12.2.2019 Procedure of acoustic loads measuring during the ILV launch

Procedure of acoustic loads measuring during the ILV launch Authors: Batutina T. 2019, (2); 92-95 DOI: https://doi.org/10.33136/stma2019.02.092 Language: Russian [...]

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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

Numerical modeling of translational and rotational vibrations of a solid-propellant rocket motor on a test stand during firing tests Authors: Lysenko M. 2023 (1); [...]

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2.1.2023 How Yuzhnoye develops models for flight safety index evaluation for the case of a rocket failure during the flight

How Yuzhnoye develops models for flight safety index evaluation for the case of a rocket failure during the flight Authors: Hladkyi E. The integral component of this problem [...]

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10.2.2017 Analysis Method of Hydraulic Parameters of Circular Intake Device in Limit Operating Modes

2017 (2); 53-56 Language: Russian Annotation: The paper presents the experiment-calculated data on hydraulic parameters of ring intake device in different operation modes. On [...]

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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

There were two conditions of plasma creation during the research: free location of samples on the surface of the cathode (configuration I) and inside the hollow cathode [...]

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13.1.2024 MODEL OF QUALITY MANAGEMENT OF TECHNICAL PREPARATION FOR THE METAL+COMPOSITE JOINTS PRODUCTION

The work proposes a comprehensive mathematical model for managing the quality of technical preparation for the production of joints based on a quantitative assessment of the [...]

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

For any point of time during the engine operation, burning area and port area of each interval are calculated, taking into account erosive impact on each interval; total [...]

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11.1.2024 PARAMETERS CALCULATION OF THE LUNAR REGOLITH TRANSPORT SYSTEM

It has been proven that the solutions based on using auger conveyors would be most rational for transporting loose lunar regolith over the Moon’s surface because the auger conveyors [...]

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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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