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SOFTWARE SUPPORT FOR TESTING COMMAND RECEPTION AND TRANSMISSION AND TELEMETRY ANALYSIS IN THE COMMAND-AND-MEASURING SYSTEM
Nozhenkova L., Isaeva O., Vogorovskiy R., Gruzenko E.
AN ELECTROMECHANICAL EXECUTIVE BODY BASED ON THE CONTACTLESS DIRECT CURRENT MOTOR WITH A WINDING PRINTING DISK STATOR FOR SMALL SPACECRAFTS
Balandina T., Balandin E.
SOLAR BATTERIES EXPERIMENTALUNIT WITH CONCENTRATOR:IDEA, CONSTRUCTION, METHODOLOGY OF FLIGHT TESTS
Mel'nikov P., Kudryashov V., Kuzoro V., Shangina E., Melnikov P., Kudryashov V., Kuzoro V., Shangina E.
Method of calculation of parameters of forest fires,as dynamic processes in the earth surface based on space monitoring data
Komorovski V., Dorrer G.
The problems of telemetric data processingin the loop of spacecrafts computer-aided control system
Pakman D., Nekrasov M., Antamoshkin A.
TECHNIQUE FOR CALCULATION AND SELECTION OF SPACECRAFT ELECTRIC HEATERS PARAMETERS UNDER UNCERTAINTY CONDITIONS
Chebotarev V., Zvonar V., Fatkulin R., Dmitriev G.
MA THEMA TICHAL PROVIDING OF THE PLANNING METHODOF SUPERVISORY EQUIPMENT SYSTEM PREP ARA TION FOR ELECTRONICAND RADIOTESTING OF SPACECRAFTS
Voronkovich V., Iosifov P.
ADVANCED UNIFIED MICRO SERIES PLATFORMS
Zimin I., Valov M., Yakovlev A.
“SibCube” - CubeSAT satellite project of SibSAU student
Zuev D., Pyatkov A., Movchan P., Smirnov D., Kostyukov A.
ORGANIZATION THROUGH CHANNEL TELEVISION SPACE BRIDGES WITH USAGE OF MULTIFUNCTIONAL SPACE SYSTEM RELAYING “LUCH”
Gromov K., Vigonskiy U., Roskin C., Kuzovnikov A., Muhin 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., 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.
SYSTEM APPROACH OF SELECTION TO PURPOSE DESIGNED EQUIPMENT OF SMALL SPACECRAFT
Kaloshin I., Kharlamov A., Skripachev V., Surovceva I., Ivanov V.
APPLICATION OF THE METHOD OF LOAD TESTING WITH GROUND experimental METHOD of CONTROL UNITS OF antenna GUIDANCE system
Kudryashova G., Babanov D., Galimzyanov A.
PROBLEMS AND DECISIONS OF DESIGNING OF MICROPROCESSOR MODULES OF NAVIGATING EQUIPMENT OF USERS GLONASS
Shaidurov V., Veisov E., Nepomnyashy O.
METHODS FOR HIGH-ACCURACY MEASUREMENTS OF PRECISION STRUCTURES FOR MOBILE AUTOMATIC SPACECRAFT IN THERMAL VACUUM CONDITIONS
Dvirniy G.
MODERN SPACECRAFTS OPERATIONAL RELIABILITY AND QUALITY ANALYSIS
Patraev V., Trifanov I., Patraev V., Trifanov I.
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.
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.
THE REVIEW OF MODERN SOLAR CELLS FOR SPACE APPLICATION BASED ON AIIIBV MATERIALS
Slyshchenko E., Naumova A., Lebedev A., Genali M., Vagapova N., Zhalnin B.
MINIATURE ANTENNAS FOR CUBERSAT
Generalov A., Gadzhiev E.
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.
IMPROVING ENERGY EFFICIENCY OF POWER SYSTEM SUPPLY OF THE PERSPECTIVE SPACE VEHICLES
Nadaraia C., Shestakov I., Fadeev A., Vinogradov K., Mikhalev D.
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.
METHODOLOGICAL BASES OF ESTIMATION OF SYSTEMIC ACTION OF ADDITIONAL PAYLOAD ON SPACECRAFT FUNCTIONING
Kislitskiy M.
Approach to select of universal vibratory system
Semenova L., Lysenko E., Lysenko K., Semenova L., Lysenko E., Lysenko K.
GEOSTATIONARY SPACECRAFT ORBIT SLAVING AND MANEUVER: THRUSTERS ON DRIVES INSTALLATION SCHEME
Ermoshkin Y., Raevskiy V., Urusov V., Yermoshkin Y., Raevsky V., Urusov V.
SYSTEM FOR MONITORING THE LEVELS OF SPACE ENVIRONMENT EXPOSURE EXPERIENCED BY SATELLITES DEVELOPED BY “INFORMATION SATELLITE SYSTEMS” COMPANY
Testoedov N., Kochura S., Maximov I.
Backgrounds and trends of all-electric propulsion geostationary satellites creation
Vnukov A., Rvacheva E.
PROBLEMS OF DEVELOPMENT OF LOW-ORBIT MULTIFUNCTIONAL PERSONAL SATELLITE COMMUNICATION SYSTEM «GONETS-D1M»
Kuzovnikov A., Testoedov N., Agureev V.
Dynamical workbench for signature analysis and operating conditions of flywheel engine group of pointing and attitude control systems of spacecrafts
Synitskiy D., Murygin A.
INCREASE RELIABILITY OF ULTRAHIGH-FREQUENCY CHANNELS OF THE ACTIVE PHASED ARRAY ANTENNA MODULES
Kartsan I., Shangina E., Kiselev G., Efremova S.
ANALYSIS OF SPACECRAFT ORBITAL MOTION STABILITY OF GONETS-M NO 37152
Kolovsky I., Shmakov D., Podolyakin V.
IMPROVEMENT OF INSULATION RESISTANCE MEASUREMENT ACCURACY DURING SPACECRAFT POWER SYSTEM TESTS
Shtabel N., Samotik L., Mizrah E.
TO GEOSTATIONARY COLLOCATION PROBLEM
Kuprin A., Medvedev A.
ASSESSMENT OF SPACECRAFT SOLAR ARRAY RELIABILITY DURING GROUND EXPERIMENTAL DEVELOPMENT TEST
Zakharov S.
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