Vnukov A.A., Volkov D.V., Kochev Y.V., Simanov R.S., Yakimov E.N., Pridannikov S.Y.
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.
The problems of telemetric data processingin the loop of spacecrafts computer-aided control system
Pakman D.N., Nekrasov M.V., Antamoshkin A.N.
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.
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.
ADVANCED UNIFIED MICRO SERIES PLATFORMS
Zimin I.I., Valov M.V., Yakovlev A.V.
“SibCube” - CubeSAT satellite project of SibSAU student
Zuev D.M., Pyatkov A.G., Movchan P.V., Smirnov D.V., Kostyukov A.S.
ORGANIZATION THROUGH CHANNEL TELEVISION SPACE BRIDGES WITH USAGE OF MULTIFUNCTIONAL SPACE SYSTEM RELAYING “LUCH”
Gromov K.V., Vigonskiy U.G., Roskin C.M., Kuzovnikov A.V., Muhin V.A.
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.
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.
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.
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.
Testing of spacecraft orientation and stabilization systems sing starry sky simulators
Gorelko M.G., Murygin A.V.
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.
METHODS FOR HIGH-ACCURACY MEASUREMENTS OF PRECISION STRUCTURES FOR MOBILE AUTOMATIC SPACECRAFT IN THERMAL VACUUM CONDITIONS
Dvirniy G.V.
MODERN SPACECRAFTS OPERATIONAL RELIABILITY AND QUALITY ANALYSIS
Patraev V.E., Trifanov I.V., Patraev V.E., Trifanov I.V.
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.
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.
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.
MINIATURE ANTENNAS FOR CUBERSAT
Generalov A.G., Gadzhiev E.V.
DESIGNING THE PROBLEM-ORIENTED INFRASTRUCTURE FOR SIMULATION MODELING OF SPACECRAFT ONBOARD EQUIPMENT
Nozhenkova L.F., Isaeva O.S.
IMPROVING ENERGY EFFICIENCY OF POWER SYSTEM SUPPLY OF THE PERSPECTIVE SPACE VEHICLES
Nadaraia C.G., Shestakov I.J., Fadeev A.A., Vinogradov K.N., Mikhalev D.V.
Ensuring the thermal regime of spacecraft structures
Shatrov A.K., Rabetskaya O.I., Fisenko E.N.
On remote sensing of the earth by spacecraft
Shlepkin A.A., Shiryaeva T.A., Shlepkin A.K., Filippov K.A., Pashkovskaya O.V.
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.
Testing laboratory patternswith thermoregulation coatings on carbon details of space vehicles
Khalimanovich V.I., Kharlamov V.A., Ermolaev R.A., Mikheev A.E., Girn A.V.
METHODOLOGICAL BASES OF ESTIMATION OF SYSTEMIC ACTION OF ADDITIONAL PAYLOAD ON SPACECRAFT FUNCTIONING
Kislitskiy M.I.
Approach to select of universal vibratory system
Semenova L.A., Lysenko E.A., Lysenko K.E., Semenova L.A., Lysenko E.A., Lysenko K.E.
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.
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.
Backgrounds and trends of all-electric propulsion geostationary satellites creation
Vnukov A.A., Rvacheva E.I.
PROBLEMS OF DEVELOPMENT OF LOW-ORBIT MULTIFUNCTIONAL PERSONAL SATELLITE COMMUNICATION SYSTEM «GONETS-D1M»
Kuzovnikov A.V., Testoedov N.A., Agureev V.A.
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.
INCREASE RELIABILITY OF ULTRAHIGH-FREQUENCY CHANNELS OF THE ACTIVE PHASED ARRAY ANTENNA MODULES
Kartsan I.N., Shangina E.A., Kiselev G.G., Efremova S.V.
ANALYSIS OF SPACECRAFT ORBITAL MOTION STABILITY OF GONETS-M NO 37152
Kolovsky I.K., Shmakov D.N., Podolyakin V.N.
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.
ASSESSMENT OF SPACECRAFT SOLAR ARRAY RELIABILITY DURING GROUND EXPERIMENTAL DEVELOPMENT TEST
Zakharov S.A.
N-version programming for nanosatellite telemetry processing
Efremova S.V.
Development of the heat panel of the small space apparatus for navigation support
Kolga V.V., Yarkov I.S., Yarkova E.A.
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.
Indicatrix account of materials dispersion at the estimations of erosion-contaminating influence of streams of plasma thrusters on space craft
Nadiradze A.B., Shaposhnikov V.V., Smirnov V.А., Maximov I.A., Kochura S.G.
The problems of the transform antennas manufacture and development
Dvirny G.V.
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.
Dual-use spacecraft conception
Kislitskiy M.I., Kislitsky M.I.
PROBLEMS OF SUPPORT OF RELIABLE OPERATION OF MODERN SC UNDER FACTORS OF SPACE AND TECHNOGENEOUS CHARACTER DESTABILISING INFLUENCE
Maksimov I.A., Maximov I.A.
Mathematical methods used to assess the position and form accuracy of a large-sized spacecraft reflector
Goldobin N.N.
MICROELECTRONIC SYSTEMS FOR AUTOMATION OF PERSPECTIVE SPACE VEHICLES
Nepomnuashy O.V., Ohotkin K.G., Habarov V.A.
ONBOARD COMPUTER COMPLEX FOR UNPRESSURISED LONG-RESOURCED SPACECRAFTS
Kozlov I.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.
THE EVOLUTION OF THE PROJECT “SEA LAUNCH” OF SPACECRAFT
Testoedov N.A., Dvirnyi V.V., Krushenko G.G., Dvirnyi G.V.
SOLAR SIMULATORS FOR THERMAL VACUUM TESTS OF SPACECRAFT
Aslanyan R.O., Anisimov D.I., Marchenko I.A., Panteleev V.I.
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.
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