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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.
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