| 1 | 7.1.2025 Features of the implementation of smart technologies in accounting processes in enterprises in the rocket and space industry | 29 | 217 |
| 2 | 6.1.2025 Studying the landing of the reusable first stage of the Cyclone-5 space launch vehicle on a maritime landing platform-duplicate-1 | 32 | 438 |
| 3 | 5.1.2025 Studying the landing of the reusable first stage of the Cyclone-5 space launch vehicle on a maritime landing platform | 31 | 626 |
| 4 | 4.1.2025 Experimental development of a pyrolysis technology for unwinding carbon composites for filler reuse | 33 | 451 |
| 5 | 3.1.2025 Experimental research on separation diaphragm performance in propellant storage and feed systems of liquid propellant tanks | 37 | 547 |
| 6 | 2.1.2025 Justification of the parameters of a vertical screw conveyor for transporting lunar regolith | 35 | 490 |
| 7 | 1.1.2025 Promomoon initiative for moon village generation in honor of dr. Alexander degtyarev | 30 | 282 |
| 8 | 16.1.2024 EDUCATIONAL TENDENCIES AS AN ELEMENT OF INNOVATIVE PROGRESS IN THE PERSONNEL TRAINING SYSTEM FOR THE STATE-OF-THE-ART ENTERPRISES | 112 | 1458 |
| 9 | 15.1.2024 Enhancing operability of the fuel system units in the hot climate conditions | 108 | 3231 |
| 10 | 14.1.2024 EXPERIMENTAL STUDIES OF THE PERFORMANCE OF PYROTECHNIC DEVICES INSTALLED ON THE LAUNCH VEHICLE SEPARATION SYSTEMS | 102 | 2440 |
| 11 | 13.1.2024 MODEL OF QUALITY MANAGEMENT OF TECHNICAL PREPARATION FOR THE METAL+COMPOSITE JOINTS PRODUCTION | 111 | 1772 |
| 12 | 12.1.2024 Hardening of steels modifying their surfaces with ion-plasma nitriding in glow discharge | 116 | 3984 |
| 13 | 11.1.2024 PARAMETERS CALCULATION OF THE LUNAR REGOLITH TRANSPORT SYSTEM | 110 | 1968 |
| 14 | 10.1.2024 METHOD OF AUTONOMOUS DETERMINATION OF THE ROCKET’S REFERENCE ATTITUDE DURING PRE-LAUNCH PROCESSING | 123 | 2311 |
| 15 | 9.1.2024 General-purpose thermostatting module – new approach in development of up-to-date thermostating systems for rocket and space complexes | 124 | 2483 |
| 16 | 8.1.2024 Theoretic-experimental evaluation of the solid-propellant grain erosive burning | 111 | 1329 |
| 17 | 7.1.2024 Selection of the functional units for the Cyclone-4M ILV separation system | 131 | 3388 |
| 18 | 6.1.2024 New methods of load-carrying capacity prediction for the ultimately compressed frame structures | 118 | 2206 |
| 19 | 5.1.2024 Assessment of risk of toxic damage to people in case of a launch vehicle accident at flight | 141 | 2392 |
| 20 | 4.1.2024 The dynamics of servo drives | 100 | 1841 |
| 21 | 3.1.2024 Future projects of lunar exploration implemented by Yuzhnoye SDO | 117 | 1467 |
| 22 | 2.1.2024 New and advanced liquid rocket engines of the Yuzhnoye SDO | 128 | 2660 |
| 23 | 1.1.2024 ANTARES: Yuzhnoye’s project of XXI century | 77 | 438 |
| 24 | 9.1.2023 Methodology for selecting design parameters of solid-propellant sustainer engines. Mathematical support and software | 70 | 2303 |
| 25 | 8.1.2023 Specificity of developing pyrobolts with low impact and vibration impulse responses | 71 | 1575 |
| 26 | 7.1.2023 Specificity of using rubbers as structural materials for making connector assemblies of temperature conditioning systems | 79 | 1374 |
| 27 | 6.1.2023 Numerical modeling of translational and rotational vibrations of a solid-propellant rocket motor on a test stand during firing tests | 65 | 1406 |
| 28 | 5.1.2023 Fueling-neutralization stations. New developments and applications | 68 | 1585 |
| 29 | 4.1.2023 On control of spacecraft orientation to the ground data acquisition station | 66 | 839 |
| 30 | 3.1.2023 Analysis of a modernized 9K51 Hrad Multiple Rocket Launcher System to determine the performance specifications of the 122-mm unguided rocket projectile in development | 71 | 2273 |
| 31 | 2.1.2023 How Yuzhnoye develops models for flight safety index evaluation for the case of a rocket failure during the flight | 71 | 1738 |
| 32 | 1.1.2023 On the development of a methodology for building air and missile defense systems. Explanation of the investigation mechanism | 68 | 2208 |
| 33 | 21.1.2020 Contemporary approaches to the improvement of methods of space launch system operation for commercial launches of ILV | 103 | 1689 |
| 34 | 20.1.2020 Studying the possibility of alternating delivery of rocket propellant wastes to a common thermal neutralization facility | 106 | 1822 |
| 35 | 19.1.2020 Pyrobolts: types, design, development. Shear type pyrobolt developed at Yuzhnoye SDO | 162 | 2990 |
| 36 | 18.1.2020 Development of autonomous power engineering systems with hydrogen energy storage | 110 | 2888 |
| 37 | 17.1.2020 Acoustic problems of rocket launch | 109 | 2410 |
| 38 | 16.1.2020 Parameters of the supersonic jet of a block propulsion system, flowing into a gas duct, considering chemical kinetics of gas-cycle transformations | 117 | 3022 |
| 39 | 15.1.2020 Simulation of thermomechanical processes in functionally-gradient materials of inhomogeneous structure in the manufacturing and operation of rocket structural elements | 119 | 2917 |
| 40 | 14.1.2020 On the problem of optimum control | 118 | 1864 |
| 41 | 13.1.2020 Mathematical models of hydraulic servomechanisms of space technology | 112 | 1500 |
| 42 | 12.1.2020 Modification of technology as the main course in the military transport aircraft development | 116 | 1756 |
| 43 | 11.1.2020 Some results of strength calculations relying on analytical and FEM approaches. Trends of using contemporary machine learning strategies | 119 | 2361 |
| 44 | 10.1.2020 Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM | 112 | 2526 |
| 45 | 9.1.2020 Experimental investigation of a liner-free propellant tank made from polymer composite materials | 122 | 3195 |
| 46 | 8.1.2020 Determining the main parameters of transport aircraft modifications considering the fuel efficiency | 106 | 1008 |
| 47 | 7.1.2020 Studying the motion of a launch vehicle and observed space debris objects during launch preparation | 106 | 1770 |
| 48 | 6.1.2020 Mechanics of a satellite cluster. Methods for estimating the probability of their maximal approach in flight | 107 | 1466 |
| 49 | 5.1.2020 Strength and stability of inhomogeneous structures of space technology, consid-ering plasticity and creep | 116 | 4375 |
| 50 | 4.1.2020 Terminal guidance of the aircraft being maneuvering while descending in the atmosphere under conditions of aerodynamic balancing | 108 | 1372 |
| 51 | 3.1.2020 Analysis of the unsteady stress-strain behavior of the launch vehicle hold-down bay at liftoff | 126 | 2972 |
| 52 | 2.1.2020 Analysis of development trends of design parameters and basic characteristics of missiles for the advanced multiple launch rocket systems | 123 | 6328 |
| 53 | 1.1.2020 Solving a problem of optimum curves of descent using the enhanced Euler equation | 111 | 2764 |
| 54 | 14.2.2019 Selection of the validation algorithm for the solid rocket motor trust measurement procedure | 123 | 1504 |
| 55 | 13.2.2019 Study of the stress and strain state of the multilayer bellows | 110 | 1433 |
| 56 | 12.2.2019 Procedure of acoustic loads measuring during the ILV launch | 107 | 1026 |
| 57 | 11.2.2019 Winding the tubes of rectangular section using dowels | 106 | 1155 |
| 58 | 10.2.2019 Dynamic performance of the gas drive with jet motor | 120 | 3455 |
| 59 | 9.2.2019 Gas-dynamic simulation of the supersonic stream in the pulsed wind tunnel | 119 | 1988 |
| 60 | 8.2.2019 Evaluation of the external acoustic loads, acting on the rocket when it passes the leg with maximum velocity head | 122 | 564 |
| 61 | 7.2.2019 On critical stress of the longitudinal stability of the stiffened cylindrical shells. Dynamic problem | 105 | 773 |
| 62 | 6.2.2019 Stabilization of gas reducers adjustment | 120 | 1233 |
| 63 | 5.2.2019 Features of the development testing of the propellants deposition inside the tanks of launch vehicles | 115 | 1195 |
| 64 | 4.2.2019 Numerical simulation of behavior of elastic structures with local stiffening elementse | 110 | 1004 |
| 65 | 3.2.2019 Features of design and production of the technological aids for assembly of the spacecraft separation system of CLAMP BAND type | 101 | 1658 |
| 66 | 2.2.2019 Mathematical models for assessment of safety in the impact area of cluster ammunition of the warhead during missile complex testing | 113 | 2281 |
| 67 | 1.2.2019 Optimization of the trajectory of the antiaircraft guided missile | 122 | 3353 |
| 68 | 27.1.2019 Phases of Cooperation of Yuzhnoye SDO and Dnipro National University Physical Engineering Department on the Issues of Mutual Human Resourcing: Past, Present. Future | 98 | 1369 |
| 69 | 26.1.2019 New Technologies and Problems of Their Introducing in Ukraine | 104 | 1278 |
| 70 | 25.1.2019 Technological Peculiarities of Manufacturing Products of Irregular Profile by Method of Selective Laser Melting of 316L Powder Metal Material | 101 | 1647 |
| 71 | 24.1.2019 Porous Cast Materials (Gasars). Options of Their Use in Space Rocket Hardware | 119 | 1682 |
| 72 | 23.1.2019 Calculation of Thermal-Physical Properties of Gaseous Xenon | 99 | 1364 |
| 73 | 22.1.2019 Calculation of Uncertainty of Represented Values of Linear Accelerations during Centrifugal Machines Certification | 100 | 1138 |
| 74 | 21.1.2019 Optimization of Geometrical Shape of Isolation Valve Blading Position | 101 | 931 |
| 75 | 20.1.2019 Possibilities of Increasing Acting Loads on Hydraulic Actuator Middle Position Lock | 112 | 1015 |
| 76 | 19.1.2019 Peculiarities of Radio Transparent Fairings Development | 134 | 1346 |
| 77 | 18.1.2019 Designing of Servo Driver of Throttle Mechanisms and Fuel Flow Regulator of ILV Main Motor | 110 | 1222 |
| 78 | 17.1.2019 Development of Prospective Small-Size Auxiliary SMR of New Type | 107 | 1579 |
| 79 | 16.1.2019 Oscillation Processes in Rig at the Moment of SRM Transfer to Main Operation Mode | 108 | 1037 |
| 80 | 15.1.2019 Simulation of SMR Oscillations in Rig that Arise during Firing Bench Test | 107 | 1705 |
| 81 | 14.1.2019 Technique of Determination of SRM Operational Life Taking into Account Materials and Elements Strength Margins | 109 | 465 |
| 82 | 13.1.2019 Prediction of Solid Propellant Burnout Time in Launch Vehicle Propulsion System in Flight | 110 | 1310 |
| 83 | 12.1.2019 Monitoring of Launch Platform Drift Parameters during Zenit-3SL Integrated Launch Vehicle Prelauch Processing | 102 | 1419 |
| 84 | 11.1.2019 Peculiarities of Development Testing of Space Rocket Thermostating System Mating Points Hoses | 110 | 754 |
| 85 | 10.1.2019 Semi-Empirical Evaluation of External Acoustic Loads in Payload Area during Lift-off | 104 | 1523 |
| 86 | 9.1.2019 Modeling of Cyclone-4M Rocket Jet Acoustic Emission by Volumetric Source | 123 | 1549 |
| 87 | 8.1.2019 Virtual Tests of Cassette Reentry Vehicle Dash Elements Attachment System during Ground Operation | 113 | 1909 |
| 88 | 7.1.2019 Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on High-Temperature Propellants | 114 | 854 |
| 89 | 6.1.2019 Investigation into Peculiarities of Delivery to Launch Base of Rocket Propellant with Specified Gasing | 104 | 1265 |
| 90 | 5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime | 121 | 1493 |
| 91 | 4.1.2019 Mathematic Modeling and Investigation into Stress-Strain State of Space Rocket Bays | 108 | 1608 |
| 92 | 3.1.2019 Analysis of Spacecraft Control Issues In Early Design Phases | 116 | 1118 |
| 93 | 2.1.2019 Flying Vehicle Maneuvering Dynamics in Atmosphere with Weight Asymmetry and Elements of Terminal Control in Turn Leg | 118 | 1027 |
| 94 | 1.1.2019 On 65-th anniversary of the company | 100 | 468 |
| 95 | 23.2.2018 On the Role of Space in Origination of Inertia Force Field, Earth Gravity Force Field and Zero Gravity of Material Body | 117 | 2119 |
| 96 | 22.2.2018 Uncertainty Calculation Procedure during Measuring Instrumentation Calibration | 101 | 3081 |
| 97 | 21.2.2018 Ensuring Aiming Accuracy of Ship’s Telemetry Reception Antenna Installation for Small Vessels | 96 | 1801 |
| 98 | 20.2.2018 The Use of Special Devices during Launch Pad Development Testing | 101 | 1486 |
| 99 | 19.2.2018 Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles | 106 | 1936 |
| 100 | 18.2.2018 Angular Stabilization of an Object Rapidly Rotating around Longitudial Axis | 104 | 1700 |
| 101 | 17.2.2018 Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine | 107 | 1218 |
| 102 | 16.2.2018 Design Solutions to Prevent Propellant Ingress into SRM Case Space behind Sealing Ring | 113 | 2038 |
| 103 | 15.2.2018 Topical Issues of Creation of Space Rocket Thermostatic System Mating Points | 112 | 1093 |
| 104 | 14.2.2018 A Concept of Modular Transport Vehicle for Lunar Program | 98 | 1239 |
| 105 | 13.2.2018 On an Approach to Constructing the Extremes in the Tasks of Optimal Solutions Search | 99 | 865 |
| 106 | 12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs | 110 | 1497 |
| 107 | 11.2.2018 Some Peculiarities of Ensuring LRE Guarantied Service Life in the Conditions of Replacement of Components of Interindustry Application | 94 | 1639 |
| 108 | 10.2.2018 Calculation of Gas Flow in High-Altitude Engine Nozzle and Experience of Using Water-Cooled Nozzle Head during Tests | 103 | 2396 |
| 109 | 9.2.2018 The Impact of Worm Design on Power and Anti-Cavitation Properties of Worm-Centrifugal Pumps | 113 | 2658 |
| 110 | 8.2.2018 Development of Nozzle Blocks New Manufacturing Technology without Blazing | 103 | 1940 |
| 111 | 7.2.2018 Theoretical Models of Sound Speed Increase Effects in Gas Duct with Corrugated Wall | 112 | 2329 |
| 112 | 6.2.2018 Introduction of Additive Technologies for LRE Parts Manufacturing | 104 | 1674 |
| 113 | 5.2.2018 Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office | 117 | 2589 |
| 114 | 4.2.2018 Turbopump Units of Rocket Engines Developed by DO-4 | 123 | 936 |
| 115 | 3.2.2018 Possible Ways of Modernization of VEGA Launch Vehicle AVUM Stage Main Engine Assembly | 114 | 2383 |
| 116 | 2.2.2018 Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines | 139 | 900 |
| 117 | 1.2.2018 Design Office of Liquid Rocket Engines is 60 | 112 | 605 |
| 118 | 16.1.2018 Some Correlation Dependences in Families of Aton and Apollo and Rendezvous Frequency in Main Asteroid Belt | 100 | 849 |
| 119 | 15.1.2018 The Results of Using Automated Methods to Solve Standardization Tasks in Yuzhnoye SDO Practice | 111 | 1655 |
| 120 | 14.1.2018 A Rectangular Section Pipes Winding Programs Calculation Procedure | 106 | 1277 |
| 121 | 13.1.2018 On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses | 114 | 1512 |
| 122 | 12.1.2018 A Device for Soft Separation of Spacecraft from Launch Vehicle | 114 | 1638 |
| 123 | 11.1.2018 Ensuring Long Lifetime of the Electrochemical Accumulators Included in Space Rocketry Electric Power Supply Systems | 115 | 1678 |
| 124 | 10.1.2018 The Rocket Propellant Vapors and Water Solutions Neutralization Units. The Accumulated Experience and Prospects of Updating the Neutralization Units | 126 | 1093 |
| 125 | 9.1.2018 On the Peculiarities of High-Temperature Rocket Propellants Drain from Delivery Means to Filling Tank for Closed Drain | 113 | 1560 |
| 126 | 8.1.2018 The Solid–Propellant Motors with Regulated Thrust | 131 | 1732 |
| 127 | 7.1.2018 Prospective Gas Purification Device for LRE Test Bench | 107 | 987 |
| 128 | 6.1.2018 On Building of Inertial Navigation System in the Condition of Presence of Considerable g-Load and Angular Velocity in Preferential Direction | 114 | 1379 |
| 129 | 5.1.2018 Experimental Determination of Lateral Force Caused by SRM Thrust Vector Eccentricity and Skew | 112 | 2124 |
| 130 | 4.1.2018 Determination of Angular Acceleration of Rotary Elements of Rocket Systems during Ground Tests | 103 | 954 |
| 131 | 3.1.2018 The Means of Functional Suppression of Radio Electronic Facilities of Small-Size Unmanned Aerial Vehicles with Electromagnetic Radiation Focusing | 111 | 1652 |
| 132 | 2.1.2018 Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop | 106 | 1442 |
| 133 | 1.1.2018 Modernization and Automation of Temperature Calculation of Measurement Errors of Climatic Chambers for Accelerated Environmental Tests | 96 | 1611 |
| 134 | 27.2.2017 Solution of “Unsolvable” Problems | 103 | 687 |
| 135 | 26.2.2017 State of the Art and Prospects for Nuclear-Quadrupole Resonance Thermometry in Ukraine | 117 | 2193 |
| 136 | 25.2.2017 Vacuum Conditions Simulation Criteria | 116 | 968 |
| 137 | 24.2.2017 Method of Supercooled Cryogenic Liquid Production | 120 | 629 |
| 138 | 23.2.2017 Optimization Technique for Mass of Locally Loaded Rocket Bays with Wafer Structure | 111 | 1888 |
| 139 | 22.2.2017 Advanced Aluminum Alloys for Launch Vehicle Pipeline Parts Manufacture | 104 | 1151 |
| 140 | 21.2.2017 Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft | 106 | 891 |
| 141 | 20.2.2017 Research Support for Development of Launch Vehicle Payload Unit Composite Load-Bearing Compartments | 114 | 2220 |
| 142 | 19.2.2017 Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation | 109 | 646 |
| 143 | 18.2.2017 Development Test of Payload Fairing Separation Dynamics under Ground Conditions | 114 | 731 |
| 144 | 17.2.2017 Development Test of Spacecraft Separation Dynamics under Ground Conditions | 113 | 860 |
| 145 | 16.2.2017 Determination of Spherical Flange Connections Gasket Clamping Site Width | 108 | 485 |
| 146 | 15.2.2017 Oxidizer Feedline Structural Optimization Results | 112 | 1342 |
| 147 | 14.2.2017 Development Test of Isolating Valve Operation under Cryogenic Conditions | 105 | 713 |
| 148 | 13.2.2017 Experience in Development of Isolating Fuel Valve with Pneumatic Drive and Hydraulic Brake for Operation under Cryogenic Conditions | 104 | 1605 |
| 149 | 12.2.2017 Determination Procedure for Pneudraulic System and Its Components No-Failure Operation Probability | 104 | 897 |
| 150 | 11.2.2017 Remote Monitoring Method of Pneudraulic System Structural Elements Integrity | 107 | 1238 |
| 151 | 10.2.2017 Analysis Method of Hydraulic Parameters of Circular Intake Device in Limit Operating Modes | 99 | 2020 |
| 152 | 9.2.2017 Peculiarities of Development of Cryogenic Propulsion System Circulating Cooling System | 108 | 1165 |
| 153 | 8.2.2017 Analysis Method of Nitrogen Tetroxide Tanks Generating Pressurization Systems | 101 | 518 |
| 154 | 7.2.2017 Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants | 112 | 1091 |
| 155 | 6.2.2017 Set of Actions on Enhancement of Launch Vehicle Payload Capability | 116 | 1043 |
| 156 | 5.2.2017 Structural Perfection of Cyclone-4 Integrated Launch Vehicle | 102 | 642 |
| 157 | 4.2.2017 Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics | 109 | 463 |
| 158 | 3.2.2017 Creation of Advanced Facilities for Spacecraft / Launch Vehicle Integration | 111 | 487 |
| 159 | 2.2.2017 Creation of Universal System of Launch Vehicle Space Head Modules for Cluster Spacecraft Missions | 118 | 1024 |
| 160 | 1.2.2017 DO-2 – Semicentenary | 98 | 481 |
| 161 | 17.1.2017 Peculiarities of Design and Development Test of Dispenser Turning Actuator System for SHM with Iridium NEXT SC | 102 | 1396 |
| 162 | 16.1.2017 Principal Directions for Creation of Integrated Launch Vehicle Autonomous Onboard Flight Safety System | 103 | 1826 |
| 163 | 15.1.2017 Assessment of Liquid Equipment Neutralization Method Effectiveness | 101 | 779 |
| 164 | 14.1.2017 Design Studies into Dynamic and Structural Characteristics of Two-Stage Direct-Action Solenoid-Operated Hydraulic Valve | 101 | 898 |
| 165 | 13.1.2017 Reliability Evaluation of ILV Thermostating System Mating Hoses | 109 | 1614 |
| 166 | 12.1.2017 Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator | 102 | 1441 |
| 167 | 11.1.2017 Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors | 109 | 753 |
| 168 | 10.1.2017 Features of Measurement System for Gas-Dynamic Model Tests of Rocket Complex Elements | 107 | 978 |
| 169 | 9.1.2017 Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles | 96 | 1242 |
| 170 | 8.1.2017 Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions | 104 | 845 |
| 171 | 7.1.2017 Static Approach Application in Analysis of Gas-Dynamic Parameters in Launch Vehicle Vented Bays | 95 | 770 |
| 172 | 6.1.2017 Drought Post-Effects Satellite Monitoring | 101 | 1732 |
| 173 | 5.1.2017 Development of Working Liquid Discontinuity Measurement Procedure and Its Certification | 96 | 928 |
| 174 | 4.1.2017 Basic Selection Criteria of Heat-Resistant and Thermal Protective Structures for High-Altitude Hypersonic Flying Vehicle | 104 | 1175 |
| 175 | 3.1.2017 Development Strength Test of Modified Antares ILV | 106 | 825 |
| 176 | 2.1.2017 Ultimate Stability Stresses in Smooth Cylindrical Skins. Dynamic Problem | 94 | 723 |
| 177 | 1.1.2017 Methodology for Measurement Uncertainty Evaluation during Metrological Certification of Measuring Instruments | 103 | 747 |
| 178 | 16.2.2016 Method of Coefficient for Optimization and Analysis of Operating State of Fine Filter Cases | 102 | 771 |
| 179 | 15.2.2016 A New Method of Testing Oil-Filled Current Transformers for Explosion-Proofness | 102 | 1093 |
| 180 | 14.2.2016 Investigation of Deformability of Carbon Plastic Panels in Moisture Absorption Process | 101 | 2089 |
| 181 | 13.2.2016 Experience of Developing Thermometric Instruments Based on Nuclear Quadrupole Resonance | 107 | 614 |
| 182 | 12.2.2016 The Use of Thermoelectric Technologies in Spacecraft Thermostatic Systems | 104 | 1006 |
| 183 | 11.2.2016 Experimental Investigation into Power Characteristics of Fast-Flowrate Gas Jet Propulsion Systems | 99 | 573 |
| 184 | 10.2.2016 Mathematical Model of High-Flowrate Electropneumatic Valve | 110 | 690 |
| 185 | 9.2.2016 Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands | 122 | 842 |
| 186 | 8.2.2016 Development and Validation of Program Module for Construction of Virtual Models of Real Structures in ANSYS System | 96 | 526 |
| 187 | 7.2.2016 Analysis of Operation Modes and Selection of Chemical Current Source Included in Autonomous Electric Power Supply Systems of Self-Propelled Launcher | 102 | 713 |
| 188 | 6.2.2016 Experimental Investigations into Results of Testing Cyclone-4 ILV Thermostating System Mating Points | 105 | 459 |
| 189 | 5.2.2016 Creation of Technological Tooling and Testing of Cocoon-Type Cases Manufacturing Technology | 107 | 1097 |
| 190 | 4.2.2016 Experimental Investigations of Possibility of Creating Impulse SRM with Short Operation Period | 104 | 1348 |
| 191 | 3.2.2016 Selection of Optimal Trajectories of Spacecraft Launch Vehicles | 104 | 872 |
| 192 | 2.2.2016 Normalization of Technical System Reliability Using Information Approach | 98 | 402 |
| 193 | 1.2.2016 On Minimal Aerodynamic Resistance of Rotation Body at Zero Angle of Attack in Hypersonic Non-Viscous Flow | 109 | 446 |
| 194 | 21.1.2016 Selection of Optimal Parameters of Wind Desalting System with Hydrogen Energy Storage Unit | 89 | 646 |
| 195 | 20.1.2016 Determination of External Characteristic of Autonomous WPP for Regulation by Rotor Withdrawal from under Wind | 103 | 616 |
| 196 | 19.1.2016 Blade Geometry for Maximal Power Coefficient and Minimal Noise Level | 96 | 369 |
| 197 | 18.1.2016 Method of Design Evaluation of SRM Lifetime and Ensuring its Long-Term Operation | 101 | 664 |
| 198 | 17.1.2016 Modeling of Solid Rocket Motor Starting Process | 98 | 1477 |
| 199 | 16.1.2016 Peculiarities of Development of SRM Thrust Vector Controls at DO-5 | 83 | 619 |
| 200 | 15.1.2016 Calculation of Solid Propellant Grain Burning Surface Using Automated 3D-Modeling Systems | 96 | 987 |
| 201 | 14.1.2016 Development of Powder Pressure Accumulators for Rocket Cold Start – the Most Important Condition of its Successful Realization | 105 | 561 |
| 202 | 13.1.2016 The Impact of Diaphragm’s Shape on Gas Dynamic Flow Characteristics in Small-Size SRM Combustion Chamber | 89 | 675 |
| 203 | 12.1.2016 Increasing Effectiveness of Meteorological Rockets when Using Hybrid Motors | 100 | 509 |
| 204 | 11.1.2016 Methodology of Design Evaluation of Main SRM Flowrate-Thrust Characteristics after Stage Separation | 101 | 602 |
| 205 | 10.1.2016 Development of Winding Pattern during Calculation of Composite Case Winding Programs | 100 | 737 |
| 206 | 9.1.2016 Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method | 100 | 443 |
| 207 | 8.1.2016 Assessment of Validity of Hypothesis of Constancy of Specific Vacuum Thrust Pulse during SRM Designing and Testing | 94 | 685 |
| 208 | 7.1.2016 Updated Design of SRM Test Rig | 96 | 680 |
| 209 | 6.1.2016 Ensuring Solid Rocket Motor Moisture Resistance by Design | 90 | 1260 |
| 210 | 5.1.2016 Scientific-Technical Base for Creation of Detonation Solid Rocket Motors | 89 | 856 |
| 211 | 4.1.2016 The Company’s Experience in Designing and Operating Special Bench Equipment for SRM Ground Tests | 86 | 433 |
| 212 | 3.1.2016 On Peculiarities of Life Testing and Safe Storage of Solid Rocket Motors | 97 | 1291 |
| 213 | 2.1.2016 Experience of Testing SRM Thrust Vector Controls | 97 | 870 |
| 214 | 1.1.2016 Solid Rocket Motors Developed by DO-5 | 119 | 536 |
