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File of Issue № 2 (2019)

ISSN 2617-5525; e-ISSN 2617-5533
Issue № 2 (2019)
Date of publication: 30.08.2019

ZBORNIK_2019_2

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

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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 Ye. H.

Мова: 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.

Мова: 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.

Мова: 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.

Мова: 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.

Мова: 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.

Мова: 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.

Мова: 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.

Мова: 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.

Мова: 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.

Мова: 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.

Мова: 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.

Мова: 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.

Мова: Russian

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

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

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File of Issue № 2 (2019)
File of Issue № 2 (2019)
File of Issue № 2 (2019)
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