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Flight efficiency of solar thermal propulsion with double-stage thermal energy storage
Finogenov S.L., Kolomentsev A.I., Nazarov V.P.
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.
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.
ANALYSIS OF THE REQUIREMENTS PERFERMANCE OF INTERAGANCY COORDINATION COMMITTEE ON DEBRIS PREVENTION
Bulynin Y.L., Sozonova I.L.
The shock-absorber for executive powers of system of stabilisation of a spaceCRAFT
Vasiltsov A.A., Lipovtsev A.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.
Method of calculation of parameters of forest fires,as dynamic processes in the earth surface based on space monitoring data
Komorovski V.S., Dorrer G.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.
PROBLEMS AND DECISIONS OF DESIGNING OF MICROPROCESSOR MODULES OF NAVIGATING EQUIPMENT OF USERS GLONASS
Shaidurov V.V., Veisov E.A., Nepomnyashy O.
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.
THE ANALYSIS OF COMPLETED, ONGOING AND POTENTIAL MISSIONS TO THE JUPITER SYSTEM
Gordienko E.S., Platov I.V., Simonov A.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.
Structural shifts in the competitive high-tech modern space rocket technology directions of economic system of Russia
Popova T.S.
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.
Inter-satellite optical communication link
Aleksandrov A.V., Vasilenko A.V., Korolev D.O.
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.
Problematic issues of application of methods of accelerated radiation testing of ECB
Avdyushkin S.A., Maximov I.A., Kochura S.G.
CREATION OF THE FUEL SILPHON TANKS MECHANICAL TEST MODES
Yermoshkin Y.M., Orlov S.A., Usanov A.Y.
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.
ADAPTIVE MULTIBEAM ANTENNAS
Tyapkin V.N., Pershin A.S., Dmitriev D.D., Moshkina T.G.
Electric propulsions rational application range on the applied spacecrafts
Ermoshkin Y.M., Yermoshkin Y.M.
OPTIMIZATION OF WORKING OFF OF THE SPACE VEHICLE «JAMAL-300К»CREATED ON THE BASIS OF THE RECURRENT PLATFORM
Patraev V.E., Patraev V.E.
Automated control system of heat fluxes at thermovacuum testing of spacecrafts
Shevlyakov A.V., Vykhristyuk I.A., Verkhoglyad A.G., Khalimanovich V.I., Hristich V.V.
Unification methods of present telemetry processing systems in satellite control centers
Nekrasov M.V., Packman D.N., Antamoshkin A.N.
SEPARATION DEVICE FOR SPACECRAFT UNPRESSURIZED PLATFORMS BASED ON ISOGRID STRUCTURES
Vehov A.S.
DEVELOPMENT OF COMPOSITE PRECISION SATELLITE REFLECTOR: FINITE ELEMENT CONSTRUCTION MODELING
Lopatin A.V., Pasechnik K.A., Vlasov A.Y., Shatov A.V.
MATHEMATICAL MODEL FOR GEOSTATIONARY SPACECRAFT DISTURBING TORQUES DETERMINATION
Latyntsev S.V., Murygin A.V.
MODELING OF SPECTROERERGETIC CHARACTERISTICS OF SPACE OBJECTS IN THE OPTICAL RANGE
Bogoyavlenskiy A.I., Kamenev A.A., Poluyan M.M., Soluyanov A.A.
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.
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.
SATELLITE-BORNE MICROPROCESSOR CONTROL SYSTEM WITH IMPROVE UPSET TOLERANCE
Udalov D.V.
Using the principle of gravitational stabilization and orientation in the design of small spacecraft
Еsina P.A., Kornev V.M.
Applying software-mathematical models of onboard equipment to develop onboard software
Lomaev Y.S., Ivanov I.A., Tolstykh A.V., Islentev E.V.
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.
Development concept of inter-satellite laser communication
Kartsan I.N.
THE DETERMINATION OF RELATIVE COORDINATES BASEDON THE RETRANSMISSION OF NAVIGATION SIGNALSOF THE GLONASS AND GPS SYSTEMS
Garin Е.N.
Land control complex for small space vehicles
Kartsan I.N.
DISTINCTIVE FEATURES OF MAINTENANCE OF FLAWLESNESS OF NONREUSABLE MECHANICAL DEVICES FUNCTIONING ON SPACE VEHICLES
Pokhabov Y.P.
CRITERIAOF ORBITALCONTROLTHRUSTER OPTIMALALLOCATIONON BOARD OFGEOSTATIONARY SPACECRAFT
Ermoshkin Y.M., Urusov V.M., Yermoshkin Y.M., Urusov V.M.
METHODS AND ALGORITHMS FOR MICROPROGRAM CONTROL OF HIGH-SPEED, IMPULSE VOLTAGE REGULATORS FOR POWER SUPPLY OF ONBOARD EQUIPMENT OF PERSPECTIVE SPACE VEHICLES
Veysov E.A., Nepomnyashchiy O.V., Krasnobaev Y.V., Kapulin D.V., Veysov Е.А., Nepomnyaschi О.V., Krasnobaev U.V., Kapulin D.V.
Rational photovoltaic batteries mounting on the earth remote sensing microsatellite
Gubin S.V., Shepetov Y.A., Dolzhukova K.O.
INVESTIGATION OF THE SPACE VEHICLES COATINGS FEATURES
Miheev A.E., Girn A.V., Ivasev S.S., Evkin I.V.
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.
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