ISSN 2617-5525; e-ISSN 2617-5533
Issue № 2 (2019)
Date of publication: 30.08.2019
Content № 2, 2019:
1. Optimization of the trajectory of the antiaircraft guided missile
Izhko V. O., Yemelyanova I. O., Reznik I. M., Khorolskiy P. G.Мова: Russian
Kosm. teh. Raket. vooruž. 2019, (2); 3-10
https://doi.org/10.33136/stma2019.02.003
Annotation | Full Text (PDF)2. Mathematical models for assessment of safety in the impact area of cluster ammunition of the warhead during missile complex testing
Hladkyi Ye. H.Мова: Russian
Kosm. teh. Raket. vooruž. 2019 (2); 11-17
https://doi.org/10.33136/stma2019.02.011
Annotation | Full Text (PDF)3. Features of design and production of the technological aids for assembly of the spacecraft separation system of CLAMP BAND type
Kodenets D. O., Sencha S. A., Makarenko A. O.Мова: Russian
Kosm. teh. Raket. vooruž. 2019, (2); 18-24
https://doi.org/10.33136/stma2019.02.018
Annotation | Full Text (PDF)4. Numerical simulation of behavior of elastic structures with local stiffening elements
Hudramovych V. S., Hart Ye. L., Strunin K. A.Мова: Russian
Kosm. teh. Raket. vooruž. 2019, (2); 25-34
https://doi.org/10.33136/stma2019.02.025
Annotation | Full Text (PDF)5. Features of the development testing of the propellants deposition inside the tanks of launch vehicles
Sedykh I. V., Nazarenko D. S., Smolenskyi D. E.Мова: Russian
Kosm. teh. Raket. vooruž. 2019, (2); 35-41
https://doi.org/10.33136/stma2019.02.035
Annotation | Full Text (PDF)6. Stabilization of gas reducers adjustment
Nazarenko O. P., Reuta V. I., Makarov O. D.Мова: Russian
Kosm. teh. Raket. vooruž. 2019, (2); 42-49
https://doi.org/10.33136/stma2019.02.042
Annotation | Full Text (PDF)7. On critical stress of the longitudinal stability of the stiffened cylindrical shells. Dynamic problem
Kaplya P. G.Мова: Russian
Kosm. teh. Raket. vooruž. 2019, (2); 50-57
https://doi.org/10.33136/stma2019.02.050
Annotation | Full Text (PDF)8. Evaluation of the external acoustic loads, acting on the rocket when it passes the leg with maximum velocity head
Batutina T. Y., Bondar’ D. S., Hrinchenko V. T., Oliinyk V. N.Мова: Russian
Kosm. teh. Raket. vooruž. 2019, (2); 58-62
https://doi.org/10.33136/stma2019.02.058
Annotation | Full Text (PDF)9. Gas-dynamic simulation of the supersonic stream in the pulsed wind tunnel
Sirenko V. M., Zhivotov O. Yu.Мова: Russian
Kosm. teh. Raket. vooruž. 2019, (2); 63-70
https://doi.org/10.33136/stma2019.02.063
Annotation | Full Text (PDF)10. Dynamic performance of the gas drive with jet motor
Oliinyk V. P., Kaluger L. G.Мова: Russian
Kosm. teh. Raket. vooruž. 2019, (2); 71-79
https://doi.org/10.33136/stma2019.02.071
Annotation | Full Text (PDF)11. Winding the tubes of rectangular section using dowels
Lavreshov V. V., Malyi L. P., Kovalev Y. V., Kramarenko O. M., Omelchenko D. S.Мова: Russian
Kosm. teh. Raket. vooruž. 2019, (2); 80-91
https://doi.org/10.33136/stma2019.02.080
Annotation | Full Text (PDF)12. Procedure of acoustic loads measuring during the ILV launch
Batutina T. Y., Bondar’ D. S.Мова: Russian
Kosm. teh. Raket. vooruž. 2019, (2); 92-95
https://doi.org/10.33136/stma2019.02.092
Annotation | Full Text (PDF)13. Study of the stress and strain state of the multilayer bellows
Vasilieva T. M., Strunin K. A., Onofriienko V. I.Мова: Russian
Kosm. teh. Raket. vooruž. 2019, (2); 96-102
https://doi.org/10.33136/stma2019.02.096
Annotation | Full Text (PDF)14. Selection of the validation algorithm for the solid rocket motor trust measurement procedure
Voloshina M. O., Gergel V. G., Yeres L. O., Kurako I. М., Oliinyk O. O., Rohulin V. V.Мова: Russian
Kosm. teh. Raket. vooruž. 2019, (2); 103-108
https://doi.org/10.33136/stma2019.02.103
Annotation | Full Text (PDF)