10.2.2019 Dynamic performance of the gas drive with jet motor

Dynamic performance of the gas drive with jet motor Authors: Oliinyk V. 2019, (2); 71-79 DOI: https://doi.org/10.33136/stma2019.02.071 Language: Russian Annotation: The use [...]

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12.1.2017 Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator

Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator Authors: Tsyganov V. 2017 (1); 78-83 Language: Russian Annotation: The basic mathematical relations are [...]

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3.1.2023 Analysis of a modernized 9K51 Hrad Multiple Rocket Launcher System to determine the performance specifications of the 122-mm unguided rocket projectile in development

The performance characteristics of the Tornado-G multiple launch rocket system which went into service with the Ministry of Defense of the Russian Federation in 2014, [...]

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21.1.2020 Contemporary approaches to the improvement of methods of space launch system operation for commercial launches of ILV

The article describes the course of development of operation model of a created object; based on investigation of the processes of this model, the object’s performance [...]

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11.1.2018 Ensuring Long Lifetime of the Electrochemical Accumulators Included in Space Rocketry Electric Power Supply Systems

2018 (1); 63-68 DOI: https://doi.org/10.33136/stma2018.01.063 Language: Russian Annotation: Several measures to ensure long service life of electrochemical batteries are proposed: [...]

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8.1.2019 Virtual Tests of Cassette Reentry Vehicle Dash Elements Attachment System during Ground Operation

2019, (1); 54-63 DOI: https://doi.org/10.33136/stma2019.01.054 Language: Russian Annotation: This paper describes the effective approach for the technology of the rocket airframe [...]

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7.1.2019 Experience of Development and Use of Generator Pressurization System for Tanks of Launch Vehicles on High-Temperature Propellants

The important steps were the development of methodology for pressurization system parameters calculation, which enabled achievement of the substantial improvements of their [...]

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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 [...]

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2.1.2019 Flying Vehicle Maneuvering Dynamics in Atmosphere with Weight Asymmetry and Elements of Terminal Control in Turn Leg

Angular motion with nominal and perturbed performances of the aircraft and flight conditions has been consistently considered. Before maneuvering, the aircraft is set at the [...]

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19.1.2019 Peculiarities of Radio Transparent Fairings Development

2019, (1); 132-138 DOI: https://doi.org/10.33136/stma2019.01.132 Language: Russian Annotation: The main task of the radiotransparent radome design is to develop a structure that [...]

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