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Article title Number of downloads Number of views
11.1.2016 Solid Rocket Motors Developed by DO-591392
22.1.2016 Experience of Testing SRM Thrust Vector Controls73725
33.1.2016 On Peculiarities of Life Testing and Safe Storage of Solid Rocket Motors741047
44.1.2016 The Company’s Experience in Designing and Operating Special Bench Equipment for SRM Ground Tests63349
55.1.2016 Scientific-Technical Base for Creation of Detonation Solid Rocket Motors64688
66.1.2016 Ensuring Solid Rocket Motor Moisture Resistance by Design631076
77.1.2016 Updated Design of SRM Test Rig68564
88.1.2016 Assessment of Validity of Hypothesis of Constancy of Specific Vacuum Thrust Pulse during SRM Designing and Testing70557
99.1.2016 Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method76352
1010.1.2016 Development of Winding Pattern during Calculation of Composite Case Winding Programs70617
1111.1.2016 Methodology of Design Evaluation of Main SRM Flowrate-Thrust Characteristics after Stage Separation71443
1212.1.2016 Increasing Effectiveness of Meteorological Rockets when Using Hybrid Motors75403
1313.1.2016 The Impact of Diaphragm’s Shape on Gas Dynamic Flow Characteristics in Small-Size SRM Combustion Chamber64548
1414.1.2016 Development of Powder Pressure Accumulators for Rocket Cold Start – the Most Important Condition of its Successful Realization76445
1515.1.2016 Calculation of Solid Propellant Grain Burning Surface Using Automated 3D-Modeling Systems68795
1616.1.2016 Peculiarities of Development of SRM Thrust Vector Controls at DO-559506
1717.1.2016 Modeling of Solid Rocket Motor Starting Process681245
1818.1.2016 Method of Design Evaluation of SRM Lifetime and Ensuring its Long-Term Operation76523
1919.1.2016 Blade Geometry for Maximal Power Coefficient and Minimal Noise Level69278
2020.1.2016 Determination of External Characteristic of Autonomous WPP for Regulation by Rotor Withdrawal from under Wind69494
2121.1.2016 Selection of Optimal Parameters of Wind Desalting System with Hydrogen Energy Storage Unit68538
221.2.2016 On Minimal Aerodynamic Resistance of Rotation Body at Zero Angle of Attack in Hypersonic Non-Viscous Flow78357
232.2.2016 Normalization of Technical System Reliability Using Information Approach68316
243.2.2016 Selection of Optimal Trajectories of Spacecraft Launch Vehicles70713
254.2.2016 Experimental Investigations of Possibility of Creating Impulse SRM with Short Operation Period731123
265.2.2016 Creation of Technological Tooling and Testing of Cocoon-Type Cases Manufacturing Technology78907
276.2.2016 Experimental Investigations into Results of Testing Cyclone-4 ILV Thermostating System Mating Points73389
287.2.2016 Analysis of Operation Modes and Selection of Chemical Current Source Included in Autonomous Electric Power Supply Systems of Self-Propelled Launcher67599
298.2.2016 Development and Validation of Program Module for Construction of Virtual Models of Real Structures in ANSYS System66406
309.2.2016 Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands78674
3110.2.2016 Mathematical Model of High-Flowrate Electropneumatic Valve77574
3211.2.2016 Experimental Investigation into Power Characteristics of Fast-Flowrate Gas Jet Propulsion Systems72486
3312.2.2016 The Use of Thermoelectric Technologies in Spacecraft Thermostatic Systems73848
3413.2.2016 Experience of Developing Thermometric Instruments Based on Nuclear Quadrupole Resonance75526
3514.2.2016 Investigation of Deformability of Carbon Plastic Panels in Moisture Absorption Process681733
3615.2.2016 A New Method of Testing Oil-Filled Current Transformers for Explosion-Proofness74919
3716.2.2016 Method of Coefficient for Optimization and Analysis of Operating State of Fine Filter Cases69624
381.1.2017 Methodology for Measurement Uncertainty Evaluation during Metrological Certification of Measuring Instruments80615
392.1.2017 Ultimate Stability Stresses in Smooth Cylindrical Skins. Dynamic Problem67586
403.1.2017 Development Strength Test of Modified Antares ILV74648
414.1.2017 Basic Selection Criteria of Heat-Resistant and Thermal Protective Structures for High-Altitude Hypersonic Flying Vehicle78956
425.1.2017 Development of Working Liquid Discontinuity Measurement Procedure and Its Certification70755
436.1.2017 Drought Post-Effects Satellite Monitoring771279
447.1.2017 Static Approach Application in Analysis of Gas-Dynamic Parameters in Launch Vehicle Vented Bays71633
458.1.2017 Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions78652
469.1.2017 Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles69972
4710.1.2017 Features of Measurement System for Gas-Dynamic Model Tests of Rocket Complex Elements73792
4811.1.2017 Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors81594
4912.1.2017 Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator751177
5013.1.2017 Reliability Evaluation of ILV Thermostating System Mating Hoses791348
5114.1.2017 Design Studies into Dynamic and Structural Characteristics of Two-Stage Direct-Action Solenoid-Operated Hydraulic Valve74737
5215.1.2017 Assessment of Liquid Equipment Neutralization Method Effectiveness80527
5316.1.2017 Principal Directions for Creation of Integrated Launch Vehicle Autonomous Onboard Flight Safety System731474
5417.1.2017 Peculiarities of Design and Development Test of Dispenser Turning Actuator System for SHM with Iridium NEXT SC731159
551.2.2017 DO-2 – Semicentenary70387
562.2.2017 Creation of Universal System of Launch Vehicle Space Head Modules for Cluster Spacecraft Missions86831
573.2.2017 Creation of Advanced Facilities for Spacecraft / Launch Vehicle Integration73378
584.2.2017 Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics79381
595.2.2017 Structural Perfection of Cyclone-4 Integrated Launch Vehicle71508
606.2.2017 Set of Actions on Enhancement of Launch Vehicle Payload Capability84842
617.2.2017 Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants76850
628.2.2017 Analysis Method of Nitrogen Tetroxide Tanks Generating Pressurization Systems71430
639.2.2017 Peculiarities of Development of Cryogenic Propulsion System Circulating Cooling System67936
6410.2.2017 Analysis Method of Hydraulic Parameters of Circular Intake Device in Limit Operating Modes701644
6511.2.2017 Remote Monitoring Method of Pneudraulic System Structural Elements Integrity74967
6612.2.2017 Determination Procedure for Pneudraulic System and Its Components No-Failure Operation Probability81734
6713.2.2017 Experience in Development of Isolating Fuel Valve with Pneumatic Drive and Hydraulic Brake for Operation under Cryogenic Conditions761309
6814.2.2017 Development Test of Isolating Valve Operation under Cryogenic Conditions75565
6915.2.2017 Oxidizer Feedline Structural Optimization Results751132
7016.2.2017 Determination of Spherical Flange Connections Gasket Clamping Site Width79386
7117.2.2017 Development Test of Spacecraft Separation Dynamics under Ground Conditions81718
7218.2.2017 Development Test of Payload Fairing Separation Dynamics under Ground Conditions85573
7319.2.2017 Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation79523
7420.2.2017 Research Support for Development of Launch Vehicle Payload Unit Composite Load-Bearing Compartments831758
7521.2.2017 Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft75727
7622.2.2017 Advanced Aluminum Alloys for Launch Vehicle Pipeline Parts Manufacture76875
7723.2.2017 Optimization Technique for Mass of Locally Loaded Rocket Bays with Wafer Structure741543
7824.2.2017 Method of Supercooled Cryogenic Liquid Production90502
7925.2.2017 Vacuum Conditions Simulation Criteria83803
8026.2.2017 State of the Art and Prospects for Nuclear-Quadrupole Resonance Thermometry in Ukraine831781
8127.2.2017 Solution of “Unsolvable” Problems70537
821.1.2018 Modernization and Automation of Temperature Calculation of Measurement Errors of Climatic Chambers for Accelerated Environmental Tests651295
832.1.2018 Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop771152
843.1.2018 The Means of Functional Suppression of Radio Electronic Facilities of Small-Size Unmanned Aerial Vehicles with Electromagnetic Radiation Focusing771334
854.1.2018 Determination of Angular Acceleration of Rotary Elements of Rocket Systems during Ground Tests75749
865.1.2018 Experimental Determination of Lateral Force Caused by SRM Thrust Vector Eccentricity and Skew851646
876.1.2018 On Building of Inertial Navigation System in the Condition of Presence of Considerable g-Load and Angular Velocity in Preferential Direction831140
887.1.2018 Prospective Gas Purification Device for LRE Test Bench78824
898.1.2018 The Solid–Propellant Motors with Regulated Thrust921412
909.1.2018 On the Peculiarities of High-Temperature Rocket Propellants Drain from Delivery Means to Filling Tank for Closed Drain761283
9110.1.2018 The Rocket Propellant Vapors and Water Solutions Neutralization Units. The Accumulated Experience and Prospects of Updating the Neutralization Units86845
9211.1.2018 Ensuring Long Lifetime of the Electrochemical Accumulators Included in Space Rocketry Electric Power Supply Systems831389
9312.1.2018 A Device for Soft Separation of Spacecraft from Launch Vehicle821330
9413.1.2018 On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses781221
9514.1.2018 A Rectangular Section Pipes Winding Programs Calculation Procedure701032
9615.1.2018 The Results of Using Automated Methods to Solve Standardization Tasks in Yuzhnoye SDO Practice781298
9716.1.2018 Some Correlation Dependences in Families of Aton and Apollo and Rendezvous Frequency in Main Asteroid Belt74656
981.2.2018 Design Office of Liquid Rocket Engines is 6081481
992.2.2018 Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines98714
1003.2.2018 Possible Ways of Modernization of VEGA Launch Vehicle AVUM Stage Main Engine Assembly821977
1014.2.2018 Turbopump Units of Rocket Engines Developed by DO-486732
1025.2.2018 Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office792077
1036.2.2018 Introduction of Additive Technologies for LRE Parts Manufacturing681337
1047.2.2018 Theoretical Models of Sound Speed Increase Effects in Gas Duct with Corrugated Wall711864
1058.2.2018 Development of Nozzle Blocks New Manufacturing Technology without Blazing651572
1069.2.2018 The Impact of Worm Design on Power and Anti-Cavitation Properties of Worm-Centrifugal Pumps772192
10710.2.2018 Calculation of Gas Flow in High-Altitude Engine Nozzle and Experience of Using Water-Cooled Nozzle Head during Tests771962
10811.2.2018 Some Peculiarities of Ensuring LRE Guarantied Service Life in the Conditions of Replacement of Components of Interindustry Application681343
10912.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs801213
11013.2.2018 On an Approach to Constructing the Extremes in the Tasks of Optimal Solutions Search62699
11114.2.2018 A Concept of Modular Transport Vehicle for Lunar Program74993
11215.2.2018 Topical Issues of Creation of Space Rocket Thermostatic System Mating Points74912
11316.2.2018 Design Solutions to Prevent Propellant Ingress into SRM Case Space behind Sealing Ring721698
11417.2.2018 Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine81984
11518.2.2018 Angular Stabilization of an Object Rapidly Rotating around Longitudial Axis721386
11619.2.2018 Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles771477
11720.2.2018 The Use of Special Devices during Launch Pad Development Testing731221
11821.2.2018 Ensuring Aiming Accuracy of Ship’s Telemetry Reception Antenna Installation for Small Vessels731500
11922.2.2018 Uncertainty Calculation Procedure during Measuring Instrumentation Calibration752519
12023.2.2018 On the Role of Space in Origination of Inertia Force Field, Earth Gravity Force Field and Zero Gravity of Material Body841804
1211.1.2019 On 65-th anniversary of the company75362
1222.1.2019 Flying Vehicle Maneuvering Dynamics in Atmosphere with Weight Asymmetry and Elements of Terminal Control in Turn Leg84815
1233.1.2019 Analysis of Spacecraft Control Issues In Early Design Phases84918
1244.1.2019 Mathematic Modeling and Investigation into Stress-Strain State of Space Rocket Bays761356
1255.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime871190
1266.1.2019 Investigation into Peculiarities of Delivery to Launch Base of Rocket Propellant with Specified Gasing731039
1277.1.2019 Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on High-Temperature Propellants80672
1288.1.2019 Virtual Tests of Cassette Reentry Vehicle Dash Elements Attachment System during Ground Operation841526
1299.1.2019 Modeling of Cyclone-4M Rocket Jet Acoustic Emission by Volumetric Source821275
13010.1.2019 Semi-Empirical Evaluation of External Acoustic Loads in Payload Area during Lift-off751181
13111.1.2019 Peculiarities of Development Testing of Space Rocket Thermostating System Mating Points Hoses77580
13212.1.2019 Monitoring of Launch Platform Drift Parameters during Zenit-3SL Integrated Launch Vehicle Prelauch Processing731166
13313.1.2019 Prediction of Solid Propellant Burnout Time in Launch Vehicle Propulsion System in Flight801051
13414.1.2019 Technique of Determination of SRM Operational Life Taking into Account Materials and Elements Strength Margins77366
13515.1.2019 Simulation of SMR Oscillations in Rig that Arise during Firing Bench Test751348
13616.1.2019 Oscillation Processes in Rig at the Moment of SRM Transfer to Main Operation Mode73855
13717.1.2019 Development of Prospective Small-Size Auxiliary SMR of New Type741279
13818.1.2019 Designing of Servo Driver of Throttle Mechanisms and Fuel Flow Regulator of ILV Main Motor72977
13919.1.2019 Peculiarities of Radio Transparent Fairings Development961101
14020.1.2019 Possibilities of Increasing Acting Loads on Hydraulic Actuator Middle Position Lock76819
14121.1.2019 Optimization of Geometrical Shape of Isolation Valve Blading Position67761
14222.1.2019 Calculation of Uncertainty of Represented Values of Linear Accelerations during Centrifugal Machines Certification68921
14323.1.2019 Calculation of Thermal-Physical Properties of Gaseous Xenon691097
14424.1.2019 Porous Cast Materials (Gasars). Options of Their Use in Space Rocket Hardware871364
14525.1.2019 Technological Peculiarities of Manufacturing Products of Irregular Profile by Method of Selective Laser Melting of 316L Powder Metal Material671376
14626.1.2019 New Technologies and Problems of Their Introducing in Ukraine761066
14727.1.2019 Phases of Cooperation of Yuzhnoye SDO and Dnipro National University Physical Engineering Department on the Issues of Mutual Human Resourcing: Past, Present. Future741154
1481.2.2019 Optimization of the trajectory of the antiaircraft guided missile912768
1492.2.2019 Mathematical models for assessment of safety in the impact area of cluster ammunition of the warhead during missile complex testing811822
1503.2.2019 Features of design and production of the technological aids for assembly of the spacecraft separation system of CLAMP BAND type641337
1514.2.2019 Numerical simulation of behavior of elastic structures with local stiffening elementse81821
1525.2.2019 Features of the development testing of the propellants deposition inside the tanks of launch vehicles80971
1536.2.2019 Stabilization of gas reducers adjustment861003
1547.2.2019 On critical stress of the longitudinal stability of the stiffened cylindrical shells. Dynamic problem72646
1558.2.2019 Evaluation of the external acoustic loads, acting on the rocket when it passes the leg with maximum velocity head87465
1569.2.2019 Gas-dynamic simulation of the supersonic stream in the pulsed wind tunnel881628
15710.2.2019 Dynamic performance of the gas drive with jet motor872895
15811.2.2019 Winding the tubes of rectangular section using dowels77937
15912.2.2019 Procedure of acoustic loads measuring during the ILV launch73854
16013.2.2019 Study of the stress and strain state of the multilayer bellows751167
16114.2.2019 Selection of the validation algorithm for the solid rocket motor trust measurement procedure861207
1621.1.2020 Solving a problem of optimum curves of descent using the enhanced Euler equation752224
1632.1.2020 Analysis of development trends of design parameters and basic characteristics of missiles for the advanced multiple launch rocket systems935380
1643.1.2020 Analysis of the unsteady stress-strain behavior of the launch vehicle hold-down bay at liftoff942448
1654.1.2020 Terminal guidance of the aircraft being maneuvering while descending in the atmosphere under conditions of aerodynamic balancing761122
1665.1.2020 Strength and stability of inhomogeneous structures of space technology, consid-ering plasticity and creep863690
1676.1.2020 Mechanics of a satellite cluster. Methods for estimating the probability of their maximal approach in flight761199
1687.1.2020 Studying the motion of a launch vehicle and observed space debris objects during launch preparation771465
1698.1.2020 Determining the main parameters of transport aircraft modifications considering the fuel efficiency80855
1709.1.2020 Experimental investigation of a liner-free propellant tank made from polymer composite materials862707
17110.1.2020 Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM842091
17211.1.2020 Some results of strength calculations relying on analytical and FEM approaches. Trends of using contemporary machine learning strategies871915
17312.1.2020 Modification of technology as the main course in the military transport aircraft development871414
17413.1.2020 Mathematical models of hydraulic servomechanisms of space technology721177
17514.1.2020 On the problem of optimum control831523
17615.1.2020 Simulation of thermomechanical processes in functionally-gradient materials of inhomogeneous structure in the manufacturing and operation of rocket structural elements872454
17716.1.2020 Parameters of the supersonic jet of a block propulsion system, flowing into a gas duct, considering chemical kinetics of gas-cycle transformations862518
17817.1.2020 Acoustic problems of rocket launch781945
17918.1.2020 Development of autonomous power engineering systems with hydrogen energy storage782355
18019.1.2020 Pyrobolts: types, design, development. Shear type pyrobolt developed at Yuzhnoye SDO1302543
18120.1.2020 Studying the possibility of alternating delivery of rocket propellant wastes to a common thermal neutralization facility791494
18221.1.2020 Contemporary approaches to the improvement of methods of space launch system operation for commercial launches of ILV721343
1831.1.2023 On the development of a methodology for building air and missile defense systems. Explanation of the investigation mechanism461484
1842.1.2023 How Yuzhnoye develops models for flight safety index evaluation for the case of a rocket failure during the flight431374
1853.1.2023 Analysis of a modernized 9K51 Hrad Multiple Rocket Launcher System to determine the performance specifications of the 122-mm unguided rocket projectile in development471749
1864.1.2023 On control of spacecraft orientation to the ground data acquisition station37649
1875.1.2023 Fueling-neutralization stations. New developments and applications401204
1886.1.2023 Numerical modeling of translational and rotational vibrations of a solid-propellant rocket motor on a test stand during firing tests381109
1897.1.2023 Specificity of using rubbers as structural materials for making connector assemblies of temperature conditioning systems471121
1908.1.2023 Specificity of developing pyrobolts with low impact and vibration impulse responses411253
1919.1.2023 Methodology for selecting design parameters of solid-propellant sustainer engines. Mathematical support and software451929
1921.1.2024 ANTARES: Yuzhnoye’s project of XXI century52288
1932.1.2024 New and advanced liquid rocket engines of the Yuzhnoye SDO731818
1943.1.2024 Future projects of lunar exploration implemented by Yuzhnoye SDO701118
1954.1.2024 The dynamics of servo drives601375
1965.1.2024 Assessment of risk of toxic damage to people in case of a launch vehicle accident at flight871751
1976.1.2024 New methods of load-carrying capacity prediction for the ultimately compressed frame structures681604
1987.1.2024 Selection of the functional units for the Cyclone-4M ILV separation system752564
1998.1.2024 Theoretic-experimental evaluation of the solid-propellant grain erosive burning67986
2009.1.2024 General-purpose thermostatting module – new approach in development of up-to-date thermostating systems for rocket and space complexes651668
20110.1.2024 METHOD OF AUTONOMOUS DETERMINATION OF THE ROCKET’S REFERENCE ATTITUDE DURING PRE-LAUNCH PROCESSING751658
20211.1.2024 PARAMETERS CALCULATION OF THE LUNAR REGOLITH TRANSPORT SYSTEM661534
20312.1.2024 Hardening of steels modifying their surfaces with ion-plasma nitriding in glow discharge673036
20413.1.2024 MODEL OF QUALITY MANAGEMENT OF TECHNICAL PREPARATION FOR THE METAL+COMPOSITE JOINTS PRODUCTION671297
20514.1.2024 EXPERIMENTAL STUDIES OF THE PERFORMANCE OF PYROTECHNIC DEVICES INSTALLED ON THE LAUNCH VEHICLE SEPARATION SYSTEMS611868
20615.1.2024 Enhancing operability of the fuel system units in the hot climate conditions612410
20716.1.2024 EDUCATIONAL TENDENCIES AS AN ELEMENT OF INNOVATIVE PROGRESS IN THE PERSONNEL TRAINING SYSTEM FOR THE STATE-OF-THE-ART ENTERPRISES701043
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