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137 search results for "ring"
14.1.2024 EXPERIMENTAL STUDIES OF THE PERFORMANCE OF PYROTECHNIC DEVICES INSTALLED ON THE LAUNCH VEHICLE SEPARATION SYSTEMS
The research methodology, experimental scenario, in particular, a description of the research object and a scheme for measuring test results are presented.
15.1.2024 Enhancing operability of the fuel system units in the hot climate conditions
Heat resistance during compression is most important for rubbers used for seals of various types: rings, collars, armored collars, gaskets for aviation and rocket [...]
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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
It proves itself and can serve as an example of introduction at any manufacturing enterprise.
7.1.2024 Selection of the functional units for the Cyclone-4M ILV separation system
Basic requirements are specified that need to be taken into account when engineering the separation system: reliable and safe separation, minimal losses in payload [...]
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5.1.2024 Assessment of risk of toxic damage to people in case of a launch vehicle accident at flight
2024, (1); 40-50 DOI: https://doi.org/10.33136/stma2024.01.040 Language: English Annotation: Despite stringent environmental requirements, modern launch vehicles/integrated [...]
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4.1.2024 The dynamics of servo drives
2024, (1); 29-39 DOI: https://doi.org/10.33136/stma2024.01.029 Language: Ukrainian Annotation: The article gives the analysis results for the servo drives dynamics, obtained from [...]
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3.1.2024 Future projects of lunar exploration implemented by Yuzhnoye SDO
2024, (1); 19-28 DOI: https://doi.org/10.33136/stma2024.01.019 Language: English Annotation: Over the past years, the leading space powers have been returning to the idea of [...]
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2.1.2024 New and advanced liquid rocket engines of the Yuzhnoye SDO
Moreover, liquid engines design office was assigned with manufacturing and testing of the main rocket engines, developed by NPO Energomash and to be installed on [...]
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9.2.2019 Gas-dynamic simulation of the supersonic stream in the pulsed wind tunnel
The shock wind tunnel is designed to simulate the incident flow during rocket flight at high supersonic and hypersonic velocities.
3.1.2020 Analysis of the unsteady stress-strain behavior of the launch vehicle hold-down bay at liftoff
Intsitute of Mechanical Engineering Problems, Kharkiv, Ukraine 2 Page: Kosm. The hold-down bay is a cylindrical shell with the load-bearing elements as the standing [...]
Read more 3.1.2020 Analysis of the unsteady stress-strain behavior of the launch vehicle hold-down bay at liftoff