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The method of Haar sums for numerical solution of kinematic Poisson equations system that determine an evolution of a spacecraft position
Kirillov K., Ovchinnikova E., Safonov K., Titov G., Khokhlov A., Gashin A.
Formation of an approach to modeling orbital operations assembly of a reconfigurable spacecraft on geostationary orbit
Koroleva Y., Hohlov A., Nikolaev D., Borisova N., Mathynenko M.
Ensuring the thermal regime of spacecraft structures
Shatrov A., Rabetskaya O., Fisenko E.
Parametric analysis of the anisogrid body of the spacecraft for cleaning the orbit of space debris
Belonovskaya I., Kolga V., Yarkov I., Yarkova E.
Results of monitoring the radiation environment in medium circular orbit
Eliseev D., Grafodatsky O., Ivanov V., Maksimov I., Molchanov K., Prokopyev V.
Applying software-mathematical models of onboard equipment to develop onboard software
Lomaev Y., Ivanov I., Tolstykh A., Islentev E.
Study of the payload extraction trajectory heavy class carrier rocket
Bordachev V., Kolga V.
Design of a thermal control system with a two-phase coolant for a spacecraft with a capacity of 7 kW
Shilkin O., Kolesnikov A., Delkov A., Kishkin A., Shevchenko Y.
Using the principle of gravitational stabilization and orientation in the design of small spacecraft
Еsina P., Kornev 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., Vnukov A., Volkov D., Kochev Y., Simanov R., Yakimov E., Grikhin G.
Inter-satellite optical communication link
Aleksandrov A., Vasilenko A., Korolev D.
On remote sensing of the earth by spacecraft
Shlepkin A., Shiryaeva T., Shlepkin A., Filippov K., Pashkovskaya O.
Multiversion model of software control systems for space vehicles with range of decision-making
Kartsan I., Efremova S.
Pressure measurement inside non-sealed equipment bay of the geostationary spacecraft
Mordovskiy S., Maximov I., Ivanov V., Sitnikova N., Trofimchuk D.
Additional screening tests at the testing technical center for ground power equipment
Aliseenko Y., Nesterishin M., Vorontsova E., Fedosov V., Panteleev V.
Development of workspace and algorithms for testing SpaceWire onboard equipment
Maksyutin A., Murygin A., Ivlenkov D., Dymov D.
Issues of ensuring the resistance of high-voltage solar arrays of spacecraft to the effects of secondary arc discharges
Valiullin V., Kochura S., Maximov I., Nadiradze A.
Calculation of the coupling loss factors for the angle connected beams
Kravchunovky A.
Study of impeller design parameters effect on the axial thrust of a centrifugal electric pump assembly
Kuznetsova Z., Sinichenko M., Kuznetsov A., Kleshnina I., Sin'kovskiy F.
Development of the heat panel of the small space apparatus for navigation support
Kolga V., Yarkov I., Yarkova E.
Methodological principles of space vehicle design for the maximum energy sup-ply of the payload
Chebotarev V., Fatkulin R., Vorontsova E., Balandina T., Shangina E.
Control and regulation equipment of electric power system for a prospective piloted transport system
Savenkov V., Tishchenko A., Volokitin V.
Testing of spacecraft orientation and stabilization systems sing starry sky simulators
Gorelko M., Murygin A.
Ground control system for distant space vehicles
Zhukov A., Ivanov K., Bondareva M., Bondarev M., Gorovoy D.
Development of interface module emulator architecture for spacecraft life support systems
Komarov V., Semkin P.
Features of defining the damping function in spacecraft finite-element models
Kravchunovky A.
Control and regulation equipment of electric power system for a prospective piloted transport system
Savenkov V., Tishchenko A., Volokitin V.
Methodology for calculating the de-weighting system of large-sized transformable elements of space vehicles for ground tests
Belyaev A., Filipas A., Tsavnin A., Tyryshkin 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.
Development of interface module emulator architecture for spacecraft life support systems
Komarov V., Semkin P.
Problematic issues of application of methods of accelerated radiation testing of ECB
Avdyushkin S., Maximov I., Kochura S.
Inter-satellite optical communication link
Aleksandrov A., Vasilenko A., Korolev D.
Development concept of inter-satellite laser communication
Kartsan I.
Applying software-mathematical models of onboard equipment to develop onboard software
Lomaev Y., Ivanov I., Tolstykh A., Islentev E.
Small satellites for sea surface sounding
Kartsan I., Zhukov A.
Development of the propulsion construction and the trajectory of the spacecrafts for the study of Martian planetary system
Platov I., Simonov A., Vorobyev A., Gordienko E.
Alternative method of solar simulation for thermal vacuum tests of spacecraft
Shevchuk A.
Formation of an approach to modeling orbital operations assembly of a reconfigurable spacecraft on geostationary orbit
Koroleva Y., Hohlov A., Nikolaev D., Borisova N., Mathynenko M.
Development of the CYCLOPS CubeSat payload
Sotnikova N., Kadadova A., Utkin V., Kadochnikov D.
Possibility of unification of requirements for radiation resistance for spacecraft with different operating conditions
Nazarenko A., Maximov I., Kochura S.
INVESTIGATION OF CHARGE-DISCHARGE PROCESSES IN THE SPACECRAFT DETACHABLE CONNECTOR
Tikhomirov R., Maximov I., Trofimchuk D., Ivanov V., Balashov S.
GEOSTATIONARY ORBITAL INJECTION OF A SPACECRAFT BY THE COMBINED METHOD
Yakovlev A., Vnukov A., Balandina T., Balandin E., Tarletskiy I.
THE INFLUENCE OF CONDITIONS FOR PASSING GLONASS AND GPS SATELLITE RADIO NAVIGATION SIGNALS ON THE ERRORS OF DEFINING RELATIVE COORDINATES
Garin E.
PLATFORM OF AUTOMATION OF COMPONENT WEIGHT COMPENSATION SYSTEM FOR LARGE SPACECRAFT REFLECTOR
Kovalev I., Badanina J.
Review of technical solutions for developing of a control and data handling as a system on a chip for ultra small spacecraft
Khanov V., Borodina T., Antamoshkin A.
SOME RESULTS OF “PLASMA-PROGRESS” AND “RADAR-PROGRESS” ACTIVE SPACE EXPERIMENTS
Khakhinov V., Potekhin A., Lebedev V., Kushnarev D., Alsatkin S.
DEPLOYMENT DYNAMICS MATHEMATICAL MODELS USED FOR THE OVERSIZED TRANSFORMABLE MECHANICAL SYSTEMS DURING ON-GROUND COMPLEX FUNCTIONAL TESTS
Romanenko I., Dvirnyy V., Kuklin V., Perminov M.
SIMULATION MODELING OF THE MAIN COMPONENTS OF MOTION CONTROL SYSTEM OF THE SATELLITE
Yelubayev S., Jamalov N., Alipbayev K., Sukhenko A., Bopeyev T.
METHOD FOR CALCULATING THE ENERGY CHARACTERISTICS AND SOLAR BATTERY PARAMETERS OF HIGH-VOLTAGE POWER SUPPLY SYSTEMS
Chernaya M.
VERIFICATION OF FINITE-ELEMENT MODEL SPACECRAFT VIA TEST RESULTS
Balyakov D.
STUDENT PICOSATELLITE PLATFORM SIBQUBE: DEVELOPMENT OF PROTOTYPE STRUCTURE OF POCKETQUB CLASS PICOSATELLITE
Kravchunovsky A., Draganyuk M., Zuev D., Skorobogatov S., Movchan P.
LATTICE CYLINDRICAL SHELL WITH A ROUND TRANSVERSE PROFILE AND VARIABLE STIFFNESS
Khakhlenkova A.
GEOMETRICAL AND FINITE-ELEMENT MODELING OF LATTICE CONICAL SHELL WITH GEODESIC PATH OF SPIRAL RIBS
Khakhlenkova A., Shatov A.
Implementation error of relative measurements
Garin E.
COMBINED METHOD OF GONETS-M SPACECRAFT CONTROL MUL TIVERSION SOFTW ARE DESIGN
Antamoshkin O.
ADVANCED UNIFIED MICRO SERIES PLATFORMS
Zimin I., Valov M., Yakovlev A.
Comparison of direct and reverse cycle of the thermal control system for the non-hermetic spacecrafts
Delkov A., Hodenkov A., Shevchenko Y.
INVESTIGATION OF THE SPACE VEHICLES COATINGS FEATURES
Miheev A., Girn A., Ivasev S., Evkin I.
SATELLITE MASS CRITERIA OPTIMIZATION WITH THE USE OF CAD “ACAB”
Kochev Y., Efremov S., Ovchinnikov A.
PROCEDURE FOR EVALUATING THE EFFECTIVE USE RANGE OF THE UNIFIED SPACE PLATFORMS
Chebotarev V., Zimin I.
ANALYSIS OF LED-BASED SOLAR SIMULATOR DEVELOPMENT CAPABILITY FOR SPACECRAFT GROUND TESTING APPLICATIONS
Dvirniy G., Shevchuk A., Dvirniy V., Elfimova M., Krushenko G.
THE ALGORITHM FOR ESTIMATING ANGULAR RATE OF SPACECRAFT IN SURVIVABILITY MODE
Latyntsev S., Meus S., Оvсhinniкоv А.
AUTOMATED WEIGHT COMPENSATION SYSTEM FOR GROUND-BASED TRYOUT OF SPACE VEHICLE SOLAR PANELS
Verhoglyad A., Kuklin V., Makarov S., Mihalkin V., Halimanovich V.
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., Simonov A.
THERMAL STORAGE TO THE TEMPERATURE CONTROL SYSTEM OF POWERFUL BLOCKS OF ELECTRONIC EQUIPMENT WITH A SHORT ACTION TIME
Vasil’ev E., Derevyanko V., Chebotarev V.
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., Kochura S., Avdyushkin S.
TECHNIQUE FOR CALCULATION AND SELECTION OF SPACECRAFT ELECTRIC HEATERS PARAMETERS UNDER UNCERTAINTY CONDITIONS
Chebotarev V., Zvonar V., Fatkulin R., Dmitriev G.
ELECTRONIC EQUIPMENT OF SPACECRAFT AND THERMOANALYSIS OF PRINTED-CIRCUIT -BOARDS
Yutkin A., Klimkin O., Dzyuvina A.
TESTING ELECTRONIC PARTS FROM FLIGHT LOTS ON DOSE EFFECTS FOR THE HARDNESS GUARANTEE OF SPACECRAFT ONBOARD EQUIPMENT
Zykov V., Maximov Y., Maximov I., Kochura S., Ivanov V., Patskov A.
Dynamics forecasting for electrical characteristics of spacecraft solar arrays by means of computational intelligence
Semenkina M., Semenkin E., Ryzhikov I.
PROPULSION OF A SPACECRAFT WITH THE ROTATING BATTERIES
Nadaraia C., Chestakov I., Fadejev A., Nadaraia K.
Estimation of the form of a large-sized transformed reflector surface for a spacecraft
Goldobin N.
DESIGN OF A LOW THRAST PROPULSION SYSTEM AND THE TRAJECTORIES OF SPASECRAFT TO THE CENTRE OF THE SOLAR SYSTEM
Platov I., Simonov A.
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., Semenov V., Kabirov V., Sukhorukov M., Torgaeva D.
SYSTEM APPROACH OF SELECTION TO PURPOSE DESIGNED EQUIPMENT OF SMALL SPACECRAFT
Kaloshin I., Kharlamov A., Skripachev V., Surovceva I., Ivanov V.
ANALYSIS OF CLEANING CONCEPTS OF NEAR-EARTH SPACE
Kirillov V., Bagateev I., Tarleckiy I., Balandina T., Balandin E.
INVESTIGATION OF CHARACTERISTICS OF ELECTRIC FIELD ARISING FROM ELECTROSTATIC DISCHARGE
Tikhomirov R., Maximov I., Trofimchuk D., Ivanov V., Maslov E.
Thermo-mechanical behavior of FORM-BUILDING EQUIPMENT FROM composite MATERIAL for reflector OF spacecraft antenna
Berdnikova N., Belov O., Babkin A., Belov D.
CREATION OF THE FUEL SILPHON TANKS MECHANICAL TEST MODES
Yermoshkin Y., Orlov S., Usanov A.
The problems of the transform antennas manufacture and development
Dvirny G.
About domestic system of space monitoring of emergencies
Testoedov N., Dvirnyj V., Nosenkov A., Elfimova M.
DISTRIBUTED PARAMETERS ENERGY-HEAT MODEL OF SPACE NICKEL-HYDROGEN STORAGE BATTERY
Sakhnov M., Lelekov A., Galochkin S., Sahnov M., Lelekov A., Galochkin S.
SYSTEM FOR MONITORING THE LEVELS OF SPACE ENVIRONMENT EXPOSURE EXPERIENCED BY SATELLITES DEVELOPED BY “INFORMATION SATELLITE SYSTEMS” COMPANY
Testoedov N., Kochura S., Maximov I.
A construction algorithm of the peripheral cord of the frontal network for the space reflector with the cable-mesh deployable structure
Goldobin N., Testoedov N.
SOME ASPECTS OF ALTERNATE DESIGN, PRODUCTION TECHNOLOGY, TESTS AND OPERATION OF AMORTIZATION PLATFORM FOR FIXATION OF AUTOMATIC SPACECRAFT IN TRANSPORT CONTAINER
Testoedov N., Lozovenko S., Golovenkin E., Antipiev A., Tsaytler 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., Derevyanko V., Vasilyev E., Kosenko V., Zvonar V., Chebotarev V.
ORGANIZATION OF COMPLEX TESTING OF THE SPACECRAFT COMMAND AND MEASURING SYSTEM
Nozhenkova L., Isaeva O., Koldyrev A.
THE ANALYSIS OF THE IMPACT OF THE METHOD OF FASTENING ON STRAIN-STRESS BEHAVIOR OF COMPOSITE OVERWRAPPED PRESSURE VESSEL
Mironenko E., Miheev A.
THE ANALYSIS OF COMPLETED, ONGOING AND POTENTIAL MISSIONS TO THE JUPITER SYSTEM
Gordienko E., Platov I., Simonov A.
DESIGNING THE PROBLEM-ORIENTED INFRASTRUCTURE FOR SIMULATION MODELING OF SPACECRAFT ONBOARD EQUIPMENT
Nozhenkova L., Isaeva O.
AUTOMATED SIMULATION SYSTEM OF ELECTRICAL CHARACTERISTICS OF SPACECRAFT POWER SYSTEM
Mizrah E., Poymanov D., Balakirev R., Tkachev S.
SATELLITE-BORNE MICROPROCESSOR CONTROL SYSTEM WITH IMPROVE UPSET TOLERANCE
Udalov D.
THE DETERMINATION OF RELATIVE COORDINATES BASEDON THE RETRANSMISSION OF NAVIGATION SIGNALSOF THE GLONASS AND GPS SYSTEMS
Garin Е.
BUNDLED SOFTWARE TO COMPUTE TEMPERATURE FIELDS OF SPACE VEHICLES PANELS WITH LEAKY CONSTRUCTION
Vasiljev E., Derevyanko V.
THE INFLUENCE OF CONDITIONS FOR PASSING GLONASS AND GPS SATELLITE RADIO NAVIGATION SIGNALS ON THE ERRORS OF DEFINING RELATIVE COORDINATES
Garin E.
MA THEMA TICHAL PROVIDING OF THE PLANNING METHODOF SUPERVISORY EQUIPMENT SYSTEM PREP ARA TION FOR ELECTRONICAND RADIOTESTING OF SPACECRAFTS
Voronkovich V., Iosifov P.
Automated control system of heat fluxes at thermovacuum testing of spacecrafts
Shevlyakov A., Vykhristyuk I., Verkhoglyad A., Khalimanovich V., Hristich V.
Backgrounds and trends of all-electric propulsion geostationary satellites creation
Vnukov A., Rvacheva E.
ELASTIC FEED SYSTEMS OF FUEL TANKS
Platov I.
Dynamical workbench for signature analysis and operating conditions of flywheel engine group of pointing and attitude control systems of spacecrafts
Synitskiy D., Murygin A.
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