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	16	602
2	22.2.2018 Uncertainty Calculation Procedure during Measuring Instrumentation Calibration	19	662
3	21.2.2018 Ensuring Aiming Accuracy of Ship’s Telemetry Reception Antenna Installation for Small Vessels	18	349
4	20.2.2018 The Use of Special Devices during Launch Pad Development Testing	16	334
5	19.2.2018 Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles	14	441
6	18.2.2018 Angular Stabilization of an Object Rapidly Rotating around Longitudial Axis	16	361
7	17.2.2018 Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine	14	319
8	16.2.2018 Design Solutions to Prevent Propellant Ingress into SRM Case Space behind Sealing Ring	16	478
9	15.2.2018 Topical Issues of Creation of Space Rocket Thermostatic System Mating Points	17	252
10	14.2.2018 A Concept of Modular Transport Vehicle for Lunar Program	15	279
11	13.2.2018 On an Approach to Constructing the Extremes in the Tasks of Optimal Solutions Search	12	178
12	12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs	15	343
13	11.2.2018 Some Peculiarities of Ensuring LRE Guarantied Service Life in the Conditions of Replacement of Components of Interindustry Application	15	353
14	10.2.2018 Calculation of Gas Flow in High-Altitude Engine Nozzle and Experience of Using Water-Cooled Nozzle Head during Tests	15	488
15	9.2.2018 The Impact of Worm Design on Power and Anti-Cavitation Properties of Worm-Centrifugal Pumps	15	595
16	8.2.2018 Development of Nozzle Blocks New Manufacturing Technology without Blazing	14	401
17	7.2.2018 Theoretical Models of Sound Speed Increase Effects in Gas Duct with Corrugated Wall	14	553
18	6.2.2018 Introduction of Additive Technologies for LRE Parts Manufacturing	15	354
19	5.2.2018 Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office	13	540
20	4.2.2018 Turbopump Units of Rocket Engines Developed by DO-4	19	222
21	3.2.2018 Possible Ways of Modernization of VEGA Launch Vehicle AVUM Stage Main Engine Assembly	15	570
22	2.2.2018 Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines	18	193
23	1.2.2018 Design Office of Liquid Rocket Engines is 60	18	91
24	16.1.2018 Some Correlation Dependences in Families of Aton and Apollo and Rendezvous Frequency in Main Asteroid Belt	17	174
25	15.1.2018 The Results of Using Automated Methods to Solve Standardization Tasks in Yuzhnoye SDO Practice	16	345
26	14.1.2018 A Rectangular Section Pipes Winding Programs Calculation Procedure	19	281
27	13.1.2018 On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses	15	323
28	11.1.2018 Ensuring Long Lifetime of the Electrochemical Accumulators Included in Space Rocketry Electric Power Supply Systems	17	362
29	12.1.2018 A Device for Soft Separation of Spacecraft from Launch Vehicle	22	464
30	10.1.2018 The Rocket Propellant Vapors and Water Solutions Neutralization Units. The Accumulated Experience and Prospects of Updating the Neutralization Units	19	221
31	9.1.2018 On the Peculiarities of High-Temperature Rocket Propellants Drain from Delivery Means to Filling Tank for Closed Drain	18	319
32	8.1.2018 The Solid–Propellant Motors with Regulated Thrust	12	329
33	7.1.2018 Prospective Gas Purification Device for LRE Test Bench	14	253
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	19	312
35	5.1.2018 Experimental Determination of Lateral Force Caused by SRM Thrust Vector Eccentricity and Skew	25	430
36	4.1.2018 Determination of Angular Acceleration of Rotary Elements of Rocket Systems during Ground Tests	19	164
37	3.1.2018 The Means of Functional Suppression of Radio Electronic Facilities of Small-Size Unmanned Aerial Vehicles with Electromagnetic Radiation Focusing	18	408
38	2.1.2018 Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop	15	297
39	1.1.2018 Modernization and Automation of Temperature Calculation of Measurement Errors of Climatic Chambers for Accelerated Environmental Tests	16	377
40	12.1.2017 Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator	16	349
41	13.1.2017 Reliability Evaluation of ILV Thermostating System Mating Hoses	20	383
42	1.1.2017 Methodology for Measurement Uncertainty Evaluation during Metrological Certification of Measuring Instruments	24	230
43	10.1.2017 Features of Measurement System for Gas-Dynamic Model Tests of Rocket Complex Elements	17	230
44	11.1.2017 Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors	19	159
45	17.1.2017 Peculiarities of Design and Development Test of Dispenser Turning Actuator System for SHM with Iridium NEXT SC	16	337
46	16.1.2017 Principal Directions for Creation of Integrated Launch Vehicle Autonomous Onboard Flight Safety System	19	377
47	15.1.2017 Assessment of Liquid Equipment Neutralization Method Effectiveness	20	171
48	14.1.2017 Design Studies into Dynamic and Structural Characteristics of Two-Stage Direct-Action Solenoid-Operated Hydraulic Valve	17	219
49	7.1.2017 Static Approach Application in Analysis of Gas-Dynamic Parameters in Launch Vehicle Vented Bays	15	149
50	9.1.2017 Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles	14	234
51	6.1.2017 Drought Post-Effects Satellite Monitoring	18	418
52	8.1.2017 Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions	19	163
53	2.1.2017 Ultimate Stability Stresses in Smooth Cylindrical Skins. Dynamic Problem	14	185
54	3.1.2017 Development Strength Test of Modified Antares ILV	18	172
55	5.1.2017 Development of Working Liquid Discontinuity Measurement Procedure and Its Certification	16	227
56	4.1.2017 Basic Selection Criteria of Heat-Resistant and Thermal Protective Structures for High-Altitude Hypersonic Flying Vehicle	17	263
57	27.2.2017 Solution of “Unsolvable” Problems	19	139
58	26.2.2017 State of the Art and Prospects for Nuclear-Quadrupole Resonance Thermometry in Ukraine	16	485
59	25.2.2017 Vacuum Conditions Simulation Criteria	18	305
60	24.2.2017 Method of Supercooled Cryogenic Liquid Production	15	94
61	23.2.2017 Optimization Technique for Mass of Locally Loaded Rocket Bays with Wafer Structure	17	368
62	22.2.2017 Advanced Aluminum Alloys for Launch Vehicle Pipeline Parts Manufacture	18	336
63	21.2.2017 Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft	13	271
64	20.2.2017 Research Support for Development of Launch Vehicle Payload Unit Composite Load-Bearing Compartments	21	448
65	19.2.2017 Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation	17	189
66	18.2.2017 Development Test of Payload Fairing Separation Dynamics under Ground Conditions	19	121
67	17.2.2017 Development Test of Spacecraft Separation Dynamics under Ground Conditions	17	249
68	16.2.2017 Determination of Spherical Flange Connections Gasket Clamping Site Width	18	124
69	15.2.2017 Oxidizer Feedline Structural Optimization Results	19	398
70	14.2.2017 Development Test of Isolating Valve Operation under Cryogenic Conditions	14	144
71	13.2.2017 Experience in Development of Isolating Fuel Valve with Pneumatic Drive and Hydraulic Brake for Operation under Cryogenic Conditions	12	329
72	12.2.2017 Determination Procedure for Pneudraulic System and Its Components No-Failure Operation Probability	17	210
73	11.2.2017 Remote Monitoring Method of Pneudraulic System Structural Elements Integrity	18	140
74	10.2.2017 Analysis Method of Hydraulic Parameters of Circular Intake Device in Limit Operating Modes	15	206
75	9.2.2017 Peculiarities of Development of Cryogenic Propulsion System Circulating Cooling System	18	243
76	2.2.2017 Creation of Universal System of Launch Vehicle Space Head Modules for Cluster Spacecraft Missions	19	245
77	8.2.2017 Analysis Method of Nitrogen Tetroxide Tanks Generating Pressurization Systems	13	117
78	7.2.2017 Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants	17	206
79	6.2.2017 Set of Actions on Enhancement of Launch Vehicle Payload Capability	21	207
80	5.2.2017 Structural Perfection of Cyclone-4 Integrated Launch Vehicle	16	139
81	4.2.2017 Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics	13	121
82	1.2.2017 DO-2 – Semicentenary	18	89
83	3.2.2017 Creation of Advanced Facilities for Spacecraft / Launch Vehicle Integration	16	103
84	10.2.2019 Dynamic performance of the gas drive with jet motor	21	881
85	9.2.2019 Gas-dynamic simulation of the supersonic stream in the pulsed wind tunnel	18	389
86	2.2.2019 Mathematical models for assessment of safety in the impact area of cluster ammunition of the warhead during missile complex testing	16	476
87	1.2.2019 Optimization of the trajectory of the antiaircraft guided missile	23	732
88	14.2.2019 Selection of the validation algorithm for the solid rocket motor trust measurement procedure	18	303
89	13.2.2019 Study of the stress and strain state of the multilayer bellows	16	346
90	12.2.2019 Procedure of acoustic loads measuring during the ILV launch	14	183
91	11.2.2019 Winding the tubes of rectangular section using dowels	14	249
92	8.2.2019 Evaluation of the external acoustic loads, acting on the rocket when it passes the leg with maximum velocity head	14	127
93	7.2.2019 On critical stress of the longitudinal stability of the stiffened cylindrical shells. Dynamic problem	15	175
94	6.2.2019 Stabilization of gas reducers adjustment	23	279
95	5.2.2019 Features of the development testing of the propellants deposition inside the tanks of launch vehicles	22	242
96	4.2.2019 Numerical simulation of behavior of elastic structures with local stiffening elementse	16	246
97	3.2.2019 Features of design and production of the technological aids for assembly of the spacecraft separation system of CLAMP BAND type	6	343
98	1.1.2016 Solid Rocket Motors Developed by DO-5	20	103
99	21.1.2016 Selection of Optimal Parameters of Wind Desalting System with Hydrogen Energy Storage Unit	15	138
100	20.1.2016 Determination of External Characteristic of Autonomous WPP for Regulation by Rotor Withdrawal from under Wind	19	110
101	19.1.2016 Blade Geometry for Maximal Power Coefficient and Minimal Noise Level	16	103
102	18.1.2016 Method of Design Evaluation of SRM Lifetime and Ensuring its Long-Term Operation	18	90
103	17.1.2016 Modeling of Solid Rocket Motor Starting Process	18	257
104	16.1.2016 Peculiarities of Development of SRM Thrust Vector Controls at DO-5	15	182
105	15.1.2016 Calculation of Solid Propellant Grain Burning Surface Using Automated 3D-Modeling Systems	17	200
106	14.1.2016 Development of Powder Pressure Accumulators for Rocket Cold Start – the Most Important Condition of its Successful Realization	21	109
107	13.1.2016 The Impact of Diaphragm’s Shape on Gas Dynamic Flow Characteristics in Small-Size SRM Combustion Chamber	14	137
108	12.1.2016 Increasing Effectiveness of Meteorological Rockets when Using Hybrid Motors	18	83
109	11.1.2016 Methodology of Design Evaluation of Main SRM Flowrate-Thrust Characteristics after Stage Separation	15	100
110	10.1.2016 Development of Winding Pattern during Calculation of Composite Case Winding Programs	14	178
111	9.1.2016 Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method	20	109
112	8.1.2016 Assessment of Validity of Hypothesis of Constancy of Specific Vacuum Thrust Pulse during SRM Designing and Testing	17	83
113	7.1.2016 Updated Design of SRM Test Rig	18	180
114	6.1.2016 Ensuring Solid Rocket Motor Moisture Resistance by Design	14	289
115	5.1.2016 Scientific-Technical Base for Creation of Detonation Solid Rocket Motors	17	207
116	2.1.2016 Experience of Testing SRM Thrust Vector Controls	17	205
117	4.1.2016 The Company’s Experience in Designing and Operating Special Bench Equipment for SRM Ground Tests	16	97
118	3.1.2016 On Peculiarities of Life Testing and Safe Storage of Solid Rocket Motors	16	257
119	1.2.2016 On Minimal Aerodynamic Resistance of Rotation Body at Zero Angle of Attack in Hypersonic Non-Viscous Flow	19	81
120	2.2.2016 Normalization of Technical System Reliability Using Information Approach	18	75
121	16.2.2016 Method of Coefficient for Optimization and Analysis of Operating State of Fine Filter Cases	18	192
122	15.2.2016 A New Method of Testing Oil-Filled Current Transformers for Explosion-Proofness	16	216
123	14.2.2016 Investigation of Deformability of Carbon Plastic Panels in Moisture Absorption Process	16	489
124	13.2.2016 Experience of Developing Thermometric Instruments Based on Nuclear Quadrupole Resonance	21	187
125	12.2.2016 The Use of Thermoelectric Technologies in Spacecraft Thermostatic Systems	15	223
126	11.2.2016 Experimental Investigation into Power Characteristics of Fast-Flowrate Gas Jet Propulsion Systems	16	136
127	10.2.2016 Mathematical Model of High-Flowrate Electropneumatic Valve	16	120
128	9.2.2016 Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands	22	198
129	8.2.2016 Development and Validation of Program Module for Construction of Virtual Models of Real Structures in ANSYS System	16	109
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	192
131	6.2.2016 Experimental Investigations into Results of Testing Cyclone-4 ILV Thermostating System Mating Points	17	163
132	5.2.2016 Creation of Technological Tooling and Testing of Cocoon-Type Cases Manufacturing Technology	17	223
133	4.2.2016 Experimental Investigations of Possibility of Creating Impulse SRM with Short Operation Period	16	295
134	3.2.2016 Selection of Optimal Trajectories of Spacecraft Launch Vehicles	15	219
135	10.1.2019 Semi-Empirical Evaluation of External Acoustic Loads in Payload Area during Lift-off	16	357
136	9.1.2019 Modeling of Cyclone-4M Rocket Jet Acoustic Emission by Volumetric Source	17	346
137	8.1.2019 Virtual Tests of Cassette Reentry Vehicle Dash Elements Attachment System during Ground Operation	18	394
138	7.1.2019 Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on High-Temperature Propellants	18	231
139	6.1.2019 Investigation into Peculiarities of Delivery to Launch Base of Rocket Propellant with Specified Gasing	13	215
140	5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime	16	292
141	4.1.2019 Mathematic Modeling and Investigation into Stress-Strain State of Space Rocket Bays	18	396
142	3.1.2019 Analysis of Spacecraft Control Issues In Early Design Phases	26	177
143	2.1.2019 Flying Vehicle Maneuvering Dynamics in Atmosphere with Weight Asymmetry and Elements of Terminal Control in Turn Leg	26	193
144	1.1.2019 On 65-th anniversary of the company	19	94
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	15	349
146	26.1.2019 New Technologies and Problems of Their Introducing in Ukraine	19	260
147	25.1.2019 Technological Peculiarities of Manufacturing Products of Irregular Profile by Method of Selective Laser Melting of 316L Powder Metal Material	16	413
148	24.1.2019 Porous Cast Materials (Gasars). Options of Their Use in Space Rocket Hardware	22	334
149	23.1.2019 Calculation of Thermal-Physical Properties of Gaseous Xenon	15	272
150	22.1.2019 Calculation of Uncertainty of Represented Values of Linear Accelerations during Centrifugal Machines Certification	16	272
151	21.1.2019 Optimization of Geometrical Shape of Isolation Valve Blading Position	16	244
152	20.1.2019 Possibilities of Increasing Acting Loads on Hydraulic Actuator Middle Position Lock	18	191
153	19.1.2019 Peculiarities of Radio Transparent Fairings Development	16	251
154	18.1.2019 Designing of Servo Driver of Throttle Mechanisms and Fuel Flow Regulator of ILV Main Motor	18	270
155	17.1.2019 Development of Prospective Small-Size Auxiliary SMR of New Type	16	407
156	16.1.2019 Oscillation Processes in Rig at the Moment of SRM Transfer to Main Operation Mode	16	296
157	15.1.2019 Simulation of SMR Oscillations in Rig that Arise during Firing Bench Test	17	371
158	14.1.2019 Technique of Determination of SRM Operational Life Taking into Account Materials and Elements Strength Margins	17	103
159	13.1.2019 Prediction of Solid Propellant Burnout Time in Launch Vehicle Propulsion System in Flight	19	305
160	12.1.2019 Monitoring of Launch Platform Drift Parameters during Zenit-3SL Integrated Launch Vehicle Prelauch Processing	18	284
161	11.1.2019 Peculiarities of Development Testing of Space Rocket Thermostating System Mating Points Hoses	15	154
162	3.1.2020 Analysis of the unsteady stress-strain behavior of the launch vehicle hold-down bay at liftoff	20	722
163	2.1.2020 Analysis of development trends of design parameters and basic characteristics of missiles for the advanced multiple launch rocket systems	15	1347
164	21.1.2020 Contemporary approaches to the improvement of methods of space launch system operation for commercial launches of ILV	13	376
165	20.1.2020 Studying the possibility of alternating delivery of rocket propellant wastes to a common thermal neutralization facility	16	415
166	19.1.2020 Pyrobolts: types, design, development. Shear type pyrobolt developed at Yuzhnoye SDO	19	866
167	18.1.2020 Development of autonomous power engineering systems with hydrogen energy storage	17	651
168	17.1.2020 Acoustic problems of rocket launch	15	511
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	13	587
170	15.1.2020 Simulation of thermomechanical processes in functionally-gradient materials of inhomogeneous structure in the manufacturing and operation of rocket structural elements	15	790
171	14.1.2020 On the problem of optimum control	16	386
172	13.1.2020 Mathematical models of hydraulic servomechanisms of space technology	11	317
173	12.1.2020 Modification of technology as the main course in the military transport aircraft development	16	411
174	11.1.2020 Some results of strength calculations relying on analytical and FEM approaches. Trends of using contemporary machine learning strategies	17	517
175	10.1.2020 Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM	17	515
176	9.1.2020 Experimental investigation of a liner-free propellant tank made from polymer composite materials	19	825
177	8.1.2020 Determining the main parameters of transport aircraft modifications considering the fuel efficiency	15	298
178	7.1.2020 Studying the motion of a launch vehicle and observed space debris objects during launch preparation	18	410
179	6.1.2020 Mechanics of a satellite cluster. Methods for estimating the probability of their maximal approach in flight	13	361
180	5.1.2020 Strength and stability of inhomogeneous structures of space technology, consid-ering plasticity and creep	18	960
181	4.1.2020 Terminal guidance of the aircraft being maneuvering while descending in the atmosphere under conditions of aerodynamic balancing	18	318
182	1.1.2020 Solving a problem of optimum curves of descent using the enhanced Euler equation	15	523
183	9.1.2023 Methodology for selecting design parameters of solid-propellant sustainer engines. Mathematical support and software	25	473
184	8.1.2023 Specificity of developing pyrobolts with low impact and vibration impulse responses	17	358
185	7.1.2023 Specificity of using rubbers as structural materials for making connector assemblies of temperature conditioning systems	25	287
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	357
187	5.1.2023 Fueling-neutralization stations. New developments and applications	22	314
188	4.1.2023 On control of spacecraft orientation to the ground data acquisition station	17	167
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	513
190	2.1.2023 How Yuzhnoye develops models for flight safety index evaluation for the case of a rocket failure during the flight	19	307
191	1.1.2023 On the development of a methodology for building air and missile defense systems. Explanation of the investigation mechanism	23	385

Visits:101