ISSN 2617-5525; e-ISSN 2617-5533
Issue № 1 (2023)
Date of publication: 12.05.2023
Content № 1, 2023:
1. On the development of a methodology for building air and missile defense systems. Explanation of the investigation mechanism
Perkov V. M., Herasimov A. P., Degtyarev O. V.Language: Ukrainian
Kosm. teh. Raket. vooruž. 2023 (1); 3-13
https://doi.org/10.33136/stma2023.01.003
Annotation | Full Text (PDF)2. How Yuzhnoye develops models for flight safety index evaluation for the case of a rocket failure during the flight
Hladkyi E. H., Perlyk V. I.Language: Ukrainian
Kosm. teh. Raket. vooruž. 2023 (1); 14-30
https://doi.org/10.33136/stma2023.01.014
Annotation | Full Text (PDF)3. Analysis of a modernized 9K51 Hrad Multiple Rocket Launcher System to determine the performance specifications of the 122-mm unguided rocket projectile in development
Aksenenko O. V., Hurskyi O. I. , Klochkov A. S., Kondratiuk Ye. A., Shyniberov D. O.Language: Ukrainian
Kosm. teh. Raket. vooruž. 2023 (1); 31-40
https://doi.org/10.33136/stma2023.01.031
Annotation | Full Text (PDF)4. On control of spacecraft orientation to the ground data acquisition station
Ivanova G. A., Khoroshilov V. S.Language: English
Kosm. teh. Raket. vooruž. 2023 (1); 41-47
https://doi.org/10.33136/stma2023.01.041
Annotation | Full Text (PDF)5. Fueling-neutralization stations. New developments and applications
Pozdieiev H.L., Litau Ye. E.Language: Ukrainian
Kosm. teh. Raket. vooruž. 2023 (1); 48-55
https://doi.org/10.33136/stma2023.01.048
Annotation | Full Text (PDF)6. Numerical modeling of translational and rotational vibrations of a solid-propellant rocket motor on a test stand during firing tests
Lysenko M. T., Rohulin V. V., Demchenko A. V., Bezkrovny І. B., Kalnysh R. V.Language: Ukrainian
Kosm. teh. Raket. vooruž. 2023 (1); 56-62
https://doi.org/10.33136/stma2023.01.056
Annotation | Full Text (PDF)7. Specificity of using rubbers as structural materials for making connector assemblies of temperature conditioning systems
Khorolskyi M. S., Bigun S. O.Language: Ukrainian
Kosm. teh. Raket. vooruž. 2023 (1); 63-69
https://doi.org/10.33136/stma2023.01.063
Annotation | Full Text (PDF)8. Specificity of developing pyrobolts with low impact and vibration impulse responses
Samoilenko I. D., Voloshin V. V., Bezkorsyi D. M.Language: Ukrainian
Kosm. teh. Raket. vooruž. 2023 (1); 70-76
https://doi.org/10.33136/stma2023.01.070
Annotation | Full Text (PDF)9. Methodology for selecting design parameters of solid-propellant sustainer engines. Mathematical support and software
Yenotov V. H., Kushnir B. I., Pustovharova O. V., Chubarov A. M.Language: Ukrainian
Kosm. teh. Raket. vooruž. 2023 (1); 77-87
https://doi.org/10.33136/stma2023.01.077
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