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

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

Hladkyi Ye. H., Perlyk V. I.

Language: Ukrainian

Kosm. teh. Raket. vooruž. 2023 (1); 14-30

https://doi.org/10.33136/stma2023.01.014

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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

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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

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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

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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

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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

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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

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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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