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1 | 1.1.2016 Solid Rocket Motors Developed by DO-5 | 91 | 392 |
2 | 2.1.2016 Experience of Testing SRM Thrust Vector Controls | 73 | 725 |
3 | 3.1.2016 On Peculiarities of Life Testing and Safe Storage of Solid Rocket Motors | 74 | 1047 |
4 | 4.1.2016 The Company’s Experience in Designing and Operating Special Bench Equipment for SRM Ground Tests | 63 | 349 |
5 | 5.1.2016 Scientific-Technical Base for Creation of Detonation Solid Rocket Motors | 64 | 688 |
6 | 6.1.2016 Ensuring Solid Rocket Motor Moisture Resistance by Design | 63 | 1076 |
7 | 7.1.2016 Updated Design of SRM Test Rig | 68 | 564 |
8 | 8.1.2016 Assessment of Validity of Hypothesis of Constancy of Specific Vacuum Thrust Pulse during SRM Designing and Testing | 70 | 557 |
9 | 9.1.2016 Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method | 76 | 352 |
10 | 10.1.2016 Development of Winding Pattern during Calculation of Composite Case Winding Programs | 70 | 617 |
11 | 11.1.2016 Methodology of Design Evaluation of Main SRM Flowrate-Thrust Characteristics after Stage Separation | 71 | 443 |
12 | 12.1.2016 Increasing Effectiveness of Meteorological Rockets when Using Hybrid Motors | 75 | 403 |
13 | 13.1.2016 The Impact of Diaphragm’s Shape on Gas Dynamic Flow Characteristics in Small-Size SRM Combustion Chamber | 64 | 548 |
14 | 14.1.2016 Development of Powder Pressure Accumulators for Rocket Cold Start – the Most Important Condition of its Successful Realization | 76 | 445 |
15 | 15.1.2016 Calculation of Solid Propellant Grain Burning Surface Using Automated 3D-Modeling Systems | 68 | 795 |
16 | 16.1.2016 Peculiarities of Development of SRM Thrust Vector Controls at DO-5 | 59 | 506 |
17 | 17.1.2016 Modeling of Solid Rocket Motor Starting Process | 68 | 1245 |
18 | 18.1.2016 Method of Design Evaluation of SRM Lifetime and Ensuring its Long-Term Operation | 76 | 523 |
19 | 19.1.2016 Blade Geometry for Maximal Power Coefficient and Minimal Noise Level | 69 | 278 |
20 | 20.1.2016 Determination of External Characteristic of Autonomous WPP for Regulation by Rotor Withdrawal from under Wind | 69 | 494 |
21 | 21.1.2016 Selection of Optimal Parameters of Wind Desalting System with Hydrogen Energy Storage Unit | 68 | 538 |
22 | 1.2.2016 On Minimal Aerodynamic Resistance of Rotation Body at Zero Angle of Attack in Hypersonic Non-Viscous Flow | 78 | 357 |
23 | 2.2.2016 Normalization of Technical System Reliability Using Information Approach | 68 | 316 |
24 | 3.2.2016 Selection of Optimal Trajectories of Spacecraft Launch Vehicles | 70 | 713 |
25 | 4.2.2016 Experimental Investigations of Possibility of Creating Impulse SRM with Short Operation Period | 73 | 1123 |
26 | 5.2.2016 Creation of Technological Tooling and Testing of Cocoon-Type Cases Manufacturing Technology | 78 | 907 |
27 | 6.2.2016 Experimental Investigations into Results of Testing Cyclone-4 ILV Thermostating System Mating Points | 73 | 389 |
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 | 67 | 599 |
29 | 8.2.2016 Development and Validation of Program Module for Construction of Virtual Models of Real Structures in ANSYS System | 66 | 406 |
30 | 9.2.2016 Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands | 78 | 674 |
31 | 10.2.2016 Mathematical Model of High-Flowrate Electropneumatic Valve | 77 | 574 |
32 | 11.2.2016 Experimental Investigation into Power Characteristics of Fast-Flowrate Gas Jet Propulsion Systems | 72 | 486 |
33 | 12.2.2016 The Use of Thermoelectric Technologies in Spacecraft Thermostatic Systems | 73 | 848 |
34 | 13.2.2016 Experience of Developing Thermometric Instruments Based on Nuclear Quadrupole Resonance | 75 | 526 |
35 | 14.2.2016 Investigation of Deformability of Carbon Plastic Panels in Moisture Absorption Process | 68 | 1733 |
36 | 15.2.2016 A New Method of Testing Oil-Filled Current Transformers for Explosion-Proofness | 74 | 919 |
37 | 16.2.2016 Method of Coefficient for Optimization and Analysis of Operating State of Fine Filter Cases | 69 | 624 |
38 | 1.1.2017 Methodology for Measurement Uncertainty Evaluation during Metrological Certification of Measuring Instruments | 80 | 615 |
39 | 2.1.2017 Ultimate Stability Stresses in Smooth Cylindrical Skins. Dynamic Problem | 67 | 586 |
40 | 3.1.2017 Development Strength Test of Modified Antares ILV | 74 | 648 |
41 | 4.1.2017 Basic Selection Criteria of Heat-Resistant and Thermal Protective Structures for High-Altitude Hypersonic Flying Vehicle | 78 | 956 |
42 | 5.1.2017 Development of Working Liquid Discontinuity Measurement Procedure and Its Certification | 70 | 755 |
43 | 6.1.2017 Drought Post-Effects Satellite Monitoring | 77 | 1279 |
44 | 7.1.2017 Static Approach Application in Analysis of Gas-Dynamic Parameters in Launch Vehicle Vented Bays | 71 | 633 |
45 | 8.1.2017 Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions | 78 | 652 |
46 | 9.1.2017 Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles | 69 | 972 |
47 | 10.1.2017 Features of Measurement System for Gas-Dynamic Model Tests of Rocket Complex Elements | 73 | 792 |
48 | 11.1.2017 Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors | 81 | 594 |
49 | 12.1.2017 Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator | 75 | 1177 |
50 | 13.1.2017 Reliability Evaluation of ILV Thermostating System Mating Hoses | 79 | 1348 |
51 | 14.1.2017 Design Studies into Dynamic and Structural Characteristics of Two-Stage Direct-Action Solenoid-Operated Hydraulic Valve | 74 | 737 |
52 | 15.1.2017 Assessment of Liquid Equipment Neutralization Method Effectiveness | 80 | 527 |
53 | 16.1.2017 Principal Directions for Creation of Integrated Launch Vehicle Autonomous Onboard Flight Safety System | 73 | 1474 |
54 | 17.1.2017 Peculiarities of Design and Development Test of Dispenser Turning Actuator System for SHM with Iridium NEXT SC | 73 | 1159 |
55 | 1.2.2017 DO-2 – Semicentenary | 70 | 387 |
56 | 2.2.2017 Creation of Universal System of Launch Vehicle Space Head Modules for Cluster Spacecraft Missions | 86 | 831 |
57 | 3.2.2017 Creation of Advanced Facilities for Spacecraft / Launch Vehicle Integration | 73 | 378 |
58 | 4.2.2017 Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics | 79 | 381 |
59 | 5.2.2017 Structural Perfection of Cyclone-4 Integrated Launch Vehicle | 71 | 508 |
60 | 6.2.2017 Set of Actions on Enhancement of Launch Vehicle Payload Capability | 84 | 842 |
61 | 7.2.2017 Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants | 76 | 850 |
62 | 8.2.2017 Analysis Method of Nitrogen Tetroxide Tanks Generating Pressurization Systems | 71 | 430 |
63 | 9.2.2017 Peculiarities of Development of Cryogenic Propulsion System Circulating Cooling System | 67 | 936 |
64 | 10.2.2017 Analysis Method of Hydraulic Parameters of Circular Intake Device in Limit Operating Modes | 70 | 1644 |
65 | 11.2.2017 Remote Monitoring Method of Pneudraulic System Structural Elements Integrity | 74 | 967 |
66 | 12.2.2017 Determination Procedure for Pneudraulic System and Its Components No-Failure Operation Probability | 81 | 734 |
67 | 13.2.2017 Experience in Development of Isolating Fuel Valve with Pneumatic Drive and Hydraulic Brake for Operation under Cryogenic Conditions | 76 | 1309 |
68 | 14.2.2017 Development Test of Isolating Valve Operation under Cryogenic Conditions | 75 | 565 |
69 | 15.2.2017 Oxidizer Feedline Structural Optimization Results | 75 | 1132 |
70 | 16.2.2017 Determination of Spherical Flange Connections Gasket Clamping Site Width | 79 | 386 |
71 | 17.2.2017 Development Test of Spacecraft Separation Dynamics under Ground Conditions | 81 | 718 |
72 | 18.2.2017 Development Test of Payload Fairing Separation Dynamics under Ground Conditions | 85 | 573 |
73 | 19.2.2017 Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation | 79 | 523 |
74 | 20.2.2017 Research Support for Development of Launch Vehicle Payload Unit Composite Load-Bearing Compartments | 83 | 1758 |
75 | 21.2.2017 Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft | 75 | 727 |
76 | 22.2.2017 Advanced Aluminum Alloys for Launch Vehicle Pipeline Parts Manufacture | 76 | 875 |
77 | 23.2.2017 Optimization Technique for Mass of Locally Loaded Rocket Bays with Wafer Structure | 74 | 1543 |
78 | 24.2.2017 Method of Supercooled Cryogenic Liquid Production | 90 | 502 |
79 | 25.2.2017 Vacuum Conditions Simulation Criteria | 83 | 803 |
80 | 26.2.2017 State of the Art and Prospects for Nuclear-Quadrupole Resonance Thermometry in Ukraine | 83 | 1781 |
81 | 27.2.2017 Solution of “Unsolvable” Problems | 70 | 537 |
82 | 1.1.2018 Modernization and Automation of Temperature Calculation of Measurement Errors of Climatic Chambers for Accelerated Environmental Tests | 65 | 1295 |
83 | 2.1.2018 Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop | 77 | 1152 |
84 | 3.1.2018 The Means of Functional Suppression of Radio Electronic Facilities of Small-Size Unmanned Aerial Vehicles with Electromagnetic Radiation Focusing | 77 | 1334 |
85 | 4.1.2018 Determination of Angular Acceleration of Rotary Elements of Rocket Systems during Ground Tests | 75 | 749 |
86 | 5.1.2018 Experimental Determination of Lateral Force Caused by SRM Thrust Vector Eccentricity and Skew | 85 | 1646 |
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 | 83 | 1140 |
88 | 7.1.2018 Prospective Gas Purification Device for LRE Test Bench | 78 | 824 |
89 | 8.1.2018 The Solid–Propellant Motors with Regulated Thrust | 92 | 1412 |
90 | 9.1.2018 On the Peculiarities of High-Temperature Rocket Propellants Drain from Delivery Means to Filling Tank for Closed Drain | 76 | 1283 |
91 | 10.1.2018 The Rocket Propellant Vapors and Water Solutions Neutralization Units. The Accumulated Experience and Prospects of Updating the Neutralization Units | 86 | 845 |
92 | 11.1.2018 Ensuring Long Lifetime of the Electrochemical Accumulators Included in Space Rocketry Electric Power Supply Systems | 83 | 1389 |
93 | 12.1.2018 A Device for Soft Separation of Spacecraft from Launch Vehicle | 82 | 1330 |
94 | 13.1.2018 On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses | 78 | 1221 |
95 | 14.1.2018 A Rectangular Section Pipes Winding Programs Calculation Procedure | 70 | 1032 |
96 | 15.1.2018 The Results of Using Automated Methods to Solve Standardization Tasks in Yuzhnoye SDO Practice | 78 | 1298 |
97 | 16.1.2018 Some Correlation Dependences in Families of Aton and Apollo and Rendezvous Frequency in Main Asteroid Belt | 74 | 656 |
98 | 1.2.2018 Design Office of Liquid Rocket Engines is 60 | 81 | 481 |
99 | 2.2.2018 Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines | 98 | 714 |
100 | 3.2.2018 Possible Ways of Modernization of VEGA Launch Vehicle AVUM Stage Main Engine Assembly | 82 | 1977 |
101 | 4.2.2018 Turbopump Units of Rocket Engines Developed by DO-4 | 86 | 732 |
102 | 5.2.2018 Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office | 79 | 2077 |
103 | 6.2.2018 Introduction of Additive Technologies for LRE Parts Manufacturing | 68 | 1337 |
104 | 7.2.2018 Theoretical Models of Sound Speed Increase Effects in Gas Duct with Corrugated Wall | 71 | 1864 |
105 | 8.2.2018 Development of Nozzle Blocks New Manufacturing Technology without Blazing | 65 | 1572 |
106 | 9.2.2018 The Impact of Worm Design on Power and Anti-Cavitation Properties of Worm-Centrifugal Pumps | 77 | 2192 |
107 | 10.2.2018 Calculation of Gas Flow in High-Altitude Engine Nozzle and Experience of Using Water-Cooled Nozzle Head during Tests | 77 | 1962 |
108 | 11.2.2018 Some Peculiarities of Ensuring LRE Guarantied Service Life in the Conditions of Replacement of Components of Interindustry Application | 68 | 1343 |
109 | 12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs | 80 | 1213 |
110 | 13.2.2018 On an Approach to Constructing the Extremes in the Tasks of Optimal Solutions Search | 62 | 699 |
111 | 14.2.2018 A Concept of Modular Transport Vehicle for Lunar Program | 74 | 993 |
112 | 15.2.2018 Topical Issues of Creation of Space Rocket Thermostatic System Mating Points | 74 | 912 |
113 | 16.2.2018 Design Solutions to Prevent Propellant Ingress into SRM Case Space behind Sealing Ring | 72 | 1698 |
114 | 17.2.2018 Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine | 81 | 984 |
115 | 18.2.2018 Angular Stabilization of an Object Rapidly Rotating around Longitudial Axis | 72 | 1386 |
116 | 19.2.2018 Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles | 77 | 1477 |
117 | 20.2.2018 The Use of Special Devices during Launch Pad Development Testing | 73 | 1221 |
118 | 21.2.2018 Ensuring Aiming Accuracy of Ship’s Telemetry Reception Antenna Installation for Small Vessels | 73 | 1500 |
119 | 22.2.2018 Uncertainty Calculation Procedure during Measuring Instrumentation Calibration | 75 | 2519 |
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 | 84 | 1804 |
121 | 1.1.2019 On 65-th anniversary of the company | 75 | 362 |
122 | 2.1.2019 Flying Vehicle Maneuvering Dynamics in Atmosphere with Weight Asymmetry and Elements of Terminal Control in Turn Leg | 84 | 815 |
123 | 3.1.2019 Analysis of Spacecraft Control Issues In Early Design Phases | 84 | 918 |
124 | 4.1.2019 Mathematic Modeling and Investigation into Stress-Strain State of Space Rocket Bays | 76 | 1356 |
125 | 5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime | 87 | 1190 |
126 | 6.1.2019 Investigation into Peculiarities of Delivery to Launch Base of Rocket Propellant with Specified Gasing | 73 | 1039 |
127 | 7.1.2019 Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on High-Temperature Propellants | 80 | 672 |
128 | 8.1.2019 Virtual Tests of Cassette Reentry Vehicle Dash Elements Attachment System during Ground Operation | 84 | 1526 |
129 | 9.1.2019 Modeling of Cyclone-4M Rocket Jet Acoustic Emission by Volumetric Source | 82 | 1275 |
130 | 10.1.2019 Semi-Empirical Evaluation of External Acoustic Loads in Payload Area during Lift-off | 75 | 1181 |
131 | 11.1.2019 Peculiarities of Development Testing of Space Rocket Thermostating System Mating Points Hoses | 77 | 580 |
132 | 12.1.2019 Monitoring of Launch Platform Drift Parameters during Zenit-3SL Integrated Launch Vehicle Prelauch Processing | 73 | 1166 |
133 | 13.1.2019 Prediction of Solid Propellant Burnout Time in Launch Vehicle Propulsion System in Flight | 80 | 1051 |
134 | 14.1.2019 Technique of Determination of SRM Operational Life Taking into Account Materials and Elements Strength Margins | 77 | 366 |
135 | 15.1.2019 Simulation of SMR Oscillations in Rig that Arise during Firing Bench Test | 75 | 1348 |
136 | 16.1.2019 Oscillation Processes in Rig at the Moment of SRM Transfer to Main Operation Mode | 73 | 855 |
137 | 17.1.2019 Development of Prospective Small-Size Auxiliary SMR of New Type | 74 | 1279 |
138 | 18.1.2019 Designing of Servo Driver of Throttle Mechanisms and Fuel Flow Regulator of ILV Main Motor | 72 | 977 |
139 | 19.1.2019 Peculiarities of Radio Transparent Fairings Development | 96 | 1101 |
140 | 20.1.2019 Possibilities of Increasing Acting Loads on Hydraulic Actuator Middle Position Lock | 76 | 819 |
141 | 21.1.2019 Optimization of Geometrical Shape of Isolation Valve Blading Position | 67 | 761 |
142 | 22.1.2019 Calculation of Uncertainty of Represented Values of Linear Accelerations during Centrifugal Machines Certification | 68 | 921 |
143 | 23.1.2019 Calculation of Thermal-Physical Properties of Gaseous Xenon | 69 | 1097 |
144 | 24.1.2019 Porous Cast Materials (Gasars). Options of Their Use in Space Rocket Hardware | 87 | 1364 |
145 | 25.1.2019 Technological Peculiarities of Manufacturing Products of Irregular Profile by Method of Selective Laser Melting of 316L Powder Metal Material | 67 | 1376 |
146 | 26.1.2019 New Technologies and Problems of Their Introducing in Ukraine | 76 | 1066 |
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 | 74 | 1154 |
148 | 1.2.2019 Optimization of the trajectory of the antiaircraft guided missile | 91 | 2768 |
149 | 2.2.2019 Mathematical models for assessment of safety in the impact area of cluster ammunition of the warhead during missile complex testing | 81 | 1822 |
150 | 3.2.2019 Features of design and production of the technological aids for assembly of the spacecraft separation system of CLAMP BAND type | 64 | 1337 |
151 | 4.2.2019 Numerical simulation of behavior of elastic structures with local stiffening elementse | 81 | 821 |
152 | 5.2.2019 Features of the development testing of the propellants deposition inside the tanks of launch vehicles | 80 | 971 |
153 | 6.2.2019 Stabilization of gas reducers adjustment | 86 | 1003 |
154 | 7.2.2019 On critical stress of the longitudinal stability of the stiffened cylindrical shells. Dynamic problem | 72 | 646 |
155 | 8.2.2019 Evaluation of the external acoustic loads, acting on the rocket when it passes the leg with maximum velocity head | 87 | 465 |
156 | 9.2.2019 Gas-dynamic simulation of the supersonic stream in the pulsed wind tunnel | 88 | 1628 |
157 | 10.2.2019 Dynamic performance of the gas drive with jet motor | 87 | 2895 |
158 | 11.2.2019 Winding the tubes of rectangular section using dowels | 77 | 937 |
159 | 12.2.2019 Procedure of acoustic loads measuring during the ILV launch | 73 | 854 |
160 | 13.2.2019 Study of the stress and strain state of the multilayer bellows | 75 | 1167 |
161 | 14.2.2019 Selection of the validation algorithm for the solid rocket motor trust measurement procedure | 86 | 1207 |
162 | 1.1.2020 Solving a problem of optimum curves of descent using the enhanced Euler equation | 75 | 2224 |
163 | 2.1.2020 Analysis of development trends of design parameters and basic characteristics of missiles for the advanced multiple launch rocket systems | 93 | 5380 |
164 | 3.1.2020 Analysis of the unsteady stress-strain behavior of the launch vehicle hold-down bay at liftoff | 94 | 2448 |
165 | 4.1.2020 Terminal guidance of the aircraft being maneuvering while descending in the atmosphere under conditions of aerodynamic balancing | 76 | 1122 |
166 | 5.1.2020 Strength and stability of inhomogeneous structures of space technology, consid-ering plasticity and creep | 86 | 3690 |
167 | 6.1.2020 Mechanics of a satellite cluster. Methods for estimating the probability of their maximal approach in flight | 76 | 1199 |
168 | 7.1.2020 Studying the motion of a launch vehicle and observed space debris objects during launch preparation | 77 | 1465 |
169 | 8.1.2020 Determining the main parameters of transport aircraft modifications considering the fuel efficiency | 80 | 855 |
170 | 9.1.2020 Experimental investigation of a liner-free propellant tank made from polymer composite materials | 86 | 2707 |
171 | 10.1.2020 Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM | 84 | 2091 |
172 | 11.1.2020 Some results of strength calculations relying on analytical and FEM approaches. Trends of using contemporary machine learning strategies | 87 | 1915 |
173 | 12.1.2020 Modification of technology as the main course in the military transport aircraft development | 87 | 1414 |
174 | 13.1.2020 Mathematical models of hydraulic servomechanisms of space technology | 72 | 1177 |
175 | 14.1.2020 On the problem of optimum control | 83 | 1523 |
176 | 15.1.2020 Simulation of thermomechanical processes in functionally-gradient materials of inhomogeneous structure in the manufacturing and operation of rocket structural elements | 87 | 2454 |
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 | 86 | 2518 |
178 | 17.1.2020 Acoustic problems of rocket launch | 78 | 1945 |
179 | 18.1.2020 Development of autonomous power engineering systems with hydrogen energy storage | 78 | 2355 |
180 | 19.1.2020 Pyrobolts: types, design, development. Shear type pyrobolt developed at Yuzhnoye SDO | 130 | 2543 |
181 | 20.1.2020 Studying the possibility of alternating delivery of rocket propellant wastes to a common thermal neutralization facility | 79 | 1494 |
182 | 21.1.2020 Contemporary approaches to the improvement of methods of space launch system operation for commercial launches of ILV | 72 | 1343 |
183 | 1.1.2023 On the development of a methodology for building air and missile defense systems. Explanation of the investigation mechanism | 46 | 1484 |
184 | 2.1.2023 How Yuzhnoye develops models for flight safety index evaluation for the case of a rocket failure during the flight | 43 | 1374 |
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 | 47 | 1749 |
186 | 4.1.2023 On control of spacecraft orientation to the ground data acquisition station | 37 | 649 |
187 | 5.1.2023 Fueling-neutralization stations. New developments and applications | 40 | 1204 |
188 | 6.1.2023 Numerical modeling of translational and rotational vibrations of a solid-propellant rocket motor on a test stand during firing tests | 38 | 1109 |
189 | 7.1.2023 Specificity of using rubbers as structural materials for making connector assemblies of temperature conditioning systems | 47 | 1121 |
190 | 8.1.2023 Specificity of developing pyrobolts with low impact and vibration impulse responses | 41 | 1253 |
191 | 9.1.2023 Methodology for selecting design parameters of solid-propellant sustainer engines. Mathematical support and software | 45 | 1929 |
192 | 1.1.2024 ANTARES: Yuzhnoye’s project of XXI century | 52 | 288 |
193 | 2.1.2024 New and advanced liquid rocket engines of the Yuzhnoye SDO | 73 | 1818 |
194 | 3.1.2024 Future projects of lunar exploration implemented by Yuzhnoye SDO | 70 | 1118 |
195 | 4.1.2024 The dynamics of servo drives | 60 | 1375 |
196 | 5.1.2024 Assessment of risk of toxic damage to people in case of a launch vehicle accident at flight | 87 | 1751 |
197 | 6.1.2024 New methods of load-carrying capacity prediction for the ultimately compressed frame structures | 68 | 1604 |
198 | 7.1.2024 Selection of the functional units for the Cyclone-4M ILV separation system | 75 | 2564 |
199 | 8.1.2024 Theoretic-experimental evaluation of the solid-propellant grain erosive burning | 67 | 986 |
200 | 9.1.2024 General-purpose thermostatting module – new approach in development of up-to-date thermostating systems for rocket and space complexes | 65 | 1668 |
201 | 10.1.2024 METHOD OF AUTONOMOUS DETERMINATION OF THE ROCKET’S REFERENCE ATTITUDE DURING PRE-LAUNCH PROCESSING | 75 | 1658 |
202 | 11.1.2024 PARAMETERS CALCULATION OF THE LUNAR REGOLITH TRANSPORT SYSTEM | 66 | 1534 |
203 | 12.1.2024 Hardening of steels modifying their surfaces with ion-plasma nitriding in glow discharge | 67 | 3036 |
204 | 13.1.2024 MODEL OF QUALITY MANAGEMENT OF TECHNICAL PREPARATION FOR THE METAL+COMPOSITE JOINTS PRODUCTION | 67 | 1297 |
205 | 14.1.2024 EXPERIMENTAL STUDIES OF THE PERFORMANCE OF PYROTECHNIC DEVICES INSTALLED ON THE LAUNCH VEHICLE SEPARATION SYSTEMS | 61 | 1868 |
206 | 15.1.2024 Enhancing operability of the fuel system units in the hot climate conditions | 61 | 2410 |
207 | 16.1.2024 EDUCATIONAL TENDENCIES AS AN ELEMENT OF INNOVATIVE PROGRESS IN THE PERSONNEL TRAINING SYSTEM FOR THE STATE-OF-THE-ART ENTERPRISES | 70 | 1043 |