6.2.2017 Set of Actions on Enhancement of Launch Vehicle Payload Capability

Set of Actions on Enhancement of Launch Vehicle Payload Capability Authors: Voloshin M. 2017 (2); 29-34 Language: Russian Annotation: The paper presents a complex of [...]

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14.1.2017 Design Studies into Dynamic and Structural Characteristics of Two-Stage Direct-Action Solenoid-Operated Hydraulic Valve

Design Studies into Dynamic and Structural Characteristics of Two-Stage Direct-Action Solenoid-Operated Hydraulic Valve Authors: Boiko V. 2017 (1); 88-94 Language: Russian [...]

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8.1.2024 Theoretic-experimental evaluation of the solid-propellant grain erosive burning

2024, (1); 72-77 Language: Ukrainian Annotation: The high demands for the flow rate and thrust characteristics specified for the modern solid-propellant rocket motors (SRM) under [...]

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16.1.2024 EDUCATIONAL TENDENCIES AS AN ELEMENT OF INNOVATIVE PROGRESS IN THE PERSONNEL TRAINING SYSTEM FOR THE STATE-OF-THE-ART ENTERPRISES

The goal-oriented educational areas represent a complex of actions of several divisions at the enterprise, supervised by the scientific-educational center, which aim to [...]

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3.1.2024 Future projects of lunar exploration implemented by Yuzhnoye SDO

...surface of the Moon and transport experimental equipment; mobile laboratories; a reconnaissance rover to provide reconnaissance missions on the surface of the Moon; vehicles to [...]

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19.1.2020 Pyrobolts: types, design, development. Shear type pyrobolt developed at Yuzhnoye SDO

Owing to the simple design, reliability and short action time, the pyrobolts have found wide application in aerospace engineering for separation of assemblies and [...]

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4.1.2020 Terminal guidance of the aircraft being maneuvering while descending in the atmosphere under conditions of aerodynamic balancing

Based on the results of processing single calculations, the corresponding flight ranges of a flying vehicle and the lateral displacement of the touchdown points are determined, the [...]

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23.2.2018 On the Role of Space in Origination of Inertia Force Field, Earth Gravity Force Field and Zero Gravity of Material Body

Solution of the problem rests on the example of the cantilever beam and mathematical model of the information reflection process, which for the first time takes into [...]

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15.2.2018 Topical Issues of Creation of Space Rocket Thermostatic System Mating Points

Besides, the methodological principles based on problematic, systematic, and structuralfunctional approach were applied using the theoretical and empirical capabilities, [...]

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5.2.2018 Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office

They are used in the operating pressure range of 0.5…56 MPa, at that, the action time is 0.025…0.15 s. This electrohydraulic valve is operable at the pressure below 8 [...]

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