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N-version programming for nanosatellite telemetry processing
Efremova S.
Ensuring the thermal regime of spacecraft structures
Shatrov A., Rabetskaya O., Fisenko E.
Applying software-mathematical models of onboard equipment to develop onboard software
Lomaev Y., Ivanov I., Tolstykh A., Islentev E.
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.
Additional screening tests at the testing technical center for ground power equipment
Aliseenko Y., Nesterishin M., Vorontsova E., Fedosov V., Panteleev V.
Pressure measurement inside non-sealed equipment bay of the geostationary spacecraft
Mordovskiy S., Maximov I., Ivanov V., Sitnikova N., Trofimchuk D.
Inter-satellite optical communication link
Aleksandrov A., Vasilenko A., Korolev D.
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.
On remote sensing of the earth by spacecraft
Shlepkin A., Shiryaeva T., Shlepkin A., Filippov K., Pashkovskaya O.
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.
Implementation of “digital twin” technology within the thermo-elastic distortion testing of a precision carbon fiber reflector for the spacecraft antenna subsystem
Ivanov A.
Inter-satellite optical communication link
Aleksandrov A., Vasilenko A., Korolev D.
Problematic issues of application of methods of accelerated radiation testing of ECB
Avdyushkin S., Maximov I., Kochura S.
Applying software-mathematical models of onboard equipment to develop onboard software
Lomaev Y., Ivanov I., Tolstykh A., Islentev 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.
Development concept of inter-satellite laser communication
Kartsan I.
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.
Ground control system for distant space vehicles
Zhukov A., Ivanov K., Bondareva M., Bondarev M., Gorovoy D.
The feature of the “Express-AMU3”, “Express-AMU7” spacecrafts injecton to geostationary orbit
Ermoshkin Y., Vnukov A., Volkov D., Kochev Y., Simanov R., Yakimov E., Pridannikov S.
Testing of spacecraft orientation and stabilization systems sing starry sky simulators
Gorelko M., Murygin A.
Features of defining the damping function in spacecraft finite-element models
Kravchunovky A.
THE ANALYSIS OF COMPLETED, ONGOING AND POTENTIAL MISSIONS TO THE JUPITER SYSTEM
Gordienko E., Platov I., Simonov A.
The shock-absorber for executive powers of system of stabilisation of a spaceCRAFT
Vasiltsov A., Lipovtsev A.
Possibility of unification of requirements for radiation resistance for spacecraft with different operating conditions
Nazarenko A., Maximov I., Kochura S.
ANALYSIS OF CLEANING CONCEPTS OF NEAR-EARTH SPACE
Kirillov V., Bagateev I., Tarleckiy I., Balandina T., Balandin E.
About domestic system of space monitoring of emergencies
Testoedov N., Dvirnyj V., Nosenkov A., Elfimova M.
Indicatrix account of materials dispersion at the estimations of erosion-contaminating influence of streams of plasma thrusters on space craft
Nadiradze A., Shaposhnikov V., Smirnov V., Maximov I., Kochura S.
Testing laboratory patternswith thermoregulation coatings on carbon details of space vehicles
Khalimanovich V., Kharlamov V., Ermolaev R., Mikheev A., Girn A.
DEVELOPMENT AND THERMAL VACUUM TESTS OF HEAT SHIELDS FOR PROTECTION OF MECHANICAL ELECTRIC DRIVE UNIT FROM EFFECT OF “SOLAR TRAP”
Vshivkov A., Tanasienko F., Golovenkin E., Yurtaev E.
Dual-use spacecraft conception
Kislitskiy M., Kislitsky M.
PROBLEMS OF SUPPORT OF RELIABLE OPERATION OF MODERN SC UNDER FACTORS OF SPACE AND TECHNOGENEOUS CHARACTER DESTABILISING INFLUENCE
Maksimov I., Maximov I.
Mathematical methods used to assess the position and form accuracy of a large-sized spacecraft reflector
Goldobin N.
MICROELECTRONIC SYSTEMS FOR AUTOMATION OF PERSPECTIVE SPACE VEHICLES
Nepomnuashy O., Ohotkin K., Habarov V.
ONBOARD COMPUTER COMPLEX FOR UNPRESSURISED LONG-RESOURCED SPACECRAFTS
Kozlov I.
ON THE CONCEPT OF ALL ELECTRIC PROPULSION SPACECRAFT
Yermoshkin Y., Volkov D., Yakimov E.
THE METHOD OF AUTOMATED DEVELOPMENT OF AN ASSEMBLY DRAWING OF A CABLE NETWORK
Butin A., Dubrovskiy E., Dobyshev E., Efremov S., Suntsov S.
THE EVOLUTION OF THE PROJECT “SEA LAUNCH” OF SPACECRAFT
Testoedov N., Dvirnyi V., Krushenko G., Dvirnyi G.
SOLAR SIMULATORS FOR THERMAL VACUUM TESTS OF SPACECRAFT
Aslanyan R., Anisimov D., Marchenko I., Panteleev V.
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.
ADAPTIVE MULTIBEAM ANTENNAS
Tyapkin V., Pershin A., Dmitriev D., Moshkina T.
Electric propulsions rational application range on the applied spacecrafts
Ermoshkin Y., Yermoshkin Y.
OPTIMIZATION OF WORKING OFF OF THE SPACE VEHICLE «JAMAL-300К»CREATED ON THE BASIS OF THE RECURRENT PLATFORM
Patraev V., Patraev V.
Automated control system of heat fluxes at thermovacuum testing of spacecrafts
Shevlyakov A., Vykhristyuk I., Verkhoglyad A., Khalimanovich V., Hristich V.
Unification methods of present telemetry processing systems in satellite control centers
Nekrasov M., Packman D., Antamoshkin A.
SEPARATION DEVICE FOR SPACECRAFT UNPRESSURIZED PLATFORMS BASED ON ISOGRID STRUCTURES
Vehov A.
DEVELOPMENT OF COMPOSITE PRECISION SATELLITE REFLECTOR: FINITE ELEMENT CONSTRUCTION MODELING
Lopatin A., Pasechnik K., Vlasov A., Shatov A.
MATHEMATICAL MODEL FOR GEOSTATIONARY SPACECRAFT DISTURBING TORQUES DETERMINATION
Latyntsev S., Murygin A.
MODELING OF SPECTROERERGETIC CHARACTERISTICS OF SPACE OBJECTS IN THE OPTICAL RANGE
Bogoyavlenskiy A., Kamenev A., Poluyan M., Soluyanov A.
SIMULATION MEANS OF ELECTROSTATIC DISCHARGES IN THE SYSTEM “STATIONARY PLASMA THRUSTER - TRANSFORMATION AND CONTROL SYSTEM”
Trofimchuk D., Bezhayev Y., Ivanov V., Kochura S., Maximov I.
GEOSTATIONARY ORBITAL INJECTION OF A SPACECRAFT BY THE COMBINED METHOD
Yakovlev A., Vnukov A., Balandina T., Balandin E., Tarletskiy I.
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.
Land control complex for small space vehicles
Kartsan I.
DISTINCTIVE FEATURES OF MAINTENANCE OF FLAWLESNESS OF NONREUSABLE MECHANICAL DEVICES FUNCTIONING ON SPACE VEHICLES
Pokhabov Y.
CRITERIAOF ORBITALCONTROLTHRUSTER OPTIMALALLOCATIONON BOARD OFGEOSTATIONARY SPACECRAFT
Ermoshkin Y., Urusov V., Yermoshkin Y., Urusov V.
METHODS AND ALGORITHMS FOR MICROPROGRAM CONTROL OF HIGH-SPEED, IMPULSE VOLTAGE REGULATORS FOR POWER SUPPLY OF ONBOARD EQUIPMENT OF PERSPECTIVE SPACE VEHICLES
Veysov E., Nepomnyashchiy O., Krasnobaev Y., Kapulin D., Veysov Е., Nepomnyaschi О., Krasnobaev U., Kapulin D.
Rational photovoltaic batteries mounting on the earth remote sensing microsatellite
Gubin S., Shepetov Y., Dolzhukova K.
INVESTIGATION OF THE SPACE VEHICLES COATINGS FEATURES
Miheev A., Girn A., Ivasev S., Evkin I.
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.
SOFTWARE SUPPORT FOR TESTING of large spacecraft REFLECTOR AND EVALUATION OF THE OPERATION PARAMETERS OF COMPONENT WEIGHT COMPENSATION SYSTEM
Kovalev I., Badanina J.
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.
FEATURES OF DEVELOPMENT OF THE COMBINED IMPELLENT INSTALLATION AND THE CIRCUIT OF FLIGHT OF THE SPACECRAFT «INTERGELIO-PROBE»
Platov I., Simonov A., Konstantinov M.
ADAPTIVE MULTI BEAM ANTENNA JSC «ISS»
Pershin A., Uzolin E., Pershin A., Uzolin E.
The influence of conditions for passing GLONASSand GPS satellite radio navigation signals on the errors of defining relative coordinates
Garin E.
Instrumental error of relative measurements
Garin E.
FEATURES OF EXPERIMENTAL DEFINITION OF COMPOSITE MATERIALS DURABILITY AGAINST EROSIVE IMPACT OF STATIONARY PLASMA THRUSTERS
Nadiradze A., Rachmatullin R., Kochura S., Maksimov I., Smirnov V.
ELECTRONIC EQUIPMENT OF SPACECRAFT AND THERMOANALYSIS OF PRINTED-CIRCUIT -BOARDS
Yutkin A., Klimkin O., Dzyuvina A.
TOP-DOWN APPROACH FOR SPACECRAFT DEVELOPMENT
Lihachev M.
Mobile system weightlessness simulation for a large spacecraft
Kovalev I., Kikot J.
THE QUESTIONS OF TECHNICAL REALIZATION OF THE DYNAMIC BENCH FOR THE RESEARCH OF THE ACTIVITY OF THE ENGINE-FLYWHEEL OF THE ATTITUDE CONTROL SYSTEM AND SPACE VEHICLE STABILIZATION
Sinitskiy D., Murigin A.
Estimation of the form of a large-sized transformed reflector surface for a spacecraft
Goldobin N.
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.
STRESS ANALYSIS OF SOLAR ARRAY DRIVER MECHANISM ACTUATOR OF THE SPACECRAFT “LUNA-RESURS-1”
Tambasova E., Tokarev A., Pavelko S., Таmbаsоv I.
STUDENT PICOSATELLITE PLATFORM SIBQUBE: DEVELOPMENT OF PROTOTYPE STRUCTURE OF POCKETQUB CLASS PICOSATELLITE
Kravchunovsky A., Draganyuk M., Zuev D., Skorobogatov S., Movchan P.
AUTOMATED SIMULATION SYSTEM OF ELECTRICAL CHARACTERISTICS OF SPACECRAFT POWER SYSTEM
Mizrah E., Poymanov D., Balakirev R., Tkachev S.
UNTIGHTENED PLATFORM OF SPACE VEHICLE FOR REMOTESOUNDING OFTHE EARTH
Shangina E., Rybakov A., Pasechnik K., Zaytsev P., Vlasov A., Shangina E., Ribakov А., Pasechnik К., Zaytsev P., Vlasov A.
GEOSTATIONARY SPACECRAFT ATTITUDE AND ORBIT CONTROL BY MOTIONLESS ORBIT CONTROL THRUSTERS
Yermoshkin Y., Raevsky V., Urusov V.
BUNDLED SOFTWARE TO COMPUTE TEMPERATURE FIELDS OF SPACE VEHICLES PANELS WITH LEAKY CONSTRUCTION
Vasiljev E., Derevyanko V.
DISTRIBUTED PARAMETERS ENERGY-HEAT MODEL OF SPACE NICKEL-HYDROGEN STORAGE BATTERY
Sakhnov M., Lelekov A., Galochkin S., Sahnov M., Lelekov A., Galochkin S.
PLATFORM OF AUTOMATION OF COMPONENT WEIGHT COMPENSATION SYSTEM FOR LARGE SPACECRAFT REFLECTOR
Kovalev I., Badanina J.
Designing and constructing of the program-mathematical model for the spacecraft command and measuring system
Nozhenkova L., Isaeva O., Gruzenko E.
RESULTS OF 347K STATIC SUN SENSOR LABORATORY TESTING
Pirogov M., Varlamov V., Tsymbal G., Strizhova N., Demeshko S., Galchinskiy D., Safronov K., Polkunov B., Gebgart A.
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.
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.
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.
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.
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