Pesquisa

Edição
Título
Autores
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.
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.
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.
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.
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 influence of conditions for passing GLONASSand GPS satellite radio navigation signals on the errors of defining relative coordinates
Garin E.
The problems of telemetric data processingin the loop of spacecrafts computer-aided control system
Pakman D., Nekrasov M., Antamoshkin A.
Dual-use spacecraft conception
Kislitskiy M., Kislitsky M.
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.
MINIATURE ANTENNAS FOR CUBERSAT
Generalov A., Gadzhiev E.
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.
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.
FEATURES OF DEVELOPMENT OF THE COMBINED IMPELLENT INSTALLATION AND THE CIRCUIT OF FLIGHT OF THE SPACECRAFT «INTERGELIO-PROBE»
Platov I., Simonov A., Konstantinov M.
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