PART 1. MATHEMATICS, MECHANICS, COMPUTER SCIENCE
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A. M. Aleshechkin, O. A. Tronin
ACCURACY INCREASE OF DETERMINING NAVIGATION PARAMETERS FOR LONG-RANGE RADIONAVIGATION SYSTEMS
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V. P. Denisov [1], D. V. Dubinin [1], A. I. Kochegurov [2]*, V. E. Laevski (V. Geringer) [3]
THE RESULTS OF THE INVESTIGATION OF THE INTEGRATED PERFORMANCE EVALUATION METHOD OF EDGE DETECTION BASED ON THE TWO-DIMENSIONAL RENEWAL STREAM
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T. V. Zykova
ABOUT INTEGRATED REPRESENTATION LIKE MELLINA–BARNSA OF THE SOLUTION OF SYSTEM OF THE POLYNOMIAL EQUATIONS OF THE SPECIAL KIND
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L. A. Kazakovtsev*, A. N. Antamoshkin
GREEDY HEURISTIC METHOD FOR LOCATION PROBLEMS
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P. A. Kuznetsov
ON THE ANALYSIS OF THE EFFECTIVENESS OF FULLY REDUNDANTSYSTEMS
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L. L. Latushkina
ASSESSMENT OF DYNAMIC STABILITY OF A SIMPLE POWER SYSTEM IN AN OBJECT-ORIENTED PROGRAMMING ENVIRONMENT DELPHI
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E. D. Mihov
OPTIMIZATION OF COEFFICIENT OF BLURRING OF THE KERNEL IN NONPARAMETRIC MODELLING
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S. I. Senashov*, E. V. Filyushina, O. V. Gomonova
CONSTRUCTION OF ELASTO-PLASTIC BOUNDARIES using CONSERVATION LAWS
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T. V. Sidorova [1], T. V. Zykova [1]*, K. V. Safonov [2]
ABOUT MODIFICATION OF ONE-DIMENSIONAL FAST FOURIER TRANSFORM ON ALGORITHM OF COOLEY-TUKEY
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N. A. Testoedov [1], V. V. Dvirnyi [1], G. G. Krushenko [2]*, G. V. Dvirnyi [1]
THE POSSIBILITY OF CONSTRUCTING A RADIO COMMUNICATION USING ORBITAL REFLECTORS AND MAGNETIC ANTENNAS POLARIZATION ROTATING
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E. A. Chzhan
O THE PROBLEM OF GENERATION SAMPLE IN SOLVING THE PROBLEM OF NON INTERIAL PROCESSES IDENTIFICATION
PART 2. AVIATION AND SPACECRAFT ENGINEERING
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R. V. Akhmetzhanov [1], A. V. Bogatyi [1], P. A. Dronov [2], G. A. Dyakonov [1]*, A. V. Ivanov [2]
LOW-POWER RADIO-FREQUENCY ION THRUSTER
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S. A. Barabanov [1], V. I. Biryukov [2]*
ATTENUATION OF THE COMPELLED FLUCTUATIONS AND HYDROSHOCK WAVES IN THE TURBULENT STREAM OF EXTENDED PATHS OF POWER SUPPLY SYSTEMS OF LIQUID ROCKET ENGINES
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M. O. Dorofeev
DEFINITIONING TECHNIQUE OF SPATIAL POSITION OF NON-DEFORMING CONSTRUCTION OF SPACECRAFT
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D. V. Ermakov
REACTION WHEELS WITH MAGNETIC-HYDRAULIC BEARINGS
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Y. M. Ermoshkin, Y. V. Kochev*, D. A. Trofimchuk, E. N. Yakimov
ELECTROSTATIC DISCHARGE PROBLEM IN GEOSTATIONARY SPACECRAFT ELECTROJET PROPULSION SUBSYSTEM
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A. V. Klyuchnikov
DEVELOPING AND REFINING THE ALGORITHM OF SINGLE-PLANE DYNAMIC BALANCING OF A HIGH-SPEED FLYING PROTOTYPE
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Y. V. Krylov*, V. B. Taygin
DESIGN FEED ANTENNA Ka/Q-BAND BASED ON “REPAIRABLE” SCHEME
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M. V. Lihachev
TOP-DOWN APPROACH FOR SPACECRAFT DEVELOPMENT
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N. A. Testoedov, V. V. Dvirnyi, E. A. Morozov, G. V. Dvirnyi, N. V. Eremenko*
EXTENDING THE LIFE OF SATELLITE ON-BOARD UNITS
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A. O. Turchinovich
SIMULATION OF CHEMICAL INTERACTION OF COMBUSTION PRODUCTS WITH AIR BEHIND THE EXIT SECTION OF NOZZLES AIRCRAFT ENGINE
PART 3. TECHNOLOGICAL PROCESSES AND MATERIAL SCIENCE
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A. V. Kuklin [1]*, A. A. Kuzubov [1], [2], V. M. Denisov [1], E. A. Kovaleva [1], S. A. Shostak [1]
QUANTUM CHEMICAL STUDY OF STRUCTURE AND PROPERTIES OF CrN MONO- AND BILAYER
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N. S. Mikhaleva [1]*, A. A. Kuzubov [1], Z. I. Popov [2], A. D. Eremina [1], M. A. Visotin [1]
THEORETICAL STUDY OF LITHIUM ATOMS PENETRATION INTO SILICON
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A. E. Miheev [1]*, T. V. Trushkina [2], A. V. Girn [1], D. V. Ravodina [1]
DEVELOPMENT OF THE FUNCTIONAL DIAGRAM OF INFLUENCE OF THE BASIC FACTORS OF THE MDO PROCESS ON THE PROPERTIES OF COATINGS
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T. V. Piskazhova [1], S. B. Sidelnikov [1], V. M. Belolipetskii [2], P. N. Yakivyuk [1]*, A. S. Sidelnikov [1]
“VIRTUAL CC&RP” – A MATHEMATICAL MODEL FOR THE CONTROL OF THE UNIT CC&RP AND ITS VISUALIZATION WITH THE HELP OF SOFTWARE PRODUCTS WinCC 7.0 AND Step 7
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O. B. Romanova [1], [2]*, A. M. Kharkov [1], M. N. Sitnikov [1], V. V. Kretinin [1]
METAL-INSULATOR TRANSITION IN THE CATION-SUBSTITUTED COMPOUNDS ReXMn1-XS (Re = Gd, Sm, Ho)
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A. V. Ushakov [1], I. V. Karpov [1], A. A. Lepeshev [1], [2], A. A. Shaihadinov [1], L. Yu. Fedorov [1]*
TECHNOLOGY READY USE FOR PRODUCING NANOMATERIALS IN THE PLASMA OF A LOW-PRESSURE PULSED ARC DISCHARGE
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L. Yu. Fedorov [1]*, A. V. Ushakov [1], I. V. Karpov [1], A. A. Lepeshev [1], [2], A. A. Shaihadinov [1]
STUDY OF CARBIDE FORMATION IN THE PLASMA OF A LOW-PRESSURE PULSED ARC DISCHARGE
PART 4. ECONOMICS AEROSPACE INDUSTRY