All articles

All articles

№	Article title	Number of downloads	Number of views
1	23.2.2018 On the Role of Space in Origination of Inertia Force Field, Earth Gravity Force Field and Zero Gravity of Material Body	17	661
2	22.2.2018 Uncertainty Calculation Procedure during Measuring Instrumentation Calibration	20	736
3	21.2.2018 Ensuring Aiming Accuracy of Ship’s Telemetry Reception Antenna Installation for Small Vessels	19	381
4	20.2.2018 The Use of Special Devices during Launch Pad Development Testing	17	369
5	19.2.2018 Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles	16	492
6	18.2.2018 Angular Stabilization of an Object Rapidly Rotating around Longitudial Axis	17	397
7	17.2.2018 Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine	15	349
8	16.2.2018 Design Solutions to Prevent Propellant Ingress into SRM Case Space behind Sealing Ring	17	547
9	15.2.2018 Topical Issues of Creation of Space Rocket Thermostatic System Mating Points	18	267
10	14.2.2018 A Concept of Modular Transport Vehicle for Lunar Program	17	316
11	13.2.2018 On an Approach to Constructing the Extremes in the Tasks of Optimal Solutions Search	13	189
12	12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs	16	360
13	11.2.2018 Some Peculiarities of Ensuring LRE Guarantied Service Life in the Conditions of Replacement of Components of Interindustry Application	17	388
14	10.2.2018 Calculation of Gas Flow in High-Altitude Engine Nozzle and Experience of Using Water-Cooled Nozzle Head during Tests	16	535
15	9.2.2018 The Impact of Worm Design on Power and Anti-Cavitation Properties of Worm-Centrifugal Pumps	16	657
16	8.2.2018 Development of Nozzle Blocks New Manufacturing Technology without Blazing	15	452
17	7.2.2018 Theoretical Models of Sound Speed Increase Effects in Gas Duct with Corrugated Wall	15	599
18	6.2.2018 Introduction of Additive Technologies for LRE Parts Manufacturing	17	389
19	5.2.2018 Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office	14	598
20	4.2.2018 Turbopump Units of Rocket Engines Developed by DO-4	20	243
21	3.2.2018 Possible Ways of Modernization of VEGA Launch Vehicle AVUM Stage Main Engine Assembly	16	626
22	2.2.2018 Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines	18	206
23	1.2.2018 Design Office of Liquid Rocket Engines is 60	19	98
24	16.1.2018 Some Correlation Dependences in Families of Aton and Apollo and Rendezvous Frequency in Main Asteroid Belt	18	192
25	15.1.2018 The Results of Using Automated Methods to Solve Standardization Tasks in Yuzhnoye SDO Practice	17	392
26	14.1.2018 A Rectangular Section Pipes Winding Programs Calculation Procedure	20	315
27	13.1.2018 On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses	16	358
28	11.1.2018 Ensuring Long Lifetime of the Electrochemical Accumulators Included in Space Rocketry Electric Power Supply Systems	18	404
29	12.1.2018 A Device for Soft Separation of Spacecraft from Launch Vehicle	23	509
30	10.1.2018 The Rocket Propellant Vapors and Water Solutions Neutralization Units. The Accumulated Experience and Prospects of Updating the Neutralization Units	20	243
31	9.1.2018 On the Peculiarities of High-Temperature Rocket Propellants Drain from Delivery Means to Filling Tank for Closed Drain	18	364
32	8.1.2018 The Solid–Propellant Motors with Regulated Thrust	13	367
33	7.1.2018 Prospective Gas Purification Device for LRE Test Bench	15	285
34	6.1.2018 On Building of Inertial Navigation System in the Condition of Presence of Considerable g-Load and Angular Velocity in Preferential Direction	20	333
35	5.1.2018 Experimental Determination of Lateral Force Caused by SRM Thrust Vector Eccentricity and Skew	26	477
36	4.1.2018 Determination of Angular Acceleration of Rotary Elements of Rocket Systems during Ground Tests	21	185
37	3.1.2018 The Means of Functional Suppression of Radio Electronic Facilities of Small-Size Unmanned Aerial Vehicles with Electromagnetic Radiation Focusing	19	453
38	2.1.2018 Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop	16	340
39	1.1.2018 Modernization and Automation of Temperature Calculation of Measurement Errors of Climatic Chambers for Accelerated Environmental Tests	17	409
40	12.1.2017 Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator	17	378
41	13.1.2017 Reliability Evaluation of ILV Thermostating System Mating Hoses	21	428
42	1.1.2017 Methodology for Measurement Uncertainty Evaluation during Metrological Certification of Measuring Instruments	25	241
43	10.1.2017 Features of Measurement System for Gas-Dynamic Model Tests of Rocket Complex Elements	17	248
44	11.1.2017 Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors	21	171
45	17.1.2017 Peculiarities of Design and Development Test of Dispenser Turning Actuator System for SHM with Iridium NEXT SC	18	384
46	16.1.2017 Principal Directions for Creation of Integrated Launch Vehicle Autonomous Onboard Flight Safety System	20	432
47	15.1.2017 Assessment of Liquid Equipment Neutralization Method Effectiveness	22	186
48	14.1.2017 Design Studies into Dynamic and Structural Characteristics of Two-Stage Direct-Action Solenoid-Operated Hydraulic Valve	18	231
49	7.1.2017 Static Approach Application in Analysis of Gas-Dynamic Parameters in Launch Vehicle Vented Bays	17	162
50	9.1.2017 Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles	15	246
51	6.1.2017 Drought Post-Effects Satellite Monitoring	19	462
52	8.1.2017 Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions	20	172
53	2.1.2017 Ultimate Stability Stresses in Smooth Cylindrical Skins. Dynamic Problem	16	200
54	3.1.2017 Development Strength Test of Modified Antares ILV	19	193
55	5.1.2017 Development of Working Liquid Discontinuity Measurement Procedure and Its Certification	17	247
56	4.1.2017 Basic Selection Criteria of Heat-Resistant and Thermal Protective Structures for High-Altitude Hypersonic Flying Vehicle	18	294
57	27.2.2017 Solution of “Unsolvable” Problems	20	151
58	26.2.2017 State of the Art and Prospects for Nuclear-Quadrupole Resonance Thermometry in Ukraine	16	552
59	25.2.2017 Vacuum Conditions Simulation Criteria	19	334
60	24.2.2017 Method of Supercooled Cryogenic Liquid Production	16	99
61	23.2.2017 Optimization Technique for Mass of Locally Loaded Rocket Bays with Wafer Structure	18	402
62	22.2.2017 Advanced Aluminum Alloys for Launch Vehicle Pipeline Parts Manufacture	18	367
63	21.2.2017 Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft	14	288
64	20.2.2017 Research Support for Development of Launch Vehicle Payload Unit Composite Load-Bearing Compartments	22	490
65	19.2.2017 Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation	19	210
66	18.2.2017 Development Test of Payload Fairing Separation Dynamics under Ground Conditions	20	131
67	17.2.2017 Development Test of Spacecraft Separation Dynamics under Ground Conditions	18	279
68	16.2.2017 Determination of Spherical Flange Connections Gasket Clamping Site Width	20	130
69	15.2.2017 Oxidizer Feedline Structural Optimization Results	20	428
70	14.2.2017 Development Test of Isolating Valve Operation under Cryogenic Conditions	16	159
71	13.2.2017 Experience in Development of Isolating Fuel Valve with Pneumatic Drive and Hydraulic Brake for Operation under Cryogenic Conditions	13	358
72	12.2.2017 Determination Procedure for Pneudraulic System and Its Components No-Failure Operation Probability	19	227
73	11.2.2017 Remote Monitoring Method of Pneudraulic System Structural Elements Integrity	20	154
74	10.2.2017 Analysis Method of Hydraulic Parameters of Circular Intake Device in Limit Operating Modes	16	228
75	9.2.2017 Peculiarities of Development of Cryogenic Propulsion System Circulating Cooling System	19	266
76	2.2.2017 Creation of Universal System of Launch Vehicle Space Head Modules for Cluster Spacecraft Missions	21	269
77	8.2.2017 Analysis Method of Nitrogen Tetroxide Tanks Generating Pressurization Systems	15	128
78	7.2.2017 Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants	18	229
79	6.2.2017 Set of Actions on Enhancement of Launch Vehicle Payload Capability	22	224
80	5.2.2017 Structural Perfection of Cyclone-4 Integrated Launch Vehicle	18	145
81	4.2.2017 Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics	15	130
82	1.2.2017 DO-2 – Semicentenary	19	97
83	3.2.2017 Creation of Advanced Facilities for Spacecraft / Launch Vehicle Integration	17	110
84	10.2.2019 Dynamic performance of the gas drive with jet motor	21	988
85	9.2.2019 Gas-dynamic simulation of the supersonic stream in the pulsed wind tunnel	18	424
86	2.2.2019 Mathematical models for assessment of safety in the impact area of cluster ammunition of the warhead during missile complex testing	17	524
87	1.2.2019 Optimization of the trajectory of the antiaircraft guided missile	24	806
88	14.2.2019 Selection of the validation algorithm for the solid rocket motor trust measurement procedure	19	332
89	13.2.2019 Study of the stress and strain state of the multilayer bellows	17	373
90	12.2.2019 Procedure of acoustic loads measuring during the ILV launch	15	197
91	11.2.2019 Winding the tubes of rectangular section using dowels	15	268
92	8.2.2019 Evaluation of the external acoustic loads, acting on the rocket when it passes the leg with maximum velocity head	16	135
93	7.2.2019 On critical stress of the longitudinal stability of the stiffened cylindrical shells. Dynamic problem	16	187
94	6.2.2019 Stabilization of gas reducers adjustment	24	307
95	5.2.2019 Features of the development testing of the propellants deposition inside the tanks of launch vehicles	23	270
96	4.2.2019 Numerical simulation of behavior of elastic structures with local stiffening elementse	17	267
97	3.2.2019 Features of design and production of the technological aids for assembly of the spacecraft separation system of CLAMP BAND type	9	393
98	1.1.2016 Solid Rocket Motors Developed by DO-5	20	109
99	21.1.2016 Selection of Optimal Parameters of Wind Desalting System with Hydrogen Energy Storage Unit	16	150
100	20.1.2016 Determination of External Characteristic of Autonomous WPP for Regulation by Rotor Withdrawal from under Wind	20	118
101	19.1.2016 Blade Geometry for Maximal Power Coefficient and Minimal Noise Level	17	107
102	18.1.2016 Method of Design Evaluation of SRM Lifetime and Ensuring its Long-Term Operation	19	94
103	17.1.2016 Modeling of Solid Rocket Motor Starting Process	19	296
104	16.1.2016 Peculiarities of Development of SRM Thrust Vector Controls at DO-5	17	197
105	15.1.2016 Calculation of Solid Propellant Grain Burning Surface Using Automated 3D-Modeling Systems	19	223
106	14.1.2016 Development of Powder Pressure Accumulators for Rocket Cold Start – the Most Important Condition of its Successful Realization	22	122
107	13.1.2016 The Impact of Diaphragm’s Shape on Gas Dynamic Flow Characteristics in Small-Size SRM Combustion Chamber	15	146
108	12.1.2016 Increasing Effectiveness of Meteorological Rockets when Using Hybrid Motors	19	88
109	11.1.2016 Methodology of Design Evaluation of Main SRM Flowrate-Thrust Characteristics after Stage Separation	17	110
110	10.1.2016 Development of Winding Pattern during Calculation of Composite Case Winding Programs	15	192
111	9.1.2016 Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method	21	119
112	8.1.2016 Assessment of Validity of Hypothesis of Constancy of Specific Vacuum Thrust Pulse during SRM Designing and Testing	18	90
113	7.1.2016 Updated Design of SRM Test Rig	19	195
114	6.1.2016 Ensuring Solid Rocket Motor Moisture Resistance by Design	15	327
115	5.1.2016 Scientific-Technical Base for Creation of Detonation Solid Rocket Motors	18	231
116	2.1.2016 Experience of Testing SRM Thrust Vector Controls	19	231
117	4.1.2016 The Company’s Experience in Designing and Operating Special Bench Equipment for SRM Ground Tests	17	101
118	3.1.2016 On Peculiarities of Life Testing and Safe Storage of Solid Rocket Motors	17	280
119	1.2.2016 On Minimal Aerodynamic Resistance of Rotation Body at Zero Angle of Attack in Hypersonic Non-Viscous Flow	20	84
120	2.2.2016 Normalization of Technical System Reliability Using Information Approach	19	81
121	16.2.2016 Method of Coefficient for Optimization and Analysis of Operating State of Fine Filter Cases	20	206
122	15.2.2016 A New Method of Testing Oil-Filled Current Transformers for Explosion-Proofness	17	240
123	14.2.2016 Investigation of Deformability of Carbon Plastic Panels in Moisture Absorption Process	17	548
124	13.2.2016 Experience of Developing Thermometric Instruments Based on Nuclear Quadrupole Resonance	21	199
125	12.2.2016 The Use of Thermoelectric Technologies in Spacecraft Thermostatic Systems	16	244
126	11.2.2016 Experimental Investigation into Power Characteristics of Fast-Flowrate Gas Jet Propulsion Systems	18	151
127	10.2.2016 Mathematical Model of High-Flowrate Electropneumatic Valve	17	126
128	9.2.2016 Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands	23	213
129	8.2.2016 Development and Validation of Program Module for Construction of Virtual Models of Real Structures in ANSYS System	17	117
130	7.2.2016 Analysis of Operation Modes and Selection of Chemical Current Source Included in Autonomous Electric Power Supply Systems of Self-Propelled Launcher	16	205
131	6.2.2016 Experimental Investigations into Results of Testing Cyclone-4 ILV Thermostating System Mating Points	18	179
132	5.2.2016 Creation of Technological Tooling and Testing of Cocoon-Type Cases Manufacturing Technology	18	250
133	4.2.2016 Experimental Investigations of Possibility of Creating Impulse SRM with Short Operation Period	17	338
134	3.2.2016 Selection of Optimal Trajectories of Spacecraft Launch Vehicles	16	240
135	10.1.2019 Semi-Empirical Evaluation of External Acoustic Loads in Payload Area during Lift-off	18	383
136	9.1.2019 Modeling of Cyclone-4M Rocket Jet Acoustic Emission by Volumetric Source	19	381
137	8.1.2019 Virtual Tests of Cassette Reentry Vehicle Dash Elements Attachment System during Ground Operation	20	433
138	7.1.2019 Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on High-Temperature Propellants	20	252
139	6.1.2019 Investigation into Peculiarities of Delivery to Launch Base of Rocket Propellant with Specified Gasing	15	236
140	5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime	17	318
141	4.1.2019 Mathematic Modeling and Investigation into Stress-Strain State of Space Rocket Bays	19	419
142	3.1.2019 Analysis of Spacecraft Control Issues In Early Design Phases	28	198
143	2.1.2019 Flying Vehicle Maneuvering Dynamics in Atmosphere with Weight Asymmetry and Elements of Terminal Control in Turn Leg	26	208
144	1.1.2019 On 65-th anniversary of the company	20	99
145	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	16	374
146	26.1.2019 New Technologies and Problems of Their Introducing in Ukraine	20	285
147	25.1.2019 Technological Peculiarities of Manufacturing Products of Irregular Profile by Method of Selective Laser Melting of 316L Powder Metal Material	17	453
148	24.1.2019 Porous Cast Materials (Gasars). Options of Their Use in Space Rocket Hardware	23	364
149	23.1.2019 Calculation of Thermal-Physical Properties of Gaseous Xenon	16	297
150	22.1.2019 Calculation of Uncertainty of Represented Values of Linear Accelerations during Centrifugal Machines Certification	17	308
151	21.1.2019 Optimization of Geometrical Shape of Isolation Valve Blading Position	17	262
152	20.1.2019 Possibilities of Increasing Acting Loads on Hydraulic Actuator Middle Position Lock	19	204
153	19.1.2019 Peculiarities of Radio Transparent Fairings Development	17	267
154	18.1.2019 Designing of Servo Driver of Throttle Mechanisms and Fuel Flow Regulator of ILV Main Motor	18	293
155	17.1.2019 Development of Prospective Small-Size Auxiliary SMR of New Type	17	450
156	16.1.2019 Oscillation Processes in Rig at the Moment of SRM Transfer to Main Operation Mode	17	321
157	15.1.2019 Simulation of SMR Oscillations in Rig that Arise during Firing Bench Test	19	413
158	14.1.2019 Technique of Determination of SRM Operational Life Taking into Account Materials and Elements Strength Margins	19	108
159	13.1.2019 Prediction of Solid Propellant Burnout Time in Launch Vehicle Propulsion System in Flight	20	324
160	12.1.2019 Monitoring of Launch Platform Drift Parameters during Zenit-3SL Integrated Launch Vehicle Prelauch Processing	19	307
161	11.1.2019 Peculiarities of Development Testing of Space Rocket Thermostating System Mating Points Hoses	16	169
162	3.1.2020 Analysis of the unsteady stress-strain behavior of the launch vehicle hold-down bay at liftoff	23	814
163	2.1.2020 Analysis of development trends of design parameters and basic characteristics of missiles for the advanced multiple launch rocket systems	16	1508
164	21.1.2020 Contemporary approaches to the improvement of methods of space launch system operation for commercial launches of ILV	14	405
165	20.1.2020 Studying the possibility of alternating delivery of rocket propellant wastes to a common thermal neutralization facility	17	458
166	19.1.2020 Pyrobolts: types, design, development. Shear type pyrobolt developed at Yuzhnoye SDO	20	956
167	18.1.2020 Development of autonomous power engineering systems with hydrogen energy storage	18	738
168	17.1.2020 Acoustic problems of rocket launch	16	567
169	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	14	641
170	15.1.2020 Simulation of thermomechanical processes in functionally-gradient materials of inhomogeneous structure in the manufacturing and operation of rocket structural elements	17	885
171	14.1.2020 On the problem of optimum control	17	421
172	13.1.2020 Mathematical models of hydraulic servomechanisms of space technology	12	355
173	12.1.2020 Modification of technology as the main course in the military transport aircraft development	17	465
174	11.1.2020 Some results of strength calculations relying on analytical and FEM approaches. Trends of using contemporary machine learning strategies	18	569
175	10.1.2020 Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM	18	575
176	9.1.2020 Experimental investigation of a liner-free propellant tank made from polymer composite materials	20	915
177	8.1.2020 Determining the main parameters of transport aircraft modifications considering the fuel efficiency	16	322
178	7.1.2020 Studying the motion of a launch vehicle and observed space debris objects during launch preparation	19	453
179	6.1.2020 Mechanics of a satellite cluster. Methods for estimating the probability of their maximal approach in flight	14	403
180	5.1.2020 Strength and stability of inhomogeneous structures of space technology, consid-ering plasticity and creep	19	1078
181	4.1.2020 Terminal guidance of the aircraft being maneuvering while descending in the atmosphere under conditions of aerodynamic balancing	19	362
182	1.1.2020 Solving a problem of optimum curves of descent using the enhanced Euler equation	16	569
183	9.1.2023 Methodology for selecting design parameters of solid-propellant sustainer engines. Mathematical support and software	26	512
184	8.1.2023 Specificity of developing pyrobolts with low impact and vibration impulse responses	20	377
185	7.1.2023 Specificity of using rubbers as structural materials for making connector assemblies of temperature conditioning systems	25	301
186	6.1.2023 Numerical modeling of translational and rotational vibrations of a solid-propellant rocket motor on a test stand during firing tests	27	377
187	5.1.2023 Fueling-neutralization stations. New developments and applications	23	346
188	4.1.2023 On control of spacecraft orientation to the ground data acquisition station	17	180
189	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	17	549
190	2.1.2023 How Yuzhnoye develops models for flight safety index evaluation for the case of a rocket failure during the flight	19	339
191	1.1.2023 On the development of a methodology for building air and missile defense systems. Explanation of the investigation mechanism	23	420

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