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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14.1.2019 Technique of Determination of SRM Operational Life Taking into Account Materials and Elements Strength Margins

Analysis of experimental and computation data as applied to solid-propellant rocket engine shows that the most dangerous zones, which define the service life, are the [...]

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12.1.2016 Increasing Effectiveness of Meteorological Rockets when Using Hybrid Motors

2016 (1); 76-81 Language: Russian Annotation: A comparative assessment of effectiveness of usage of hybrid rocket motors and solid rocket motors for meteorological rocket [...]

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11.1.2016 Methodology of Design Evaluation of Main SRM Flowrate-Thrust Characteristics after Stage Separation

It is shown that thrust behavior in the leg of deep decay is determined by two main processes: afterburning of solid propellant charge residues within the first 3-5 s [...]

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Сollected book of scientific-technical articles

design and development of the components parts for the launch vehicles/integrated launch vehicles, missiles (solid- and liquid-propellants engines, power supply [...]

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