| 1 | 12.2.2025 Algorithm for filling databases of the automated control system utilized at space rocketry enterprises, considering the differentiation of working and archived information. | 61 | 1712 | 0 | 0 | 0 | 0 | 35849 | 2025 | 2 | 12 |
| 2 | 11.2.2025 Reviewing the benefits of utilizing AL–Mg–Sc alloys in Ukraine’s space rocket industry. Analysis of market factors | 75 | 1551 | 0 | 0 | 0 | 0 | 35846 | 2025 | 2 | 11 |
| 3 | 10.2.2025 Digitalization of design documentation development processes within the enterprise | 66 | 965 | 0 | 0 | 0 | 0 | 35843 | 2025 | 2 | 10 |
| 4 | 9.2.2025 Product quality analysis using methods of statistical study of repair results | 63 | 738 | 0 | 0 | 0 | 0 | 35840 | 2025 | 2 | 9 |
| 5 | 8.2.2025 Specificity of spaceport construction at a lunar base | 57 | 765 | 0 | 0 | 0 | 0 | 35837 | 2025 | 2 | 8 |
| 6 | 7.2.2025 Autonomous deployable landing interface: a detailed technical framework for Mitigating terminal descent risks on planetary surfaces | 58 | 683 | 0 | 0 | 0 | 0 | 35834 | 2025 | 2 | 7 |
| 7 | 6.2.2025 Floating launch platform of a sea-based space launch site | 65 | 972 | 0 | 0 | 0 | 0 | 35831 | 2025 | 2 | 6 |
| 8 | 5.2.2025 Analysis and minimization of resistive forces occurring during rocket stage separation. Possibility of using a single pneumatic pusher for stage separation | 71 | 909 | 0 | 0 | 0 | 0 | 35828 | 2025 | 2 | 5 |
| 9 | 4.2.2025 Thermal decomposition of hydrogen peroxide in the combustion zone of a gas generator. Simulation of the process | 61 | 1490 | 0 | 0 | 0 | 0 | 35825 | 2025 | 2 | 4 |
| 10 | 3.2.2025 Electric thrusters utilizing metal plasma | 74 | 1201 | 0 | 0 | 0 | 0 | 35821 | 2025 | 2 | 3 |
| 11 | 2.2.2025 Performance analysis and validation of a monopropellant air-detonation ramjet engine | 118 | 1557 | 0 | 0 | 0 | 0 | 35818 | 2025 | 2 | 2 |
| 12 | 1.2.2025 Methods for structural strength investigations of rocketry. | 83 | 1713 | 0 | 0 | 0 | 0 | 35812 | 2025 | 2 | 1 |
| 13 | 7.1.2025 Features of the implementation of smart technologies in accounting processes in enterprises in the rocket and space industry | 87 | 609 | 0 | 0 | 0 | 0 | 35491 | 2025 | 1 | 7 |
| 14 | 6.1.2025 Studying the landing of the reusable first stage of the Cyclone-5 space launch vehicle on a maritime landing platform-duplicate-1 | 103 | 1058 | 0 | 0 | 0 | 0 | 35488 | 2025 | 1 | 6 |
| 15 | 5.1.2025 Studying the landing of the reusable first stage of the Cyclone-5 space launch vehicle on a maritime landing platform | 104 | 1423 | 0 | 0 | 0 | 0 | 35485 | 2025 | 1 | 5 |
| 16 | 4.1.2025 Experimental development of a pyrolysis technology for unwinding carbon composites for filler reuse | 96 | 1360 | 0 | 0 | 0 | 0 | 35483 | 2025 | 1 | 4 |
| 17 | 3.1.2025 Experimental research on separation diaphragm performance in propellant storage and feed systems of liquid propellant tanks | 98 | 1873 | 0 | 0 | 0 | 0 | 35481 | 2025 | 1 | 3 |
| 18 | 2.1.2025 Justification of the parameters of a vertical screw conveyor for transporting lunar regolith | 117 | 1536 | 0 | 0 | 0 | 0 | 35479 | 2025 | 1 | 2 |
| 19 | 1.1.2025 Promomoon initiative for moon village generation in honor of dr. Alexander degtyarev | 95 | 1782 | 0 | 0 | 0 | 0 | 35475 | 2025 | 1 | 1 |
| 20 | 16.1.2024 EDUCATIONAL TENDENCIES AS AN ELEMENT OF INNOVATIVE PROGRESS IN THE PERSONNEL TRAINING SYSTEM FOR THE STATE-OF-THE-ART ENTERPRISES | 200 | 2076 | 0 | 0 | 0 | 0 | 34966 | 2024 | 1 | 16 |
| 21 | 15.1.2024 Enhancing operability of the fuel system units in the hot climate conditions | 181 | 4755 | 0 | 0 | 0 | 0 | 34974 | 2024 | 1 | 15 |
| 22 | 14.1.2024 EXPERIMENTAL STUDIES OF THE PERFORMANCE OF PYROTECHNIC DEVICES INSTALLED ON THE LAUNCH VEHICLE SEPARATION SYSTEMS | 172 | 3441 | 1 | 0 | 1 | 0 | 35004 | 2024 | 1 | 14 |
| 23 | 13.1.2024 MODEL OF QUALITY MANAGEMENT OF TECHNICAL PREPARATION FOR THE METAL+COMPOSITE JOINTS PRODUCTION | 187 | 2638 | 0 | 0 | 0 | 0 | 35010 | 2024 | 1 | 13 |
| 24 | 12.1.2024 Hardening of steels modifying their surfaces with ion-plasma nitriding in glow discharge | 225 | 5743 | 0 | 0 | 0 | 0 | 35070 | 2024 | 1 | 12 |
| 25 | 11.1.2024 PARAMETERS CALCULATION OF THE LUNAR REGOLITH TRANSPORT SYSTEM | 202 | 2439 | 1 | 0 | 2 | 0 | 35014 | 2024 | 1 | 11 |
| 26 | 10.1.2024 METHOD OF AUTONOMOUS DETERMINATION OF THE ROCKET’S REFERENCE ATTITUDE DURING PRE-LAUNCH PROCESSING | 222 | 3148 | 0 | 0 | 0 | 0 | 35018 | 2024 | 1 | 10 |
| 27 | 9.1.2024 General-purpose thermostatting module – new approach in development of up-to-date thermostating systems for rocket and space complexes | 201 | 3701 | 0 | 0 | 0 | 0 | 35030 | 2024 | 1 | 9 |
| 28 | 8.1.2024 Theoretic-experimental evaluation of the solid-propellant grain erosive burning | 207 | 1845 | 0 | 0 | 0 | 0 | 35027 | 2024 | 1 | 8 |
| 29 | 7.1.2024 Selection of the functional units for the Cyclone-4M ILV separation system | 224 | 4874 | 0 | 0 | 0 | 0 | 34957 | 2024 | 1 | 7 |
| 30 | 6.1.2024 New methods of load-carrying capacity prediction for the ultimately compressed frame structures | 201 | 3281 | 0 | 0 | 0 | 0 | 34992 | 2024 | 1 | 6 |
| 31 | 5.1.2024 Assessment of risk of toxic damage to people in case of a launch vehicle accident at flight | 206 | 3435 | 0 | 0 | 0 | 0 | 34981 | 2024 | 1 | 5 |
| 32 | 4.1.2024 The dynamics of servo drives | 185 | 2727 | 0 | 0 | 0 | 0 | 34978 | 2024 | 1 | 4 |
| 33 | 3.1.2024 Future projects of lunar exploration implemented by Yuzhnoye SDO | 195 | 1983 | 0 | 0 | 0 | 0 | 34965 | 2024 | 1 | 3 |
| 34 | 2.1.2024 New and advanced liquid rocket engines of the Yuzhnoye SDO | 239 | 3852 | 0 | 0 | 1 | 0 | 34964 | 2024 | 1 | 2 |
| 35 | 1.1.2024 ANTARES: Yuzhnoye’s project of XXI century | 138 | 757 | 0 | 0 | 0 | 0 | 35034 | 2024 | 1 | 1 |
| 36 | 9.1.2023 Methodology for selecting design parameters of solid-propellant sustainer engines. Mathematical support and software | 131 | 3093 | 0 | 0 | 0 | 0 | 26993 | 2023 | 1 | 9 |
| 37 | 8.1.2023 Specificity of developing pyrobolts with low impact and vibration impulse responses | 126 | 2088 | 0 | 0 | 0 | 0 | 26992 | 2023 | 1 | 8 |
| 38 | 7.1.2023 Specificity of using rubbers as structural materials for making connector assemblies of temperature conditioning systems | 157 | 1885 | 0 | 0 | 0 | 0 | 26991 | 2023 | 1 | 7 |
| 39 | 6.1.2023 Numerical modeling of translational and rotational vibrations of a solid-propellant rocket motor on a test stand during firing tests | 127 | 1971 | 0 | 0 | 0 | 0 | 26990 | 2023 | 1 | 6 |
| 40 | 5.1.2023 Fueling-neutralization stations. New developments and applications | 127 | 2146 | 0 | 0 | 0 | 0 | 26989 | 2023 | 1 | 5 |
| 41 | 4.1.2023 On control of spacecraft orientation to the ground data acquisition station | 119 | 1168 | 0 | 0 | 0 | 0 | 26988 | 2023 | 1 | 4 |
| 42 | 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 | 140 | 3099 | 0 | 0 | 0 | 0 | 26987 | 2023 | 1 | 3 |
| 43 | 2.1.2023 How Yuzhnoye develops models for flight safety index evaluation for the case of a rocket failure during the flight | 138 | 2390 | 0 | 0 | 0 | 0 | 26986 | 2023 | 1 | 2 |
| 44 | 1.1.2023 On the development of a methodology for building air and missile defense systems. Explanation of the investigation mechanism | 131 | 3859 | 0 | 0 | 0 | 0 | 26682 | 2023 | 1 | 1 |
| 45 | 21.1.2020 Contemporary approaches to the improvement of methods of space launch system operation for commercial launches of ILV | 160 | 2257 | 0 | 0 | 0 | 0 | 31081 | 2020 | 1 | 21 |
| 46 | 20.1.2020 Studying the possibility of alternating delivery of rocket propellant wastes to a common thermal neutralization facility | 169 | 2510 | 0 | 0 | 0 | 0 | 31078 | 2020 | 1 | 20 |
| 47 | 19.1.2020 Pyrobolts: types, design, development. Shear type pyrobolt developed at Yuzhnoye SDO | 229 | 4052 | 0 | 0 | 0 | 1 | 31074 | 2020 | 1 | 19 |
| 48 | 18.1.2020 Development of autonomous power engineering systems with hydrogen energy storage | 171 | 3905 | 1 | 1 | 1 | 2 | 31056 | 2020 | 1 | 18 |
| 49 | 17.1.2020 Acoustic problems of rocket launch | 162 | 3321 | 0 | 0 | 0 | 0 | 31054 | 2020 | 1 | 17 |
| 50 | 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 | 172 | 4206 | 0 | 0 | 0 | 0 | 31052 | 2020 | 1 | 16 |
| 51 | 15.1.2020 Simulation of thermomechanical processes in functionally-gradient materials of inhomogeneous structure in the manufacturing and operation of rocket structural elements | 179 | 3887 | 0 | 0 | 0 | 0 | 31050 | 2020 | 1 | 15 |
| 52 | 14.1.2020 On the problem of optimum control | 181 | 2623 | 0 | 0 | 0 | 0 | 31048 | 2020 | 1 | 14 |
| 53 | 13.1.2020 Mathematical models of hydraulic servomechanisms of space technology | 170 | 2110 | 0 | 0 | 0 | 0 | 31045 | 2020 | 1 | 13 |
| 54 | 12.1.2020 Modification of technology as the main course in the military transport aircraft development | 197 | 2501 | 2 | 2 | 2 | 0 | 31043 | 2020 | 1 | 12 |
| 55 | 11.1.2020 Some results of strength calculations relying on analytical and FEM approaches. Trends of using contemporary machine learning strategies | 176 | 3122 | 0 | 0 | 0 | 0 | 31040 | 2020 | 1 | 11 |
| 56 | 10.1.2020 Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM | 164 | 3482 | 0 | 0 | 0 | 0 | 31037 | 2020 | 1 | 10 |
| 57 | 9.1.2020 Experimental investigation of a liner-free propellant tank made from polymer composite materials | 173 | 3974 | 1 | 1 | 1 | 6 | 31035 | 2020 | 1 | 9 |
| 58 | 8.1.2020 Determining the main parameters of transport aircraft modifications considering the fuel efficiency | 163 | 1311 | 0 | 0 | 0 | 0 | 31033 | 2020 | 1 | 8 |
| 59 | 7.1.2020 Studying the motion of a launch vehicle and observed space debris objects during launch preparation | 170 | 2291 | 0 | 0 | 0 | 0 | 31031 | 2020 | 1 | 7 |
| 60 | 6.1.2020 Mechanics of a satellite cluster. Methods for estimating the probability of their maximal approach in flight | 166 | 2068 | 0 | 0 | 0 | 0 | 31028 | 2020 | 1 | 6 |
| 61 | 5.1.2020 Strength and stability of inhomogeneous structures of space technology, consid-ering plasticity and creep | 186 | 5618 | 0 | 0 | 0 | 0 | 31026 | 2020 | 1 | 5 |
| 62 | 4.1.2020 Terminal guidance of the aircraft being maneuvering while descending in the atmosphere under conditions of aerodynamic balancing | 157 | 1883 | 1 | 0 | 2 | 0 | 31024 | 2020 | 1 | 4 |
| 63 | 3.1.2020 Analysis of the unsteady stress-strain behavior of the launch vehicle hold-down bay at liftoff | 199 | 4061 | 0 | 0 | 0 | 0 | 32230 | 2020 | 1 | 3 |
| 64 | 2.1.2020 Analysis of development trends of design parameters and basic characteristics of missiles for the advanced multiple launch rocket systems | 183 | 8036 | 2 | 2 | 1 | 0 | 31001 | 2020 | 1 | 2 |
| 65 | 1.1.2020 Solving a problem of optimum curves of descent using the enhanced Euler equation | 169 | 3674 | 0 | 0 | 0 | 0 | 27120 | 2020 | 1 | 1 |
| 66 | 14.2.2019 Selection of the validation algorithm for the solid rocket motor trust measurement procedure | 188 | 1846 | 0 | 0 | 0 | 0 | 27216 | 2019 | 2 | 14 |
| 67 | 13.2.2019 Study of the stress and strain state of the multilayer bellows | 177 | 1887 | 0 | 0 | 0 | 0 | 27215 | 2019 | 2 | 13 |
| 68 | 12.2.2019 Procedure of acoustic loads measuring during the ILV launch | 169 | 1283 | 0 | 0 | 0 | 0 | 27214 | 2019 | 2 | 12 |
| 69 | 11.2.2019 Winding the tubes of rectangular section using dowels | 167 | 1677 | 0 | 0 | 0 | 0 | 27213 | 2019 | 2 | 11 |
| 70 | 10.2.2019 Dynamic performance of the gas drive with jet motor | 182 | 4412 | 0 | 0 | 0 | 0 | 32366 | 2019 | 2 | 10 |
| 71 | 9.2.2019 Gas-dynamic simulation of the supersonic stream in the pulsed wind tunnel | 183 | 2440 | 0 | 0 | 0 | 0 | 27211 | 2019 | 2 | 9 |
| 72 | 8.2.2019 Evaluation of the external acoustic loads, acting on the rocket when it passes the leg with maximum velocity head | 184 | 755 | 1 | 1 | 1 | 0 | 27210 | 2019 | 2 | 8 |
| 73 | 7.2.2019 On critical stress of the longitudinal stability of the stiffened cylindrical shells. Dynamic problem | 163 | 1054 | 0 | 0 | 0 | 0 | 27209 | 2019 | 2 | 7 |
| 74 | 6.2.2019 Stabilization of gas reducers adjustment | 182 | 1704 | 0 | 0 | 0 | 1 | 27208 | 2019 | 2 | 6 |
| 75 | 5.2.2019 Features of the development testing of the propellants deposition inside the tanks of launch vehicles | 174 | 1643 | 1 | 1 | 0 | 0 | 27207 | 2019 | 2 | 5 |
| 76 | 4.2.2019 Numerical simulation of behavior of elastic structures with local stiffening elementse | 168 | 1380 | 1 | 0 | 1 | 0 | 27206 | 2019 | 2 | 4 |
| 77 | 3.2.2019 Features of design and production of the technological aids for assembly of the spacecraft separation system of CLAMP BAND type | 153 | 2240 | 0 | 0 | 0 | 0 | 27205 | 2019 | 2 | 3 |
| 78 | 2.2.2019 Mathematical models for assessment of safety in the impact area of cluster ammunition of the warhead during missile complex testing | 176 | 3103 | 0 | 0 | 0 | 1 | 27204 | 2019 | 2 | 2 |
| 79 | 1.2.2019 Optimization of the trajectory of the antiaircraft guided missile | 186 | 4517 | 0 | 0 | 0 | 4 | 28723 | 2019 | 2 | 1 |
| 80 | 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 | 153 | 1767 | 0 | 0 | 0 | 0 | 27732 | 2019 | 1 | 27 |
| 81 | 26.1.2019 New Technologies and Problems of Their Introducing in Ukraine | 160 | 1606 | 0 | 0 | 0 | 0 | 27731 | 2019 | 1 | 26 |
| 82 | 25.1.2019 Technological Peculiarities of Manufacturing Products of Irregular Profile by Method of Selective Laser Melting of 316L Powder Metal Material | 154 | 2211 | 0 | 0 | 0 | 102 | 27730 | 2019 | 1 | 25 |
| 83 | 24.1.2019 Porous Cast Materials (Gasars). Options of Their Use in Space Rocket Hardware | 181 | 2341 | 0 | 0 | 0 | 0 | 27729 | 2019 | 1 | 24 |
| 84 | 23.1.2019 Calculation of Thermal-Physical Properties of Gaseous Xenon | 160 | 1832 | 1 | 1 | 1 | 0 | 27728 | 2019 | 1 | 23 |
| 85 | 22.1.2019 Calculation of Uncertainty of Represented Values of Linear Accelerations during Centrifugal Machines Certification | 155 | 1666 | 0 | 0 | 0 | 0 | 27727 | 2019 | 1 | 22 |
| 86 | 21.1.2019 Optimization of Geometrical Shape of Isolation Valve Blading Position | 161 | 1341 | 0 | 0 | 0 | 0 | 27726 | 2019 | 1 | 21 |
| 87 | 20.1.2019 Possibilities of Increasing Acting Loads on Hydraulic Actuator Middle Position Lock | 157 | 1372 | 0 | 0 | 0 | 0 | 27725 | 2019 | 1 | 20 |
| 88 | 19.1.2019 Peculiarities of Radio Transparent Fairings Development | 211 | 1723 | 2 | 2 | 2 | 2 | 27724 | 2019 | 1 | 19 |
| 89 | 18.1.2019 Designing of Servo Driver of Throttle Mechanisms and Fuel Flow Regulator of ILV Main Motor | 170 | 1710 | 0 | 0 | 0 | 0 | 27723 | 2019 | 1 | 18 |
| 90 | 17.1.2019 Development of Prospective Small-Size Auxiliary SMR of New Type | 165 | 2329 | 0 | 0 | 0 | 0 | 27722 | 2019 | 1 | 17 |
| 91 | 16.1.2019 Oscillation Processes in Rig at the Moment of SRM Transfer to Main Operation Mode | 161 | 1427 | 0 | 0 | 0 | 0 | 27721 | 2019 | 1 | 16 |
| 92 | 15.1.2019 Simulation of SMR Oscillations in Rig that Arise during Firing Bench Test | 176 | 2476 | 0 | 0 | 0 | 0 | 27720 | 2019 | 1 | 15 |
| 93 | 14.1.2019 Technique of Determination of SRM Operational Life Taking into Account Materials and Elements Strength Margins | 166 | 753 | 0 | 0 | 0 | 0 | 27719 | 2019 | 1 | 14 |
| 94 | 13.1.2019 Prediction of Solid Propellant Burnout Time in Launch Vehicle Propulsion System in Flight | 168 | 2065 | 0 | 0 | 0 | 0 | 27718 | 2019 | 1 | 13 |
| 95 | 12.1.2019 Monitoring of Launch Platform Drift Parameters during Zenit-3SL Integrated Launch Vehicle Prelauch Processing | 153 | 1875 | 1 | 1 | 1 | 0 | 27717 | 2019 | 1 | 12 |
| 96 | 11.1.2019 Peculiarities of Development Testing of Space Rocket Thermostating System Mating Points Hoses | 171 | 1125 | 0 | 0 | 0 | 0 | 27716 | 2019 | 1 | 11 |
| 97 | 10.1.2019 Semi-Empirical Evaluation of External Acoustic Loads in Payload Area during Lift-off | 170 | 2153 | 1 | 1 | 1 | 0 | 27715 | 2019 | 1 | 10 |
| 98 | 9.1.2019 Modeling of Cyclone-4M Rocket Jet Acoustic Emission by Volumetric Source | 179 | 2034 | 0 | 0 | 0 | 2 | 27714 | 2019 | 1 | 9 |
| 99 | 8.1.2019 Virtual Tests of Cassette Reentry Vehicle Dash Elements Attachment System during Ground Operation | 186 | 2473 | 0 | 0 | 0 | 0 | 27713 | 2019 | 1 | 8 |
| 100 | 7.1.2019 Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on High-Temperature Propellants | 179 | 1124 | 2 | 1 | 1 | 0 | 27712 | 2019 | 1 | 7 |
| 101 | 6.1.2019 Investigation into Peculiarities of Delivery to Launch Base of Rocket Propellant with Specified Gasing | 179 | 1700 | 1 | 1 | 1 | 0 | 27711 | 2019 | 1 | 6 |
| 102 | 5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime | 189 | 2097 | 0 | 0 | 0 | 0 | 27710 | 2019 | 1 | 5 |
| 103 | 4.1.2019 Mathematic Modeling and Investigation into Stress-Strain State of Space Rocket Bays | 175 | 2247 | 4 | 3 | 4 | 0 | 27709 | 2019 | 1 | 4 |
| 104 | 3.1.2019 Analysis of Spacecraft Control Issues In Early Design Phases | 194 | 1625 | 0 | 0 | 0 | 0 | 27708 | 2019 | 1 | 3 |
| 105 | 2.1.2019 Flying Vehicle Maneuvering Dynamics in Atmosphere with Weight Asymmetry and Elements of Terminal Control in Turn Leg | 171 | 1506 | 1 | 1 | 1 | 0 | 27707 | 2019 | 1 | 2 |
| 106 | 1.1.2019 On 65-th anniversary of the company | 156 | 678 | 0 | 0 | 0 | 0 | 27703 | 2019 | 1 | 1 |
| 107 | 23.2.2018 On the Role of Space in Origination of Inertia Force Field, Earth Gravity Force Field and Zero Gravity of Material Body | 174 | 2835 | 0 | 0 | 0 | 0 | 30813 | 2018 | 2 | 23 |
| 108 | 22.2.2018 Uncertainty Calculation Procedure during Measuring Instrumentation Calibration | 176 | 4065 | 0 | 0 | 0 | 0 | 30810 | 2018 | 2 | 22 |
| 109 | 21.2.2018 Ensuring Aiming Accuracy of Ship’s Telemetry Reception Antenna Installation for Small Vessels | 143 | 2371 | 0 | 0 | 0 | 0 | 30807 | 2018 | 2 | 21 |
| 110 | 20.2.2018 The Use of Special Devices during Launch Pad Development Testing | 164 | 2012 | 0 | 0 | 0 | 0 | 30805 | 2018 | 2 | 20 |
| 111 | 19.2.2018 Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles | 165 | 2663 | 0 | 0 | 0 | 0 | 30801 | 2018 | 2 | 19 |
| 112 | 18.2.2018 Angular Stabilization of an Object Rapidly Rotating around Longitudial Axis | 170 | 2258 | 0 | 0 | 0 | 0 | 30799 | 2018 | 2 | 18 |
| 113 | 17.2.2018 Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine | 185 | 1667 | 0 | 0 | 0 | 0 | 30796 | 2018 | 2 | 17 |
| 114 | 16.2.2018 Design Solutions to Prevent Propellant Ingress into SRM Case Space behind Sealing Ring | 267 | 2724 | 0 | 0 | 0 | 0 | 30792 | 2018 | 2 | 16 |
| 115 | 15.2.2018 Topical Issues of Creation of Space Rocket Thermostatic System Mating Points | 172 | 1530 | 1 | 1 | 1 | 0 | 30786 | 2018 | 2 | 15 |
| 116 | 14.2.2018 A Concept of Modular Transport Vehicle for Lunar Program | 168 | 1759 | 0 | 0 | 0 | 0 | 30780 | 2018 | 2 | 14 |
| 117 | 13.2.2018 On an Approach to Constructing the Extremes in the Tasks of Optimal Solutions Search | 154 | 1250 | 0 | 0 | 0 | 0 | 30778 | 2018 | 2 | 13 |
| 118 | 12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs | 165 | 2178 | 6 | 5 | 6 | 2 | 30770 | 2018 | 2 | 12 |
| 119 | 11.2.2018 Some Peculiarities of Ensuring LRE Guarantied Service Life in the Conditions of Replacement of Components of Interindustry Application | 152 | 2148 | 0 | 0 | 0 | 0 | 30768 | 2018 | 2 | 11 |
| 120 | 10.2.2018 Calculation of Gas Flow in High-Altitude Engine Nozzle and Experience of Using Water-Cooled Nozzle Head during Tests | 167 | 3177 | 0 | 0 | 0 | 0 | 30766 | 2018 | 2 | 10 |
| 121 | 9.2.2018 The Impact of Worm Design on Power and Anti-Cavitation Properties of Worm-Centrifugal Pumps | 169 | 3473 | 0 | 0 | 0 | 0 | 30763 | 2018 | 2 | 9 |
| 122 | 8.2.2018 Development of Nozzle Blocks New Manufacturing Technology without Blazing | 178 | 2572 | 3 | 2 | 2 | 0 | 30757 | 2018 | 2 | 8 |
| 123 | 7.2.2018 Theoretical Models of Sound Speed Increase Effects in Gas Duct with Corrugated Wall | 183 | 3233 | 0 | 0 | 0 | 0 | 30754 | 2018 | 2 | 7 |
| 124 | 6.2.2018 Introduction of Additive Technologies for LRE Parts Manufacturing | 153 | 2333 | 0 | 0 | 0 | 0 | 30751 | 2018 | 2 | 6 |
| 125 | 5.2.2018 Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office | 187 | 3389 | 1 | 1 | 1 | 0 | 30749 | 2018 | 2 | 5 |
| 126 | 4.2.2018 Turbopump Units of Rocket Engines Developed by DO-4 | 190 | 1255 | 1 | 1 | 1 | 0 | 30735 | 2018 | 2 | 4 |
| 127 | 3.2.2018 Possible Ways of Modernization of VEGA Launch Vehicle AVUM Stage Main Engine Assembly | 175 | 3071 | 0 | 0 | 0 | 0 | 30733 | 2018 | 2 | 3 |
| 128 | 2.2.2018 Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines | 203 | 1377 | 0 | 0 | 0 | 0 | 30729 | 2018 | 2 | 2 |
| 129 | 1.2.2018 Design Office of Liquid Rocket Engines is 60 | 176 | 858 | 0 | 0 | 0 | 0 | 30723 | 2018 | 2 | 1 |
| 130 | 16.1.2018 Some Correlation Dependences in Families of Aton and Apollo and Rendezvous Frequency in Main Asteroid Belt | 147 | 1281 | 0 | 0 | 0 | 0 | 30477 | 2018 | 1 | 16 |
| 131 | 15.1.2018 The Results of Using Automated Methods to Solve Standardization Tasks in Yuzhnoye SDO Practice | 164 | 2279 | 0 | 0 | 0 | 0 | 30474 | 2018 | 1 | 15 |
| 132 | 14.1.2018 A Rectangular Section Pipes Winding Programs Calculation Procedure | 153 | 1970 | 0 | 0 | 0 | 0 | 30472 | 2018 | 1 | 14 |
| 133 | 13.1.2018 On Selection of Materials for Creation of Modern LV Thermostating System Mating Hoses | 177 | 2139 | 2 | 2 | 2 | 0 | 30469 | 2018 | 1 | 13 |
| 134 | 12.1.2018 A Device for Soft Separation of Spacecraft from Launch Vehicle | 165 | 2164 | 0 | 0 | 0 | 0 | 30464 | 2018 | 1 | 12 |
| 135 | 11.1.2018 Ensuring Long Lifetime of the Electrochemical Accumulators Included in Space Rocketry Electric Power Supply Systems | 180 | 2116 | 0 | 0 | 0 | 0 | 30466 | 2018 | 1 | 11 |
| 136 | 10.1.2018 The Rocket Propellant Vapors and Water Solutions Neutralization Units. The Accumulated Experience and Prospects of Updating the Neutralization Units | 182 | 1652 | 0 | 0 | 0 | 0 | 30462 | 2018 | 1 | 10 |
| 137 | 9.1.2018 On the Peculiarities of High-Temperature Rocket Propellants Drain from Delivery Means to Filling Tank for Closed Drain | 179 | 2183 | 0 | 0 | 0 | 0 | 30460 | 2018 | 1 | 9 |
| 138 | 8.1.2018 The Solid–Propellant Motors with Regulated Thrust | 187 | 2399 | 1 | 0 | 1 | 1 | 30458 | 2018 | 1 | 8 |
| 139 | 7.1.2018 Prospective Gas Purification Device for LRE Test Bench | 170 | 1311 | 0 | 0 | 0 | 0 | 30456 | 2018 | 1 | 7 |
| 140 | 6.1.2018 On Building of Inertial Navigation System in the Condition of Presence of Considerable g-Load and Angular Velocity in Preferential Direction | 186 | 1945 | 0 | 0 | 0 | 0 | 30454 | 2018 | 1 | 6 |
| 141 | 5.1.2018 Experimental Determination of Lateral Force Caused by SRM Thrust Vector Eccentricity and Skew | 165 | 2960 | 0 | 0 | 0 | 0 | 30421 | 2018 | 1 | 5 |
| 142 | 4.1.2018 Determination of Angular Acceleration of Rotary Elements of Rocket Systems during Ground Tests | 165 | 1476 | 0 | 0 | 0 | 0 | 30411 | 2018 | 1 | 4 |
| 143 | 3.1.2018 The Means of Functional Suppression of Radio Electronic Facilities of Small-Size Unmanned Aerial Vehicles with Electromagnetic Radiation Focusing | 175 | 2278 | 0 | 0 | 0 | 0 | 30408 | 2018 | 1 | 3 |
| 144 | 2.1.2018 Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop | 180 | 2016 | 0 | 0 | 0 | 0 | 30403 | 2018 | 1 | 2 |
| 145 | 1.1.2018 Modernization and Automation of Temperature Calculation of Measurement Errors of Climatic Chambers for Accelerated Environmental Tests | 170 | 2304 | 0 | 0 | 0 | 0 | 30158 | 2018 | 1 | 1 |
| 146 | 27.2.2017 Solution of “Unsolvable” Problems | 156 | 972 | 0 | 0 | 0 | 0 | 29966 | 2017 | 2 | 27 |
| 147 | 26.2.2017 State of the Art and Prospects for Nuclear-Quadrupole Resonance Thermometry in Ukraine | 177 | 3059 | 0 | 0 | 0 | 0 | 29962 | 2017 | 2 | 26 |
| 148 | 25.2.2017 Vacuum Conditions Simulation Criteria | 172 | 1300 | 0 | 0 | 0 | 0 | 29958 | 2017 | 2 | 25 |
| 149 | 24.2.2017 Method of Supercooled Cryogenic Liquid Production | 179 | 913 | 0 | 0 | 0 | 0 | 29954 | 2017 | 2 | 24 |
| 150 | 23.2.2017 Optimization Technique for Mass of Locally Loaded Rocket Bays with Wafer Structure | 161 | 2552 | 0 | 0 | 0 | 0 | 29948 | 2017 | 2 | 23 |
| 151 | 22.2.2017 Advanced Aluminum Alloys for Launch Vehicle Pipeline Parts Manufacture | 158 | 1581 | 0 | 0 | 0 | 0 | 29944 | 2017 | 2 | 22 |
| 152 | 21.2.2017 Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft | 167 | 1303 | 0 | 0 | 0 | 0 | 29940 | 2017 | 2 | 21 |
| 153 | 20.2.2017 Research Support for Development of Launch Vehicle Payload Unit Composite Load-Bearing Compartments | 168 | 3067 | 0 | 0 | 0 | 0 | 29866 | 2017 | 2 | 20 |
| 154 | 19.2.2017 Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation | 171 | 885 | 0 | 0 | 0 | 0 | 29862 | 2017 | 2 | 19 |
| 155 | 18.2.2017 Development Test of Payload Fairing Separation Dynamics under Ground Conditions | 176 | 1143 | 0 | 0 | 0 | 0 | 29858 | 2017 | 2 | 18 |
| 156 | 17.2.2017 Development Test of Spacecraft Separation Dynamics under Ground Conditions | 172 | 1224 | 0 | 0 | 0 | 0 | 29854 | 2017 | 2 | 17 |
| 157 | 16.2.2017 Determination of Spherical Flange Connections Gasket Clamping Site Width | 178 | 724 | 0 | 0 | 0 | 0 | 29850 | 2017 | 2 | 16 |
| 158 | 15.2.2017 Oxidizer Feedline Structural Optimization Results | 171 | 1852 | 0 | 0 | 0 | 0 | 29846 | 2017 | 2 | 15 |
| 159 | 14.2.2017 Development Test of Isolating Valve Operation under Cryogenic Conditions | 164 | 983 | 0 | 0 | 0 | 0 | 29842 | 2017 | 2 | 14 |
| 160 | 13.2.2017 Experience in Development of Isolating Fuel Valve with Pneumatic Drive and Hydraulic Brake for Operation under Cryogenic Conditions | 162 | 2251 | 0 | 0 | 0 | 0 | 29836 | 2017 | 2 | 13 |
| 161 | 12.2.2017 Determination Procedure for Pneudraulic System and Its Components No-Failure Operation Probability | 162 | 1302 | 0 | 0 | 0 | 0 | 29785 | 2017 | 2 | 12 |
| 162 | 11.2.2017 Remote Monitoring Method of Pneudraulic System Structural Elements Integrity | 162 | 1784 | 0 | 0 | 0 | 0 | 29781 | 2017 | 2 | 11 |
| 163 | 10.2.2017 Analysis Method of Hydraulic Parameters of Circular Intake Device in Limit Operating Modes | 166 | 2631 | 0 | 0 | 0 | 0 | 29771 | 2017 | 2 | 10 |
| 164 | 9.2.2017 Peculiarities of Development of Cryogenic Propulsion System Circulating Cooling System | 167 | 1615 | 0 | 0 | 0 | 0 | 29767 | 2017 | 2 | 9 |
| 165 | 8.2.2017 Analysis Method of Nitrogen Tetroxide Tanks Generating Pressurization Systems | 158 | 769 | 0 | 0 | 0 | 0 | 29763 | 2017 | 2 | 8 |
| 166 | 7.2.2017 Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants | 171 | 1570 | 0 | 0 | 0 | 0 | 29758 | 2017 | 2 | 7 |
| 167 | 6.2.2017 Set of Actions on Enhancement of Launch Vehicle Payload Capability | 175 | 1371 | 0 | 0 | 0 | 0 | 29754 | 2017 | 2 | 6 |
| 168 | 5.2.2017 Structural Perfection of Cyclone-4 Integrated Launch Vehicle | 155 | 1024 | 0 | 0 | 0 | 0 | 29750 | 2017 | 2 | 5 |
| 169 | 4.2.2017 Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics | 160 | 785 | 0 | 0 | 0 | 0 | 29746 | 2017 | 2 | 4 |
| 170 | 3.2.2017 Creation of Advanced Facilities for Spacecraft / Launch Vehicle Integration | 163 | 675 | 0 | 0 | 0 | 0 | 29739 | 2017 | 2 | 3 |
| 171 | 2.2.2017 Creation of Universal System of Launch Vehicle Space Head Modules for Cluster Spacecraft Missions | 182 | 1428 | 0 | 0 | 0 | 0 | 29649 | 2017 | 2 | 2 |
| 172 | 1.2.2017 DO-2 – Semicentenary | 153 | 698 | 0 | 0 | 0 | 0 | 30174 | 2017 | 2 | 1 |
| 173 | 17.1.2017 Peculiarities of Design and Development Test of Dispenser Turning Actuator System for SHM with Iridium NEXT SC | 166 | 1910 | 0 | 0 | 0 | 0 | 29518 | 2017 | 1 | 17 |
| 174 | 16.1.2017 Principal Directions for Creation of Integrated Launch Vehicle Autonomous Onboard Flight Safety System | 154 | 2483 | 0 | 0 | 0 | 0 | 29514 | 2017 | 1 | 16 |
| 175 | 15.1.2017 Assessment of Liquid Equipment Neutralization Method Effectiveness | 155 | 1160 | 0 | 0 | 0 | 0 | 29505 | 2017 | 1 | 15 |
| 176 | 14.1.2017 Design Studies into Dynamic and Structural Characteristics of Two-Stage Direct-Action Solenoid-Operated Hydraulic Valve | 156 | 1262 | 0 | 0 | 0 | 0 | 29497 | 2017 | 1 | 14 |
| 177 | 13.1.2017 Reliability Evaluation of ILV Thermostating System Mating Hoses | 158 | 2272 | 0 | 0 | 0 | 0 | 29483 | 2017 | 1 | 13 |
| 178 | 12.1.2017 Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator | 165 | 1858 | 0 | 0 | 0 | 0 | 31702 | 2017 | 1 | 12 |
| 179 | 11.1.2017 Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors | 170 | 1178 | 0 | 0 | 0 | 0 | 29442 | 2017 | 1 | 11 |
| 180 | 10.1.2017 Features of Measurement System for Gas-Dynamic Model Tests of Rocket Complex Elements | 156 | 1367 | 0 | 0 | 0 | 0 | 29438 | 2017 | 1 | 10 |
| 181 | 9.1.2017 Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles | 159 | 1770 | 0 | 0 | 0 | 0 | 29434 | 2017 | 1 | 9 |
| 182 | 8.1.2017 Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions | 159 | 1358 | 0 | 0 | 0 | 0 | 29430 | 2017 | 1 | 8 |
| 183 | 7.1.2017 Static Approach Application in Analysis of Gas-Dynamic Parameters in Launch Vehicle Vented Bays | 144 | 1127 | 0 | 0 | 0 | 0 | 29425 | 2017 | 1 | 7 |
| 184 | 6.1.2017 Drought Post-Effects Satellite Monitoring | 156 | 2404 | 0 | 0 | 0 | 0 | 29420 | 2017 | 1 | 6 |
| 185 | 5.1.2017 Development of Working Liquid Discontinuity Measurement Procedure and Its Certification | 156 | 1296 | 0 | 0 | 0 | 0 | 29374 | 2017 | 1 | 5 |
| 186 | 4.1.2017 Basic Selection Criteria of Heat-Resistant and Thermal Protective Structures for High-Altitude Hypersonic Flying Vehicle | 154 | 1628 | 0 | 0 | 0 | 0 | 29370 | 2017 | 1 | 4 |
| 187 | 3.1.2017 Development Strength Test of Modified Antares ILV | 160 | 1317 | 0 | 0 | 0 | 0 | 29366 | 2017 | 1 | 3 |
| 188 | 2.1.2017 Ultimate Stability Stresses in Smooth Cylindrical Skins. Dynamic Problem | 153 | 1105 | 0 | 0 | 0 | 0 | 29361 | 2017 | 1 | 2 |
| 189 | 1.1.2017 Methodology for Measurement Uncertainty Evaluation during Metrological Certification of Measuring Instruments | 160 | 1067 | 0 | 0 | 0 | 0 | 29354 | 2017 | 1 | 1 |
| 190 | 16.2.2016 Method of Coefficient for Optimization and Analysis of Operating State of Fine Filter Cases | 146 | 999 | 0 | 0 | 0 | 0 | 28333 | 2016 | 2 | 16 |
| 191 | 15.2.2016 A New Method of Testing Oil-Filled Current Transformers for Explosion-Proofness | 159 | 1368 | 0 | 0 | 0 | 0 | 28331 | 2016 | 2 | 15 |
| 192 | 14.2.2016 Investigation of Deformability of Carbon Plastic Panels in Moisture Absorption Process | 162 | 2715 | 0 | 0 | 0 | 0 | 28329 | 2016 | 2 | 14 |
| 193 | 13.2.2016 Experience of Developing Thermometric Instruments Based on Nuclear Quadrupole Resonance | 168 | 892 | 0 | 0 | 0 | 0 | 28327 | 2016 | 2 | 13 |
| 194 | 12.2.2016 The Use of Thermoelectric Technologies in Spacecraft Thermostatic Systems | 160 | 1374 | 0 | 0 | 0 | 0 | 28325 | 2016 | 2 | 12 |
| 195 | 11.2.2016 Experimental Investigation into Power Characteristics of Fast-Flowrate Gas Jet Propulsion Systems | 151 | 787 | 0 | 0 | 0 | 0 | 28323 | 2016 | 2 | 11 |
| 196 | 10.2.2016 Mathematical Model of High-Flowrate Electropneumatic Valve | 169 | 940 | 0 | 0 | 0 | 0 | 28321 | 2016 | 2 | 10 |
| 197 | 9.2.2016 Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands | 178 | 1120 | 0 | 0 | 0 | 0 | 28319 | 2016 | 2 | 9 |
| 198 | 8.2.2016 Development and Validation of Program Module for Construction of Virtual Models of Real Structures in ANSYS System | 135 | 775 | 0 | 0 | 0 | 0 | 28316 | 2016 | 2 | 8 |
| 199 | 7.2.2016 Analysis of Operation Modes and Selection of Chemical Current Source Included in Autonomous Electric Power Supply Systems of Self-Propelled Launcher | 161 | 957 | 0 | 0 | 0 | 0 | 28314 | 2016 | 2 | 7 |
| 200 | 6.2.2016 Experimental Investigations into Results of Testing Cyclone-4 ILV Thermostating System Mating Points | 164 | 653 | 0 | 0 | 0 | 0 | 28312 | 2016 | 2 | 6 |
| 201 | 5.2.2016 Creation of Technological Tooling and Testing of Cocoon-Type Cases Manufacturing Technology | 160 | 1464 | 0 | 0 | 0 | 0 | 28310 | 2016 | 2 | 5 |
| 202 | 4.2.2016 Experimental Investigations of Possibility of Creating Impulse SRM with Short Operation Period | 158 | 2069 | 0 | 0 | 0 | 0 | 28308 | 2016 | 2 | 4 |
| 203 | 3.2.2016 Selection of Optimal Trajectories of Spacecraft Launch Vehicles | 160 | 1233 | 0 | 0 | 0 | 0 | 28306 | 2016 | 2 | 3 |
| 204 | 2.2.2016 Normalization of Technical System Reliability Using Information Approach | 154 | 608 | 0 | 0 | 0 | 0 | 28304 | 2016 | 2 | 2 |
| 205 | 1.2.2016 On Minimal Aerodynamic Resistance of Rotation Body at Zero Angle of Attack in Hypersonic Non-Viscous Flow | 165 | 655 | 0 | 0 | 0 | 0 | 28016 | 2016 | 2 | 1 |
| 206 | 21.1.2016 Selection of Optimal Parameters of Wind Desalting System with Hydrogen Energy Storage Unit | 139 | 951 | 0 | 0 | 0 | 0 | 27643 | 2016 | 1 | 21 |
| 207 | 20.1.2016 Determination of External Characteristic of Autonomous WPP for Regulation by Rotor Withdrawal from under Wind | 156 | 1012 | 0 | 0 | 0 | 0 | 27641 | 2016 | 1 | 20 |
| 208 | 19.1.2016 Blade Geometry for Maximal Power Coefficient and Minimal Noise Level | 146 | 609 | 0 | 0 | 0 | 0 | 27639 | 2016 | 1 | 19 |
| 209 | 18.1.2016 Method of Design Evaluation of SRM Lifetime and Ensuring its Long-Term Operation | 184 | 904 | 0 | 0 | 0 | 0 | 27637 | 2016 | 1 | 18 |
| 210 | 17.1.2016 Modeling of Solid Rocket Motor Starting Process | 160 | 2067 | 0 | 0 | 0 | 0 | 27635 | 2016 | 1 | 17 |
| 211 | 16.1.2016 Peculiarities of Development of SRM Thrust Vector Controls at DO-5 | 134 | 961 | 0 | 0 | 0 | 0 | 27633 | 2016 | 1 | 16 |
| 212 | 15.1.2016 Calculation of Solid Propellant Grain Burning Surface Using Automated 3D-Modeling Systems | 162 | 1487 | 0 | 0 | 0 | 0 | 27631 | 2016 | 1 | 15 |
| 213 | 14.1.2016 Development of Powder Pressure Accumulators for Rocket Cold Start – the Most Important Condition of its Successful Realization | 167 | 888 | 0 | 0 | 0 | 0 | 27629 | 2016 | 1 | 14 |
| 214 | 13.1.2016 The Impact of Diaphragm’s Shape on Gas Dynamic Flow Characteristics in Small-Size SRM Combustion Chamber | 144 | 921 | 0 | 0 | 0 | 0 | 27627 | 2016 | 1 | 13 |
| 215 | 12.1.2016 Increasing Effectiveness of Meteorological Rockets when Using Hybrid Motors | 146 | 729 | 0 | 0 | 0 | 0 | 27624 | 2016 | 1 | 12 |
| 216 | 11.1.2016 Methodology of Design Evaluation of Main SRM Flowrate-Thrust Characteristics after Stage Separation | 154 | 996 | 0 | 0 | 0 | 0 | 27621 | 2016 | 1 | 11 |
| 217 | 10.1.2016 Development of Winding Pattern during Calculation of Composite Case Winding Programs | 149 | 1071 | 0 | 0 | 0 | 0 | 27619 | 2016 | 1 | 10 |
| 218 | 9.1.2016 Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method | 151 | 722 | 0 | 0 | 0 | 0 | 27617 | 2016 | 1 | 9 |
| 219 | 8.1.2016 Assessment of Validity of Hypothesis of Constancy of Specific Vacuum Thrust Pulse during SRM Designing and Testing | 149 | 1010 | 0 | 0 | 0 | 0 | 27614 | 2016 | 1 | 8 |
| 220 | 7.1.2016 Updated Design of SRM Test Rig | 159 | 1006 | 0 | 0 | 0 | 0 | 27612 | 2016 | 1 | 7 |
| 221 | 6.1.2016 Ensuring Solid Rocket Motor Moisture Resistance by Design | 134 | 1744 | 0 | 0 | 0 | 0 | 27610 | 2016 | 1 | 6 |
| 222 | 5.1.2016 Scientific-Technical Base for Creation of Detonation Solid Rocket Motors | 137 | 1394 | 0 | 0 | 0 | 0 | 27608 | 2016 | 1 | 5 |
| 223 | 4.1.2016 The Company’s Experience in Designing and Operating Special Bench Equipment for SRM Ground Tests | 141 | 659 | 0 | 0 | 0 | 0 | 27605 | 2016 | 1 | 4 |
| 224 | 3.1.2016 On Peculiarities of Life Testing and Safe Storage of Solid Rocket Motors | 155 | 1826 | 0 | 0 | 0 | 0 | 27602 | 2016 | 1 | 3 |
| 225 | 2.1.2016 Experience of Testing SRM Thrust Vector Controls | 145 | 1391 | 0 | 0 | 0 | 0 | 27600 | 2016 | 1 | 2 |
| 226 | 1.1.2016 Solid Rocket Motors Developed by DO-5 | 183 | 891 | 0 | 0 | 0 | 0 | 27589 | 2016 | 1 | 1 |
