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| 1 | 1.1.2016 Solid Rocket Motors Developed by DO-5 | 78 | 327 |
| 2 | 2.1.2016 Experience of Testing SRM Thrust Vector Controls | 58 | 632 |
| 3 | 3.1.2016 On Peculiarities of Life Testing and Safe Storage of Solid Rocket Motors | 58 | 872 |
| 4 | 4.1.2016 The Company’s Experience in Designing and Operating Special Bench Equipment for SRM Ground Tests | 52 | 287 |
| 5 | 5.1.2016 Scientific-Technical Base for Creation of Detonation Solid Rocket Motors | 51 | 574 |
| 6 | 6.1.2016 Ensuring Solid Rocket Motor Moisture Resistance by Design | 50 | 916 |
| 7 | 7.1.2016 Updated Design of SRM Test Rig | 54 | 469 |
| 8 | 8.1.2016 Assessment of Validity of Hypothesis of Constancy of Specific Vacuum Thrust Pulse during SRM Designing and Testing | 57 | 451 |
| 9 | 9.1.2016 Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method | 61 | 311 |
| 10 | 10.1.2016 Development of Winding Pattern during Calculation of Composite Case Winding Programs | 52 | 530 |
| 11 | 11.1.2016 Methodology of Design Evaluation of Main SRM Flowrate-Thrust Characteristics after Stage Separation | 54 | 374 |
| 12 | 12.1.2016 Increasing Effectiveness of Meteorological Rockets when Using Hybrid Motors | 60 | 332 |
| 13 | 13.1.2016 The Impact of Diaphragm’s Shape on Gas Dynamic Flow Characteristics in Small-Size SRM Combustion Chamber | 51 | 467 |
| 14 | 14.1.2016 Development of Powder Pressure Accumulators for Rocket Cold Start – the Most Important Condition of its Successful Realization | 63 | 353 |
| 15 | 15.1.2016 Calculation of Solid Propellant Grain Burning Surface Using Automated 3D-Modeling Systems | 54 | 654 |
| 16 | 16.1.2016 Peculiarities of Development of SRM Thrust Vector Controls at DO-5 | 48 | 435 |
| 17 | 17.1.2016 Modeling of Solid Rocket Motor Starting Process | 52 | 1058 |
| 18 | 18.1.2016 Method of Design Evaluation of SRM Lifetime and Ensuring its Long-Term Operation | 62 | 419 |
| 19 | 19.1.2016 Blade Geometry for Maximal Power Coefficient and Minimal Noise Level | 54 | 227 |
| 20 | 20.1.2016 Determination of External Characteristic of Autonomous WPP for Regulation by Rotor Withdrawal from under Wind | 57 | 413 |
| 21 | 21.1.2016 Selection of Optimal Parameters of Wind Desalting System with Hydrogen Energy Storage Unit | 55 | 448 |
| 22 | 1.2.2016 On Minimal Aerodynamic Resistance of Rotation Body at Zero Angle of Attack in Hypersonic Non-Viscous Flow | 63 | 318 |
| 23 | 2.2.2016 Normalization of Technical System Reliability Using Information Approach | 56 | 286 |
| 24 | 3.2.2016 Selection of Optimal Trajectories of Spacecraft Launch Vehicles | 57 | 616 |
| 25 | 4.2.2016 Experimental Investigations of Possibility of Creating Impulse SRM with Short Operation Period | 56 | 946 |
| 26 | 5.2.2016 Creation of Technological Tooling and Testing of Cocoon-Type Cases Manufacturing Technology | 60 | 758 |
| 27 | 6.2.2016 Experimental Investigations into Results of Testing Cyclone-4 ILV Thermostating System Mating Points | 58 | 356 |
| 28 | 7.2.2016 Analysis of Operation Modes and Selection of Chemical Current Source Included in Autonomous Electric Power Supply Systems of Self-Propelled Launcher | 55 | 512 |
| 29 | 8.2.2016 Development and Validation of Program Module for Construction of Virtual Models of Real Structures in ANSYS System | 54 | 350 |
| 30 | 9.2.2016 Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands | 62 | 577 |
| 31 | 10.2.2016 Mathematical Model of High-Flowrate Electropneumatic Valve | 62 | 482 |
| 32 | 11.2.2016 Experimental Investigation into Power Characteristics of Fast-Flowrate Gas Jet Propulsion Systems | 59 | 415 |
| 33 | 12.2.2016 The Use of Thermoelectric Technologies in Spacecraft Thermostatic Systems | 60 | 744 |
| 34 | 13.2.2016 Experience of Developing Thermometric Instruments Based on Nuclear Quadrupole Resonance | 59 | 492 |
| 35 | 14.2.2016 Investigation of Deformability of Carbon Plastic Panels in Moisture Absorption Process | 55 | 1416 |
| 36 | 15.2.2016 A New Method of Testing Oil-Filled Current Transformers for Explosion-Proofness | 59 | 784 |
| 37 | 16.2.2016 Method of Coefficient for Optimization and Analysis of Operating State of Fine Filter Cases | 56 | 531 |
| 38 | 1.1.2017 Methodology for Measurement Uncertainty Evaluation during Metrological Certification of Measuring Instruments | 67 | 533 |
| 39 | 2.1.2017 Ultimate Stability Stresses in Smooth Cylindrical Skins. Dynamic Problem | 57 | 495 |
| 40 | 3.1.2017 Development Strength Test of Modified Antares ILV | 60 | 545 |
| 41 | 4.1.2017 Basic Selection Criteria of Heat-Resistant and Thermal Protective Structures for High-Altitude Hypersonic Flying Vehicle | 62 | 819 |
| 42 | 5.1.2017 Development of Working Liquid Discontinuity Measurement Procedure and Its Certification | 55 | 645 |
| 43 | 6.1.2017 Drought Post-Effects Satellite Monitoring | 64 | 1092 |
| 44 | 7.1.2017 Static Approach Application in Analysis of Gas-Dynamic Parameters in Launch Vehicle Vented Bays | 56 | 510 |
| 45 | 8.1.2017 Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions | 64 | 550 |
| 46 | 9.1.2017 Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles | 58 | 824 |
| 47 | 10.1.2017 Features of Measurement System for Gas-Dynamic Model Tests of Rocket Complex Elements | 56 | 676 |
| 48 | 11.1.2017 Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors | 65 | 506 |
| 49 | 12.1.2017 Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator | 56 | 1005 |
| 50 | 13.1.2017 Reliability Evaluation of ILV Thermostating System Mating Hoses | 64 | 1169 |
| 51 | 14.1.2017 Design Studies into Dynamic and Structural Characteristics of Two-Stage Direct-Action Solenoid-Operated Hydraulic Valve | 56 | 630 |
| 52 | 15.1.2017 Assessment of Liquid Equipment Neutralization Method Effectiveness | 66 | 462 |
| 53 | 16.1.2017 Principal Directions for Creation of Integrated Launch Vehicle Autonomous Onboard Flight Safety System | 60 | 1228 |
| 54 | 17.1.2017 Peculiarities of Design and Development Test of Dispenser Turning Actuator System for SHM with Iridium NEXT SC | 55 | 976 |
| 55 | 1.2.2017 DO-2 – Semicentenary | 56 | 331 |
| 56 | 2.2.2017 Creation of Universal System of Launch Vehicle Space Head Modules for Cluster Spacecraft Missions | 71 | 718 |
| 57 | 3.2.2017 Creation of Advanced Facilities for Spacecraft / Launch Vehicle Integration | 59 | 320 |
| 58 | 4.2.2017 Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics | 62 | 324 |
| 59 | 5.2.2017 Structural Perfection of Cyclone-4 Integrated Launch Vehicle | 57 | 432 |
| 60 | 6.2.2017 Set of Actions on Enhancement of Launch Vehicle Payload Capability | 65 | 685 |
| 61 | 7.2.2017 Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants | 58 | 706 |
| 62 | 8.2.2017 Analysis Method of Nitrogen Tetroxide Tanks Generating Pressurization Systems | 53 | 371 |
| 63 | 9.2.2017 Peculiarities of Development of Cryogenic Propulsion System Circulating Cooling System | 51 | 785 |
| 64 | 10.2.2017 Analysis Method of Hydraulic Parameters of Circular Intake Device in Limit Operating Modes | 56 | 1298 |
| 65 | 11.2.2017 Remote Monitoring Method of Pneudraulic System Structural Elements Integrity | 59 | 769 |
| 66 | 12.2.2017 Determination Procedure for Pneudraulic System and Its Components No-Failure Operation Probability | 64 | 628 |
| 67 | 13.2.2017 Experience in Development of Isolating Fuel Valve with Pneumatic Drive and Hydraulic Brake for Operation under Cryogenic Conditions | 59 | 1104 |
| 68 | 14.2.2017 Development Test of Isolating Valve Operation under Cryogenic Conditions | 59 | 483 |
| 69 | 15.2.2017 Oxidizer Feedline Structural Optimization Results | 58 | 974 |
| 70 | 16.2.2017 Determination of Spherical Flange Connections Gasket Clamping Site Width | 58 | 336 |
| 71 | 17.2.2017 Development Test of Spacecraft Separation Dynamics under Ground Conditions | 66 | 627 |
| 72 | 18.2.2017 Development Test of Payload Fairing Separation Dynamics under Ground Conditions | 65 | 473 |
| 73 | 19.2.2017 Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation | 61 | 462 |
| 74 | 20.2.2017 Research Support for Development of Launch Vehicle Payload Unit Composite Load-Bearing Compartments | 64 | 1495 |
| 75 | 21.2.2017 Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft | 58 | 623 |
| 76 | 22.2.2017 Advanced Aluminum Alloys for Launch Vehicle Pipeline Parts Manufacture | 62 | 768 |
| 77 | 23.2.2017 Optimization Technique for Mass of Locally Loaded Rocket Bays with Wafer Structure | 56 | 1265 |
| 78 | 24.2.2017 Method of Supercooled Cryogenic Liquid Production | 72 | 413 |
| 79 | 25.2.2017 Vacuum Conditions Simulation Criteria | 64 | 702 |
| 80 | 26.2.2017 State of the Art and Prospects for Nuclear-Quadrupole Resonance Thermometry in Ukraine | 61 | 1489 |
| 81 | 27.2.2017 Solution of “Unsolvable” Problems | 54 | 438 |
| 82 | 1.1.2018 Modernization and Automation of Temperature Calculation of Measurement Errors of Climatic Chambers for Accelerated Environmental Tests | 54 | 1105 |
| 83 | 2.1.2018 Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop | 60 | 948 |
| 84 | 3.1.2018 The Means of Functional Suppression of Radio Electronic Facilities of Small-Size Unmanned Aerial Vehicles with Electromagnetic Radiation Focusing | 65 | 1127 |
| 85 | 4.1.2018 Determination of Angular Acceleration of Rotary Elements of Rocket Systems during Ground Tests | 60 | 623 |
| 86 | 5.1.2018 Experimental Determination of Lateral Force Caused by SRM Thrust Vector Eccentricity and Skew | 71 | 1399 |
| 87 | 6.1.2018 On Building of Inertial Navigation System in the Condition of Presence of Considerable g-Load and Angular Velocity in Preferential Direction | 66 | 961 |
| 88 | 7.1.2018 Prospective Gas Purification Device for LRE Test Bench | 62 | 723 |
| 89 | 8.1.2018 The Solid–Propellant Motors with Regulated Thrust | 68 | 1137 |
| 90 | 9.1.2018 On the Peculiarities of High-Temperature Rocket Propellants Drain from Delivery Means to Filling Tank for Closed Drain | 62 | 1079 |
| 91 | 10.1.2018 The Rocket Propellant Vapors and Water Solutions Neutralization Units. The Accumulated Experience and Prospects of Updating the Neutralization Units | 70 | 715 |
| 92 | 11.1.2018 Ensuring Long Lifetime of the Electrochemical Accumulators Included in Space Rocketry Electric Power Supply Systems | 66 | 1162 |
| 93 | 12.1.2018 A Device for Soft Separation of Spacecraft from Launch Vehicle | 64 | 1117 |
| 94 | 13.1.2018 On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses | 63 | 1031 |
| 95 | 14.1.2018 A Rectangular Section Pipes Winding Programs Calculation Procedure | 56 | 859 |
| 96 | 15.1.2018 The Results of Using Automated Methods to Solve Standardization Tasks in Yuzhnoye SDO Practice | 64 | 1057 |
| 97 | 16.1.2018 Some Correlation Dependences in Families of Aton and Apollo and Rendezvous Frequency in Main Asteroid Belt | 62 | 554 |
| 98 | 1.2.2018 Design Office of Liquid Rocket Engines is 60 | 68 | 394 |
| 99 | 2.2.2018 Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines | 80 | 595 |
| 100 | 3.2.2018 Possible Ways of Modernization of VEGA Launch Vehicle AVUM Stage Main Engine Assembly | 66 | 1702 |
| 101 | 4.2.2018 Turbopump Units of Rocket Engines Developed by DO-4 | 71 | 643 |
| 102 | 5.2.2018 Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office | 64 | 1754 |
| 103 | 6.2.2018 Introduction of Additive Technologies for LRE Parts Manufacturing | 51 | 1111 |
| 104 | 7.2.2018 Theoretical Models of Sound Speed Increase Effects in Gas Duct with Corrugated Wall | 57 | 1564 |
| 105 | 8.2.2018 Development of Nozzle Blocks New Manufacturing Technology without Blazing | 50 | 1297 |
| 106 | 9.2.2018 The Impact of Worm Design on Power and Anti-Cavitation Properties of Worm-Centrifugal Pumps | 62 | 1830 |
| 107 | 10.2.2018 Calculation of Gas Flow in High-Altitude Engine Nozzle and Experience of Using Water-Cooled Nozzle Head during Tests | 64 | 1651 |
| 108 | 11.2.2018 Some Peculiarities of Ensuring LRE Guarantied Service Life in the Conditions of Replacement of Components of Interindustry Application | 55 | 1142 |
| 109 | 12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs | 65 | 1006 |
| 110 | 13.2.2018 On an Approach to Constructing the Extremes in the Tasks of Optimal Solutions Search | 51 | 597 |
| 111 | 14.2.2018 A Concept of Modular Transport Vehicle for Lunar Program | 59 | 837 |
| 112 | 15.2.2018 Topical Issues of Creation of Space Rocket Thermostatic System Mating Points | 59 | 772 |
| 113 | 16.2.2018 Design Solutions to Prevent Propellant Ingress into SRM Case Space behind Sealing Ring | 61 | 1447 |
| 114 | 17.2.2018 Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine | 69 | 843 |
| 115 | 18.2.2018 Angular Stabilization of an Object Rapidly Rotating around Longitudial Axis | 61 | 1202 |
| 116 | 19.2.2018 Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles | 59 | 1254 |
| 117 | 20.2.2018 The Use of Special Devices during Launch Pad Development Testing | 59 | 1035 |
| 118 | 21.2.2018 Ensuring Aiming Accuracy of Ship’s Telemetry Reception Antenna Installation for Small Vessels | 58 | 1240 |
| 119 | 22.2.2018 Uncertainty Calculation Procedure during Measuring Instrumentation Calibration | 59 | 2093 |
| 120 | 23.2.2018 On the Role of Space in Origination of Inertia Force Field, Earth Gravity Force Field and Zero Gravity of Material Body | 59 | 1564 |
| 121 | 1.1.2019 On 65-th anniversary of the company | 61 | 306 |
| 122 | 2.1.2019 Flying Vehicle Maneuvering Dynamics in Atmosphere with Weight Asymmetry and Elements of Terminal Control in Turn Leg | 67 | 704 |
| 123 | 3.1.2019 Analysis of Spacecraft Control Issues In Early Design Phases | 70 | 769 |
| 124 | 4.1.2019 Mathematic Modeling and Investigation into Stress-Strain State of Space Rocket Bays | 62 | 1184 |
| 125 | 5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime | 72 | 974 |
| 126 | 6.1.2019 Investigation into Peculiarities of Delivery to Launch Base of Rocket Propellant with Specified Gasing | 57 | 866 |
| 127 | 7.1.2019 Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on High-Temperature Propellants | 62 | 586 |
| 128 | 8.1.2019 Virtual Tests of Cassette Reentry Vehicle Dash Elements Attachment System during Ground Operation | 69 | 1243 |
| 129 | 9.1.2019 Modeling of Cyclone-4M Rocket Jet Acoustic Emission by Volumetric Source | 67 | 1068 |
| 130 | 10.1.2019 Semi-Empirical Evaluation of External Acoustic Loads in Payload Area during Lift-off | 59 | 982 |
| 131 | 11.1.2019 Peculiarities of Development Testing of Space Rocket Thermostating System Mating Points Hoses | 64 | 477 |
| 132 | 12.1.2019 Monitoring of Launch Platform Drift Parameters during Zenit-3SL Integrated Launch Vehicle Prelauch Processing | 60 | 964 |
| 133 | 13.1.2019 Prediction of Solid Propellant Burnout Time in Launch Vehicle Propulsion System in Flight | 63 | 880 |
| 134 | 14.1.2019 Technique of Determination of SRM Operational Life Taking into Account Materials and Elements Strength Margins | 66 | 315 |
| 135 | 15.1.2019 Simulation of SMR Oscillations in Rig that Arise during Firing Bench Test | 58 | 1133 |
| 136 | 16.1.2019 Oscillation Processes in Rig at the Moment of SRM Transfer to Main Operation Mode | 60 | 740 |
| 137 | 17.1.2019 Development of Prospective Small-Size Auxiliary SMR of New Type | 58 | 1070 |
| 138 | 18.1.2019 Designing of Servo Driver of Throttle Mechanisms and Fuel Flow Regulator of ILV Main Motor | 57 | 819 |
| 139 | 19.1.2019 Peculiarities of Radio Transparent Fairings Development | 71 | 910 |
| 140 | 20.1.2019 Possibilities of Increasing Acting Loads on Hydraulic Actuator Middle Position Lock | 59 | 688 |
| 141 | 21.1.2019 Optimization of Geometrical Shape of Isolation Valve Blading Position | 53 | 643 |
| 142 | 22.1.2019 Calculation of Uncertainty of Represented Values of Linear Accelerations during Centrifugal Machines Certification | 55 | 793 |
| 143 | 23.1.2019 Calculation of Thermal-Physical Properties of Gaseous Xenon | 53 | 926 |
| 144 | 24.1.2019 Porous Cast Materials (Gasars). Options of Their Use in Space Rocket Hardware | 68 | 1126 |
| 145 | 25.1.2019 Technological Peculiarities of Manufacturing Products of Irregular Profile by Method of Selective Laser Melting of 316L Powder Metal Material | 50 | 1155 |
| 146 | 26.1.2019 New Technologies and Problems of Their Introducing in Ukraine | 62 | 886 |
| 147 | 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 | 51 | 977 |
| 148 | 1.2.2019 Optimization of the trajectory of the antiaircraft guided missile | 72 | 2323 |
| 149 | 2.2.2019 Mathematical models for assessment of safety in the impact area of cluster ammunition of the warhead during missile complex testing | 65 | 1510 |
| 150 | 3.2.2019 Features of design and production of the technological aids for assembly of the spacecraft separation system of CLAMP BAND type | 50 | 1116 |
| 151 | 4.2.2019 Numerical simulation of behavior of elastic structures with local stiffening elementse | 63 | 718 |
| 152 | 5.2.2019 Features of the development testing of the propellants deposition inside the tanks of launch vehicles | 66 | 826 |
| 153 | 6.2.2019 Stabilization of gas reducers adjustment | 68 | 853 |
| 154 | 7.2.2019 On critical stress of the longitudinal stability of the stiffened cylindrical shells. Dynamic problem | 59 | 549 |
| 155 | 8.2.2019 Evaluation of the external acoustic loads, acting on the rocket when it passes the leg with maximum velocity head | 61 | 405 |
| 156 | 9.2.2019 Gas-dynamic simulation of the supersonic stream in the pulsed wind tunnel | 72 | 1355 |
| 157 | 10.2.2019 Dynamic performance of the gas drive with jet motor | 67 | 2447 |
| 158 | 11.2.2019 Winding the tubes of rectangular section using dowels | 59 | 793 |
| 159 | 12.2.2019 Procedure of acoustic loads measuring during the ILV launch | 60 | 727 |
| 160 | 13.2.2019 Study of the stress and strain state of the multilayer bellows | 58 | 988 |
| 161 | 14.2.2019 Selection of the validation algorithm for the solid rocket motor trust measurement procedure | 67 | 1002 |
| 162 | 1.1.2020 Solving a problem of optimum curves of descent using the enhanced Euler equation | 61 | 1819 |
| 163 | 2.1.2020 Analysis of development trends of design parameters and basic characteristics of missiles for the advanced multiple launch rocket systems | 72 | 4414 |
| 164 | 3.1.2020 Analysis of the unsteady stress-strain behavior of the launch vehicle hold-down bay at liftoff | 76 | 2051 |
| 165 | 4.1.2020 Terminal guidance of the aircraft being maneuvering while descending in the atmosphere under conditions of aerodynamic balancing | 61 | 944 |
| 166 | 5.1.2020 Strength and stability of inhomogeneous structures of space technology, consid-ering plasticity and creep | 68 | 3080 |
| 167 | 6.1.2020 Mechanics of a satellite cluster. Methods for estimating the probability of their maximal approach in flight | 58 | 1020 |
| 168 | 7.1.2020 Studying the motion of a launch vehicle and observed space debris objects during launch preparation | 62 | 1231 |
| 169 | 8.1.2020 Determining the main parameters of transport aircraft modifications considering the fuel efficiency | 64 | 731 |
| 170 | 9.1.2020 Experimental investigation of a liner-free propellant tank made from polymer composite materials | 67 | 2285 |
| 171 | 10.1.2020 Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM | 65 | 1741 |
| 172 | 11.1.2020 Some results of strength calculations relying on analytical and FEM approaches. Trends of using contemporary machine learning strategies | 69 | 1596 |
| 173 | 12.1.2020 Modification of technology as the main course in the military transport aircraft development | 69 | 1206 |
| 174 | 13.1.2020 Mathematical models of hydraulic servomechanisms of space technology | 58 | 976 |
| 175 | 14.1.2020 On the problem of optimum control | 66 | 1275 |
| 176 | 15.1.2020 Simulation of thermomechanical processes in functionally-gradient materials of inhomogeneous structure in the manufacturing and operation of rocket structural elements | 68 | 2092 |
| 177 | 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 | 61 | 2094 |
| 178 | 17.1.2020 Acoustic problems of rocket launch | 62 | 1613 |
| 179 | 18.1.2020 Development of autonomous power engineering systems with hydrogen energy storage | 63 | 1971 |
| 180 | 19.1.2020 Pyrobolts: types, design, development. Shear type pyrobolt developed at Yuzhnoye SDO | 103 | 2182 |
| 181 | 20.1.2020 Studying the possibility of alternating delivery of rocket propellant wastes to a common thermal neutralization facility | 63 | 1243 |
| 182 | 21.1.2020 Contemporary approaches to the improvement of methods of space launch system operation for commercial launches of ILV | 59 | 1145 |
| 183 | 1.1.2023 On the development of a methodology for building air and missile defense systems. Explanation of the investigation mechanism | 29 | 1254 |
| 184 | 2.1.2023 How Yuzhnoye develops models for flight safety index evaluation for the case of a rocket failure during the flight | 27 | 1148 |
| 185 | 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 | 30 | 1466 |
| 186 | 4.1.2023 On control of spacecraft orientation to the ground data acquisition station | 23 | 542 |
| 187 | 5.1.2023 Fueling-neutralization stations. New developments and applications | 28 | 1030 |
| 188 | 6.1.2023 Numerical modeling of translational and rotational vibrations of a solid-propellant rocket motor on a test stand during firing tests | 24 | 970 |
| 189 | 7.1.2023 Specificity of using rubbers as structural materials for making connector assemblies of temperature conditioning systems | 30 | 950 |
| 190 | 8.1.2023 Specificity of developing pyrobolts with low impact and vibration impulse responses | 29 | 1054 |
| 191 | 9.1.2023 Methodology for selecting design parameters of solid-propellant sustainer engines. Mathematical support and software | 30 | 1636 |
| 192 | 1.1.2024 ANTARES: Yuzhnoye’s project of XXI century | 39 | 211 |
| 193 | 2.1.2024 New and advanced liquid rocket engines of the Yuzhnoye SDO | 53 | 1342 |
| 194 | 3.1.2024 Future projects of lunar exploration implemented by Yuzhnoye SDO | 45 | 869 |
| 195 | 4.1.2024 The dynamics of servo drives | 44 | 1032 |
| 196 | 5.1.2024 Assessment of risk of toxic damage to people in case of a launch vehicle accident at flight | 63 | 1334 |
| 197 | 6.1.2024 New methods of load-carrying capacity prediction for the ultimately compressed frame structures | 47 | 1201 |
| 198 | 7.1.2024 Selection of the functional units for the Cyclone-4M ILV separation system | 50 | 1888 |
| 199 | 8.1.2024 Theoretic-experimental evaluation of the solid-propellant grain erosive burning | 44 | 730 |
| 200 | 9.1.2024 General-purpose thermostatting module – new approach in development of up-to-date thermostating systems for rocket and space complexes | 45 | 1249 |
| 201 | 10.1.2024 METHOD OF AUTONOMOUS DETERMINATION OF THE ROCKET’S REFERENCE ATTITUDE DURING PRE-LAUNCH PROCESSING | 50 | 1234 |
| 202 | 11.1.2024 PARAMETERS CALCULATION OF THE LUNAR REGOLITH TRANSPORT SYSTEM | 41 | 1128 |
| 203 | 12.1.2024 Hardening of steels modifying their surfaces with ion-plasma nitriding in glow discharge | 48 | 2258 |
| 204 | 13.1.2024 MODEL OF QUALITY MANAGEMENT OF TECHNICAL PREPARATION FOR THE METAL+COMPOSITE JOINTS PRODUCTION | 51 | 968 |
| 205 | 14.1.2024 EXPERIMENTAL STUDIES OF THE PERFORMANCE OF PYROTECHNIC DEVICES INSTALLED ON THE LAUNCH VEHICLE SEPARATION SYSTEMS | 43 | 1429 |
| 206 | 15.1.2024 Enhancing operability of the fuel system units in the hot climate conditions | 43 | 1782 |
| 207 | 16.1.2024 EDUCATIONAL TENDENCIES AS AN ELEMENT OF INNOVATIVE PROGRESS IN THE PERSONNEL TRAINING SYSTEM FOR THE STATE-OF-THE-ART ENTERPRISES | 52 | 780 |
