Content № 2, 2019

Current issue
 

ISSN 2617-5525; e-ISSN 2617-5533

Issue № 2 (2019)

Date of publication: 30.08.2019

Authors of the issue

 

 

 

 

 

 

 

Content № 2, 2019

1. Optimization of the trajectory of the antiaircraft guided missile

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

Language: Russian
Kosm. teh. Raket. vooruž. 2019 (2); 3-10
 
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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

Hladkiy E. G.

Language: Russian
Kosm. teh. Raket. vooruž. 2019 (2); 11-17
 
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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. A., Sencha S. A., Makarenko A. A.

Language: Russian
Kosm. teh. Raket. vooruž. 2019 (2); 18-24
 
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4. Numerical simulation of behavior of elastic structures with local stiffening elements

Hudramovich V. S., Hart E. L., Strunin K. A.

Language: Russian
Kosm. teh. Raket. vooruž. 2019 (2); 25-34
 
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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., Smolenskiy D. E.

Language: Russian
Kosm. teh. Raket. vooruž. 2019 (2); 35-41
 
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6. Stabilization of gas reducers adjustment

Nazarenko Y. P., Reuta V. I., Makarov A. D.

Language: Russian
Kosm. teh. Raket. vooruž. 2019 (2); 42-49
 
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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
 
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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., Grinchenko V. T., Olyinick V. N.

Language: Russian
Kosm. teh. Raket. vooruž. 2019 (2); 58-62
 
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9. Gas-dynamic simulation of the supersonic stream in the pulsed wind tunnel

Sirenko V. N., Zhivotov A. Y.

Language: Russian
Kosm. teh. Raket. vooruž. 2019 (2); 63-70
 
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10. Dynamic performance of the gas drive with jet motor

Oleinyk V. P., Kaluger L. G.

Language: Russian
Kosm. teh. Raket. vooruž. 2019 (2); 71-79
 
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11. Winding the tubes of rectangular section using dowels

Lavreshov V. V., Maliy L. P., Kovalev Y. V., Kramarenko Y. N., Omelchenko D. S.

Language: Russian
Kosm. teh. Raket. vooruž. 2019 (2); 80-91
 
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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
 
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13. Study of the stress and strain state of the multilayer bellows

Vasilieva T. N., Strunin K. A., Onofrienko V. I.

Language: Russian
Kosm. teh. Raket. vooruž. 2019 (2); 96-102
 
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14. Selection of the validation algorithm for the solid rocket motor trust measurement procedure

Voloshina M. A., Gergel V. G., Yeres L. A., Kurako I. M., Oleinyk A. O., Rogulin V. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2019 (2); 103-108
 
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