All articles

All articles

№	Article title	Number of downloads	Number of views
1	12.1.2024 Hardening of steels modifying their surfaces with ion-plasma nitriding in glow discharge	10	953
2	13.1.2024 MODEL OF QUALITY MANAGEMENT OF TECHNICAL PREPARATION FOR THE METAL+COMPOSITE JOINTS PRODUCTION	9	393
3	9.1.2024 General-purpose thermostatting module – new approach in development of up-to-date thermostating systems for rocket and space complexes	12	436
4	10.1.2024 METHOD OF AUTONOMOUS DETERMINATION OF THE ROCKET’S REFERENCE ATTITUDE DURING PRE-LAUNCH PROCESSING	11	504
5	8.1.2024 Theoretic-experimental evaluation of the solid-propellant grain erosive burning	13	248
6	11.1.2024 PARAMETERS CALCULATION OF THE LUNAR REGOLITH TRANSPORT SYSTEM	13	453
7	6.1.2024 New methods of load-carrying capacity prediction for the ultimately compressed frame structures	11	482
8	14.1.2024 EXPERIMENTAL STUDIES OF THE PERFORMANCE OF PYROTECHNIC DEVICES INSTALLED ON THE LAUNCH VEHICLE SEPARATION SYSTEMS	13	640
9	15.1.2024 Enhancing operability of the fuel system units in the hot climate conditions	13	671
10	16.1.2024 EDUCATIONAL TENDENCIES AS AN ELEMENT OF INNOVATIVE PROGRESS IN THE PERSONNEL TRAINING SYSTEM FOR THE STATE-OF-THE-ART ENTERPRISES	11	317
11	7.1.2024 Selection of the functional units for the Cyclone-4M ILV separation system	12	710
12	5.1.2024 Assessment of risk of toxic damage to people in case of a launch vehicle accident at flight	14	536
13	4.1.2024 The dynamics of servo drives	13	401
14	3.1.2024 Future projects of lunar exploration implemented by Yuzhnoye SDO	11	315
15	2.1.2024 New and advanced liquid rocket engines of the Yuzhnoye SDO	12	530
16	1.1.2024 ANTARES: Yuzhnoye’s project of XXI century	12	110
17	1.1.2020 Solving a problem of optimum curves of descent using the enhanced Euler equation	29	1150
18	2.1.2020 Analysis of development trends of design parameters and basic characteristics of missiles for the advanced multiple launch rocket systems	31	2898
19	10.1.2020 Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM	31	1131
20	3.1.2020 Analysis of the unsteady stress-strain behavior of the launch vehicle hold-down bay at liftoff	35	1441
21	21.1.2020 Contemporary approaches to the improvement of methods of space launch system operation for commercial launches of ILV	27	760
22	20.1.2020 Studying the possibility of alternating delivery of rocket propellant wastes to a common thermal neutralization facility	31	827
23	19.1.2020 Pyrobolts: types, design, development. Shear type pyrobolt developed at Yuzhnoye SDO	34	1516
24	18.1.2020 Development of autonomous power engineering systems with hydrogen energy storage	31	1259
25	17.1.2020 Acoustic problems of rocket launch	28	1027
26	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	31	1341
27	15.1.2020 Simulation of thermomechanical processes in functionally-gradient materials of inhomogeneous structure in the manufacturing and operation of rocket structural elements	31	1479
28	14.1.2020 On the problem of optimum control	31	798
29	13.1.2020 Mathematical models of hydraulic servomechanisms of space technology	25	649
30	12.1.2020 Modification of technology as the main course in the military transport aircraft development	29	809
31	11.1.2020 Some results of strength calculations relying on analytical and FEM approaches. Trends of using contemporary machine learning strategies	31	1032
32	9.1.2020 Experimental investigation of a liner-free propellant tank made from polymer composite materials	30	1562
33	8.1.2020 Determining the main parameters of transport aircraft modifications considering the fuel efficiency	30	513
34	7.1.2020 Studying the motion of a launch vehicle and observed space debris objects during launch preparation	30	820
35	6.1.2020 Mechanics of a satellite cluster. Methods for estimating the probability of their maximal approach in flight	27	685
36	5.1.2020 Strength and stability of inhomogeneous structures of space technology, consid-ering plasticity and creep	31	2074
37	4.1.2020 Terminal guidance of the aircraft being maneuvering while descending in the atmosphere under conditions of aerodynamic balancing	30	625
38	10.2.2017 Analysis Method of Hydraulic Parameters of Circular Intake Device in Limit Operating Modes	29	714
39	11.2.2017 Remote Monitoring Method of Pneudraulic System Structural Elements Integrity	30	465
40	27.2.2017 Solution of “Unsolvable” Problems	31	268
41	26.2.2017 State of the Art and Prospects for Nuclear-Quadrupole Resonance Thermometry in Ukraine	30	1000
42	25.2.2017 Vacuum Conditions Simulation Criteria	31	501
43	24.2.2017 Method of Supercooled Cryogenic Liquid Production	33	242
44	23.2.2017 Optimization Technique for Mass of Locally Loaded Rocket Bays with Wafer Structure	30	840
45	22.2.2017 Advanced Aluminum Alloys for Launch Vehicle Pipeline Parts Manufacture	31	558
46	21.2.2017 Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft	27	437
47	20.2.2017 Research Support for Development of Launch Vehicle Payload Unit Composite Load-Bearing Compartments	37	942
48	19.2.2017 Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation	27	344
49	18.2.2017 Development Test of Payload Fairing Separation Dynamics under Ground Conditions	36	270
50	17.2.2017 Development Test of Spacecraft Separation Dynamics under Ground Conditions	31	459
51	16.2.2017 Determination of Spherical Flange Connections Gasket Clamping Site Width	31	203
52	15.2.2017 Oxidizer Feedline Structural Optimization Results	31	696
53	14.2.2017 Development Test of Isolating Valve Operation under Cryogenic Conditions	29	307
54	13.2.2017 Experience in Development of Isolating Fuel Valve with Pneumatic Drive and Hydraulic Brake for Operation under Cryogenic Conditions	29	704
55	12.2.2017 Determination Procedure for Pneudraulic System and Its Components No-Failure Operation Probability	33	447
56	9.2.2017 Peculiarities of Development of Cryogenic Propulsion System Circulating Cooling System	29	524
57	2.2.2017 Creation of Universal System of Launch Vehicle Space Head Modules for Cluster Spacecraft Missions	31	504
58	8.2.2017 Analysis Method of Nitrogen Tetroxide Tanks Generating Pressurization Systems	24	257
59	7.2.2017 Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants	32	435
60	6.2.2017 Set of Actions on Enhancement of Launch Vehicle Payload Capability	35	439
61	5.2.2017 Structural Perfection of Cyclone-4 Integrated Launch Vehicle	27	257
62	4.2.2017 Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics	30	215
63	1.2.2017 DO-2 – Semicentenary	31	202
64	3.2.2017 Creation of Advanced Facilities for Spacecraft / Launch Vehicle Integration	30	212
65	23.2.2018 On the Role of Space in Origination of Inertia Force Field, Earth Gravity Force Field and Zero Gravity of Material Body	28	1092
66	22.2.2018 Uncertainty Calculation Procedure during Measuring Instrumentation Calibration	30	1423
67	21.2.2018 Ensuring Aiming Accuracy of Ship’s Telemetry Reception Antenna Installation for Small Vessels	30	750
68	20.2.2018 The Use of Special Devices during Launch Pad Development Testing	26	680
69	19.2.2018 Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles	26	859
70	18.2.2018 Angular Stabilization of an Object Rapidly Rotating around Longitudial Axis	29	746
71	17.2.2018 Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine	28	574
72	16.2.2018 Design Solutions to Prevent Propellant Ingress into SRM Case Space behind Sealing Ring	27	970
73	15.2.2018 Topical Issues of Creation of Space Rocket Thermostatic System Mating Points	30	473
74	14.2.2018 A Concept of Modular Transport Vehicle for Lunar Program	27	566
75	13.2.2018 On an Approach to Constructing the Extremes in the Tasks of Optimal Solutions Search	23	380
76	12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs	29	683
77	11.2.2018 Some Peculiarities of Ensuring LRE Guarantied Service Life in the Conditions of Replacement of Components of Interindustry Application	28	726
78	10.2.2018 Calculation of Gas Flow in High-Altitude Engine Nozzle and Experience of Using Water-Cooled Nozzle Head during Tests	28	1051
79	9.2.2018 The Impact of Worm Design on Power and Anti-Cavitation Properties of Worm-Centrifugal Pumps	29	1142
80	8.2.2018 Development of Nozzle Blocks New Manufacturing Technology without Blazing	26	805
81	7.2.2018 Theoretical Models of Sound Speed Increase Effects in Gas Duct with Corrugated Wall	26	1024
82	6.2.2018 Introduction of Additive Technologies for LRE Parts Manufacturing	27	741
83	5.2.2018 Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office	25	1138
84	4.2.2018 Turbopump Units of Rocket Engines Developed by DO-4	34	444
85	3.2.2018 Possible Ways of Modernization of VEGA Launch Vehicle AVUM Stage Main Engine Assembly	28	1145
86	2.2.2018 Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines	32	378
87	1.2.2018 Design Office of Liquid Rocket Engines is 60	32	248
88	16.1.2018 Some Correlation Dependences in Families of Aton and Apollo and Rendezvous Frequency in Main Asteroid Belt	30	329
89	15.1.2018 The Results of Using Automated Methods to Solve Standardization Tasks in Yuzhnoye SDO Practice	27	685
90	14.1.2018 A Rectangular Section Pipes Winding Programs Calculation Procedure	28	588
91	13.1.2018 On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses	29	672
92	11.1.2018 Ensuring Long Lifetime of the Electrochemical Accumulators Included in Space Rocketry Electric Power Supply Systems	31	773
93	12.1.2018 A Device for Soft Separation of Spacecraft from Launch Vehicle	35	828
94	10.1.2018 The Rocket Propellant Vapors and Water Solutions Neutralization Units. The Accumulated Experience and Prospects of Updating the Neutralization Units	35	443
95	9.1.2018 On the Peculiarities of High-Temperature Rocket Propellants Drain from Delivery Means to Filling Tank for Closed Drain	29	741
96	8.1.2018 The Solid–Propellant Motors with Regulated Thrust	25	728
97	7.1.2018 Prospective Gas Purification Device for LRE Test Bench	27	494
98	6.1.2018 On Building of Inertial Navigation System in the Condition of Presence of Considerable g-Load and Angular Velocity in Preferential Direction	30	608
99	5.1.2018 Experimental Determination of Lateral Force Caused by SRM Thrust Vector Eccentricity and Skew	38	928
100	4.1.2018 Determination of Angular Acceleration of Rotary Elements of Rocket Systems during Ground Tests	31	369
101	3.1.2018 The Means of Functional Suppression of Radio Electronic Facilities of Small-Size Unmanned Aerial Vehicles with Electromagnetic Radiation Focusing	30	736
102	2.1.2018 Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop	26	626
103	1.1.2018 Modernization and Automation of Temperature Calculation of Measurement Errors of Climatic Chambers for Accelerated Environmental Tests	27	742
104	12.1.2017 Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator	26	673
105	13.1.2017 Reliability Evaluation of ILV Thermostating System Mating Hoses	34	821
106	1.1.2017 Methodology for Measurement Uncertainty Evaluation during Metrological Certification of Measuring Instruments	37	388
107	10.1.2017 Features of Measurement System for Gas-Dynamic Model Tests of Rocket Complex Elements	31	451
108	11.1.2017 Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors	32	322
109	17.1.2017 Peculiarities of Design and Development Test of Dispenser Turning Actuator System for SHM with Iridium NEXT SC	27	684
110	16.1.2017 Principal Directions for Creation of Integrated Launch Vehicle Autonomous Onboard Flight Safety System	30	794
111	15.1.2017 Assessment of Liquid Equipment Neutralization Method Effectiveness	35	321
112	14.1.2017 Design Studies into Dynamic and Structural Characteristics of Two-Stage Direct-Action Solenoid-Operated Hydraulic Valve	28	412
113	7.1.2017 Static Approach Application in Analysis of Gas-Dynamic Parameters in Launch Vehicle Vented Bays	28	328
114	9.1.2017 Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles	27	519
115	6.1.2017 Drought Post-Effects Satellite Monitoring	31	755
116	8.1.2017 Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions	33	326
117	2.1.2017 Ultimate Stability Stresses in Smooth Cylindrical Skins. Dynamic Problem	28	329
118	3.1.2017 Development Strength Test of Modified Antares ILV	34	354
119	5.1.2017 Development of Working Liquid Discontinuity Measurement Procedure and Its Certification	26	447
120	4.1.2017 Basic Selection Criteria of Heat-Resistant and Thermal Protective Structures for High-Altitude Hypersonic Flying Vehicle	33	538
121	10.2.2019 Dynamic performance of the gas drive with jet motor	32	1680
122	9.2.2019 Gas-dynamic simulation of the supersonic stream in the pulsed wind tunnel	31	852
123	2.2.2019 Mathematical models for assessment of safety in the impact area of cluster ammunition of the warhead during missile complex testing	30	976
124	1.2.2019 Optimization of the trajectory of the antiaircraft guided missile	37	1631
125	14.2.2019 Selection of the validation algorithm for the solid rocket motor trust measurement procedure	33	626
126	13.2.2019 Study of the stress and strain state of the multilayer bellows	31	680
127	12.2.2019 Procedure of acoustic loads measuring during the ILV launch	30	436
128	11.2.2019 Winding the tubes of rectangular section using dowels	28	492
129	8.2.2019 Evaluation of the external acoustic loads, acting on the rocket when it passes the leg with maximum velocity head	28	261
130	7.2.2019 On critical stress of the longitudinal stability of the stiffened cylindrical shells. Dynamic problem	30	346
131	6.2.2019 Stabilization of gas reducers adjustment	38	566
132	5.2.2019 Features of the development testing of the propellants deposition inside the tanks of launch vehicles	35	538
133	4.2.2019 Numerical simulation of behavior of elastic structures with local stiffening elementse	32	489
134	3.2.2019 Features of design and production of the technological aids for assembly of the spacecraft separation system of CLAMP BAND type	20	711
135	1.1.2016 Solid Rocket Motors Developed by DO-5	49	223
136	21.1.2016 Selection of Optimal Parameters of Wind Desalting System with Hydrogen Energy Storage Unit	29	254
137	20.1.2016 Determination of External Characteristic of Autonomous WPP for Regulation by Rotor Withdrawal from under Wind	33	249
138	19.1.2016 Blade Geometry for Maximal Power Coefficient and Minimal Noise Level	30	155
139	18.1.2016 Method of Design Evaluation of SRM Lifetime and Ensuring its Long-Term Operation	34	248
140	17.1.2016 Modeling of Solid Rocket Motor Starting Process	30	565
141	16.1.2016 Peculiarities of Development of SRM Thrust Vector Controls at DO-5	25	311
142	15.1.2016 Calculation of Solid Propellant Grain Burning Surface Using Automated 3D-Modeling Systems	29	412
143	14.1.2016 Development of Powder Pressure Accumulators for Rocket Cold Start – the Most Important Condition of its Successful Realization	35	225
144	13.1.2016 The Impact of Diaphragm’s Shape on Gas Dynamic Flow Characteristics in Small-Size SRM Combustion Chamber	27	309
145	12.1.2016 Increasing Effectiveness of Meteorological Rockets when Using Hybrid Motors	29	184
146	11.1.2016 Methodology of Design Evaluation of Main SRM Flowrate-Thrust Characteristics after Stage Separation	29	220
147	10.1.2016 Development of Winding Pattern during Calculation of Composite Case Winding Programs	27	351
148	9.1.2016 Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method	34	221
149	8.1.2016 Assessment of Validity of Hypothesis of Constancy of Specific Vacuum Thrust Pulse during SRM Designing and Testing	29	260
150	7.1.2016 Updated Design of SRM Test Rig	28	332
151	6.1.2016 Ensuring Solid Rocket Motor Moisture Resistance by Design	26	623
152	5.1.2016 Scientific-Technical Base for Creation of Detonation Solid Rocket Motors	27	399
153	2.1.2016 Experience of Testing SRM Thrust Vector Controls	30	455
154	4.1.2016 The Company’s Experience in Designing and Operating Special Bench Equipment for SRM Ground Tests	27	185
155	3.1.2016 On Peculiarities of Life Testing and Safe Storage of Solid Rocket Motors	31	585
156	1.2.2016 On Minimal Aerodynamic Resistance of Rotation Body at Zero Angle of Attack in Hypersonic Non-Viscous Flow	32	195
157	2.2.2016 Normalization of Technical System Reliability Using Information Approach	31	165
158	16.2.2016 Method of Coefficient for Optimization and Analysis of Operating State of Fine Filter Cases	31	365
159	15.2.2016 A New Method of Testing Oil-Filled Current Transformers for Explosion-Proofness	30	520
160	14.2.2016 Investigation of Deformability of Carbon Plastic Panels in Moisture Absorption Process	29	972
161	13.2.2016 Experience of Developing Thermometric Instruments Based on Nuclear Quadrupole Resonance	34	330
162	12.2.2016 The Use of Thermoelectric Technologies in Spacecraft Thermostatic Systems	30	471
163	11.2.2016 Experimental Investigation into Power Characteristics of Fast-Flowrate Gas Jet Propulsion Systems	31	280
164	10.2.2016 Mathematical Model of High-Flowrate Electropneumatic Valve	28	303
165	9.2.2016 Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands	34	378
166	8.2.2016 Development and Validation of Program Module for Construction of Virtual Models of Real Structures in ANSYS System	28	222
167	7.2.2016 Analysis of Operation Modes and Selection of Chemical Current Source Included in Autonomous Electric Power Supply Systems of Self-Propelled Launcher	27	349
168	6.2.2016 Experimental Investigations into Results of Testing Cyclone-4 ILV Thermostating System Mating Points	29	263
169	5.2.2016 Creation of Technological Tooling and Testing of Cocoon-Type Cases Manufacturing Technology	31	496
170	4.2.2016 Experimental Investigations of Possibility of Creating Impulse SRM with Short Operation Period	28	651
171	3.2.2016 Selection of Optimal Trajectories of Spacecraft Launch Vehicles	29	417
172	10.1.2019 Semi-Empirical Evaluation of External Acoustic Loads in Payload Area during Lift-off	31	670
173	9.1.2019 Modeling of Cyclone-4M Rocket Jet Acoustic Emission by Volumetric Source	29	718
174	8.1.2019 Virtual Tests of Cassette Reentry Vehicle Dash Elements Attachment System during Ground Operation	34	799
175	7.1.2019 Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on High-Temperature Propellants	32	393
176	6.1.2019 Investigation into Peculiarities of Delivery to Launch Base of Rocket Propellant with Specified Gasing	27	513
177	5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime	30	661
178	4.1.2019 Mathematic Modeling and Investigation into Stress-Strain State of Space Rocket Bays	29	901
179	3.1.2019 Analysis of Spacecraft Control Issues In Early Design Phases	37	462
180	2.1.2019 Flying Vehicle Maneuvering Dynamics in Atmosphere with Weight Asymmetry and Elements of Terminal Control in Turn Leg	40	479
181	1.1.2019 On 65-th anniversary of the company	32	200
182	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	25	625
183	26.1.2019 New Technologies and Problems of Their Introducing in Ukraine	32	589
184	25.1.2019 Technological Peculiarities of Manufacturing Products of Irregular Profile by Method of Selective Laser Melting of 316L Powder Metal Material	26	745
185	24.1.2019 Porous Cast Materials (Gasars). Options of Their Use in Space Rocket Hardware	30	726
186	23.1.2019 Calculation of Thermal-Physical Properties of Gaseous Xenon	23	587
187	22.1.2019 Calculation of Uncertainty of Represented Values of Linear Accelerations during Centrifugal Machines Certification	23	523
188	21.1.2019 Optimization of Geometrical Shape of Isolation Valve Blading Position	27	432
189	20.1.2019 Possibilities of Increasing Acting Loads on Hydraulic Actuator Middle Position Lock	26	442
190	19.1.2019 Peculiarities of Radio Transparent Fairings Development	28	596
191	18.1.2019 Designing of Servo Driver of Throttle Mechanisms and Fuel Flow Regulator of ILV Main Motor	32	554
192	17.1.2019 Development of Prospective Small-Size Auxiliary SMR of New Type	26	740
193	16.1.2019 Oscillation Processes in Rig at the Moment of SRM Transfer to Main Operation Mode	27	508
194	15.1.2019 Simulation of SMR Oscillations in Rig that Arise during Firing Bench Test	29	763
195	14.1.2019 Technique of Determination of SRM Operational Life Taking into Account Materials and Elements Strength Margins	31	204
196	13.1.2019 Prediction of Solid Propellant Burnout Time in Launch Vehicle Propulsion System in Flight	31	576
197	12.1.2019 Monitoring of Launch Platform Drift Parameters during Zenit-3SL Integrated Launch Vehicle Prelauch Processing	30	602
198	11.1.2019 Peculiarities of Development Testing of Space Rocket Thermostating System Mating Points Hoses	30	302
199	9.1.2023 Methodology for selecting design parameters of solid-propellant sustainer engines. Mathematical support and software	39	1057
200	8.1.2023 Specificity of developing pyrobolts with low impact and vibration impulse responses	30	644
201	7.1.2023 Specificity of using rubbers as structural materials for making connector assemblies of temperature conditioning systems	38	572
202	6.1.2023 Numerical modeling of translational and rotational vibrations of a solid-propellant rocket motor on a test stand during firing tests	39	596
203	5.1.2023 Fueling-neutralization stations. New developments and applications	34	592
204	4.1.2023 On control of spacecraft orientation to the ground data acquisition station	26	309
205	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	32	926
206	2.1.2023 How Yuzhnoye develops models for flight safety index evaluation for the case of a rocket failure during the flight	33	685
207	1.1.2023 On the development of a methodology for building air and missile defense systems. Explanation of the investigation mechanism	37	790

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