5.1.2019 Methodology of Normative Principles of Justification of Launch Vehicle Launching Facility Structures Lifetime

Developing strength standards and useful life calculation basis, it is advisable to use modern methods of engineering diagnostics, in particular, holographic interferometry and [...]

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17.1.2019 Development of Prospective Small-Size Auxiliary SMR of New Type

Preliminary results of design and experimental activities, performed in Yuzhnoye SDO, showed the possibility in principle and practicability to develop two new types of [...]

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16.1.2019 Oscillation Processes in Rig at the Moment of SRM Transfer to Main Operation Mode

2019, (1); 110-113 DOI: https://doi.org/10.33136/stma2019.01.110 Language: Ukrainian Annotation: This paper describes the configuration of the rig, designed to fasten the [...]

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16.1.2016 Peculiarities of Development of SRM Thrust Vector Controls at DO-5

2016 (1); 97-104 Language: Russian Annotation: The thrust vector controls, peculiarities of designing and development testing of most sophisticated units and assemblies of [...]

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4.1.2016 The Company’s Experience in Designing and Operating Special Bench Equipment for SRM Ground Tests

2016 (1); 26-33 Language: Russian Annotation: The information on Yuzhnoye SDO experience in designing and operation of special equipment for testing of SRM of [...]

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7.2.2019 On critical stress of the longitudinal stability of the stiffened cylindrical shells. Dynamic problem

They were obtained due to application of the dynamic approach to the solution of the refined equilibrium equations, introduction of the Qfactor of the structural elements into the [...]

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6.2.2019 Stabilization of gas reducers adjustment

2019, (2); 42-49 DOI: https://doi.org/10.33136/stma2019.02.042 Language: Russian Annotation: The general information on gas pressure reducers, on their purpose in launch [...]

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3.2.2019 Features of design and production of the technological aids for assembly of the spacecraft separation system of CLAMP BAND type

Features of design and production of the technological aids for assembly of the spacecraft separation system of CLAMP BAND type Authors: Kodenets D. The pressing mechanism is [...]

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7.1.2023 Specificity of using rubbers as structural materials for making connector assemblies of temperature conditioning systems

Specificity of using rubbers as structural materials for making connector assemblies of temperature conditioning systems Authors: Khorolskyi M. Damper, made of easily [...]

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6.1.2023 Numerical modeling of translational and rotational vibrations of a solid-propellant rocket motor on a test stand during firing tests

2023 (1); 56-62 DOI: https://doi.org/10.33136/stma2023.01.056 Language: Ukrainian Annotation: This article dwells on results of firing bench testing of the solid-propellant [...]

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