2.1.2020 Analysis of development trends of design parameters and basic characteristics of missiles for the advanced multiple launch rocket systems

The guided missiles of multiple launch rocket system are intended for delivering munitions to the given spatial point with required and specified kinematic motion parameters [...]

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12.1.2024 Hardening of steels modifying their surfaces with ion-plasma nitriding in glow discharge

The subjects of research included: austenitic steel 12X18Н10T, carbon steel Ст3 and structural steel 45. There were two conditions of plasma creation during the [...]

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6.1.2024 New methods of load-carrying capacity prediction for the ultimately compressed frame structures

2024, (1); 51-60 DOI: https://doi.org/10.33136/stma2024.01.051 Language: English Annotation: Amid acute problems that arise in the field of rocket and space technology, mechanical [...]

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7.1.2024 Selection of the functional units for the Cyclone-4M ILV separation system

2024, (1); 61-71 DOI: https://doi.org/10.33136/stma2024.01.061 Language: Ukrainian Annotation: Separation of the spent LV stages is one of the important problems of the rocket [...]

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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 [...]

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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 bays, in [...]

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

For this purpose, the analysis of operating conditions and possible situations during rocket launches is made. Besides, the methodological principles based on problematic, [...]

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12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs

2018 (2); 101-116 DOI: https://doi.org/10.33136/stma2018.02.101 Language: Russian Annotation: The main scientific and methodological propositions for designing single-stage guided [...]

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21.2.2017 Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft

2017 (2); 121-126 Language: Russian Annotation: The paper considers the TZS-U design developed by Yuzhnoye SDO specialists for windward part of reusable spacecraft with external [...]

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

In different countries they have their own characteristics, depending on the type and performance of the launch vehicles, infrastructure features (geography of the site, [...]

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