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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.A., Ovchinnikova E.V., Safonov K.V., Titov G.P., Khokhlov A.I., Gashin A.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.
Ensuring the thermal regime of spacecraft structures
Shatrov A.K., Rabetskaya O.I., Fisenko E.N.
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.
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.
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.
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 the payload extraction trajectory heavy class carrier rocket
Bordachev V.A., Kolga V.V.
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.
Using the principle of gravitational stabilization and orientation in the design of small spacecraft
Еsina P.A., Kornev V.M.
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.
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.
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.
Development of the heat panel of the small space apparatus for navigation support
Kolga V.V., Yarkov I.S., Yarkova E.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.
Development of workspace and algorithms for testing SpaceWire onboard equipment
Maksyutin A.S., Murygin A.V., Ivlenkov D.V., Dymov D.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.
Calculation of the coupling loss factors for the angle connected beams
Kravchunovky A.P.
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.
Small satellites for sea surface sounding
Kartsan I.N., Zhukov A.O.
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.
Control and regulation equipment of electric power system for a prospective piloted transport system
Savenkov V.V., Tishchenko A.K., Volokitin V.N.
Testing of spacecraft orientation and stabilization systems sing starry sky simulators
Gorelko M.G., Murygin A.V.
Ground control system for distant space vehicles
Zhukov A.O., Ivanov K.A., Bondareva M.K., Bondarev M.N., Gorovoy D.S.
Development of interface module emulator architecture for spacecraft life support systems
Komarov V.A., Semkin P.V.
Features of defining the damping function in spacecraft finite-element models
Kravchunovky A.P.
Control and regulation equipment of electric power system for a prospective piloted transport system
Savenkov V.V., Tishchenko A.K., Volokitin V.N.
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.
Development of interface module emulator architecture for spacecraft life support systems
Komarov V.A., Semkin P.V.
Problematic issues of application of methods of accelerated radiation testing of ECB
Avdyushkin S.A., Maximov I.A., Kochura S.G.
Inter-satellite optical communication link
Aleksandrov A.V., Vasilenko A.V., Korolev D.O.
Development concept of inter-satellite laser communication
Kartsan I.N.
Applying software-mathematical models of onboard equipment to develop onboard software
Lomaev Y.S., Ivanov I.A., Tolstykh A.V., Islentev E.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.
Development of the CYCLOPS CubeSat payload
Sotnikova N.V., Kadadova A.V., Utkin V.V., Kadochnikov D.M.
Possibility of unification of requirements for radiation resistance for spacecraft with different operating conditions
Nazarenko A.A., Maximov I.A., Kochura S.G.
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.
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.
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.
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.
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.
Implementation error of relative measurements
Garin E.N.
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.
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.
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.
CREATION OF THE FUEL SILPHON TANKS MECHANICAL TEST MODES
Yermoshkin Y.M., Orlov S.A., Usanov A.Y.
The problems of the transform antennas manufacture and development
Dvirny G.V.
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.
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