1. Optimization of the trajectory of the antiaircraft guided missile

Izhko V. O., Yemelyanova I. O., Reznik I. M., Khorolskiy P. G.

Language: Russian

Kosm. teh. Raket. vooruž. 2019, (2); 3-10

https://doi.org/10.33136/stma2019.02.003

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2. Mathematical models for assessment of safety in the impact area of cluster ammunition of the warhead during missile complex testing

Hladkyi E. H.

Language: Russian

Kosm. teh. Raket. vooruž. 2019 (2); 11-17

https://doi.org/10.33136/stma2019.02.011

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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.

Language: Russian

Kosm. teh. Raket. vooruž. 2019, (2); 18-24

https://doi.org/10.33136/stma2019.02.018

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4. Numerical simulation of behavior of elastic structures with local stiffening elements

Hudramovych V. S., Hart Ye. L., Strunin K. A.

Language: Russian

Kosm. teh. Raket. vooruž. 2019, (2); 25-34

https://doi.org/10.33136/stma2019.02.025

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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.

Language: Russian

Kosm. teh. Raket. vooruž. 2019, (2); 35-41

https://doi.org/10.33136/stma2019.02.035

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6. Stabilization of gas reducers adjustment

Nazarenko O. P., Reuta V. I., Makarov O. D.

Language: Russian

Kosm. teh. Raket. vooruž. 2019, (2); 42-49

https://doi.org/10.33136/stma2019.02.042

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7. On critical stress of the longitudinal stability of the stiffened cylindrical shells. Dynamic problem

Kaplya P. G.

Language: Russian

Kosm. teh. Raket. vooruž. 2019, (2); 50-57

https://doi.org/10.33136/stma2019.02.050

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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.

Language: Russian

Kosm. teh. Raket. vooruž. 2019, (2); 58-62

https://doi.org/10.33136/stma2019.02.058

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9. Gas-dynamic simulation of the supersonic stream in the pulsed wind tunnel

Sirenko V. M., Zhivotov O. Yu.

Language: Russian

Kosm. teh. Raket. vooruž. 2019, (2); 63-70

https://doi.org/10.33136/stma2019.02.063

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10. Dynamic performance of the gas drive with jet motor

Oliinyk V. P., Kaluger L. G.

Language: Russian

Kosm. teh. Raket. vooruž. 2019, (2); 71-79

https://doi.org/10.33136/stma2019.02.071

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11. Winding the tubes of rectangular section using dowels

Lavreshov V. V., Malyi L. P., Kovalev Y. V., Kramarenko O. M., Omelchenko D. S.

Language: Russian

Kosm. teh. Raket. vooruž. 2019, (2); 80-91

https://doi.org/10.33136/stma2019.02.080

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12. Procedure of acoustic loads measuring during the ILV launch

Batutina T. Y., Bondar’ D. S.

Language: Russian

Kosm. teh. Raket. vooruž. 2019, (2); 92-95

https://doi.org/10.33136/stma2019.02.092

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13. Study of the stress and strain state of the multilayer bellows

Vasilieva T. M., Strunin K. A., Onofriienko V. I.

Language: Russian

Kosm. teh. Raket. vooruž. 2019, (2); 96-102

https://doi.org/10.33136/stma2019.02.096

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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.

Language: Russian

Kosm. teh. Raket. vooruž. 2019, (2); 103-108

https://doi.org/10.33136/stma2019.02.103

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