Content №1 (2020)

Current issue
 

ISSN 2617-5525; e-ISSN 2617-5533

Issue № 1 (2020)

Date of publication: 20.07.2020

Authors of the issue

 

 

 

 

 

 

 

Content № 1, 2020

1. Solving a problem of optimum curves of descent using the enhanced Euler equation

Horbulin V. P., Degtyarev A. V., Shekhovtsov V. S.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 3-12
 
|

2. Analysis of development trends of design parameters and basic characteristics of missiles for the advanced multiple launch rocket systems

Aksenenko A. V., Hursky A. I., Klochkov A. S., Kondratiuk E. A., Senkin V. S., Siutkina-Doronina S. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 13-25
 
|

3. Analysis of the unsteady stress-strain behavior of the launch vehicle hold-down bay at liftoff

Degtiarov М. А., Avramov K. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 26-33
 
|

4. Terminal guidance of the aircraft being maneuvering while descending in the atmosphere under conditions of aerodynamic balancing

Sirenko V. N., Levin А. S., Mashtak I. V., Sheptun А. D.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 34-43
 
|

5. Strength and stability of inhomogeneous structures of space technology, considering plasticity and creep

Hudramovich V. S., Sirenko V. N., Klimenko D. V., Hart E. L.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 44-56
 
|

6. Mechanics of a satellite cluster. Methods for estimating the probability of their maximal approach in flight

Degtyarev A. V., Sheptun A. D.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 57-75
 
|

7. Studying the motion of a launch vehicle and observed space debris objects during launch preparation

Holubek А. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 76-84
 
|

8. Determining the main parameters of transport aircraft modifications considering the fuel efficiency

Los' А. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 85-89
 
|

9. Experimental investigation of a liner-free propellant tank made from polymer composite materials

Sidoruk А. V., Popov D. А., Zadoia А. S., Kalinichenko D. S., Aksenenko А. V., Husarova I. А., Derevianko I. I., Kharchenko V. N., Litot А. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 90-98
 
|

10. Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM

Enotov V. H., Pustovharova Е. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 99-106
 
|

11. Some results of strength calculations relying on analytical and FEM approaches. Trends of using contemporary machine learning strategies

Gristchak V. Z.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 107-113
 
|

12. Modification of technology as the main course in the military transport aircraft development

Los' А. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 114-120
 
|

13. Mathematical models of hydraulic servomechanisms of space technology

Kozak L. R., Shakhov М. I.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 121-132
 
|

14. On the problem of optimum control

Zavialov P. P., Sidoruk V. О.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 133-136
 
|

15. Simulation of thermomechanical processes in functionally-gradient materials of inhomogeneous structure in the manufacturing and operation of rocket structural elements

Usov A. V., Kunitsyn М. V.

Language: Ukrainian
Kosm. teh. Raket. vooruž. 2020 (1); 137-148
 
|

16. Parameters of the supersonic jet of a block propulsion system, flowing into a gas duct, considering chemical kinetics of gas-cycle transformations

Furkalo S. A., Stelmakh K. L., Lazarev T. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 149-154
 
|

17. Acoustic problems of rocket launch

Hrinchenko V. Т.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 155-159
 
|

18. Development of autonomous power engineering systems with hydrogen energy storage

Shevchenko A. A., Kozak L. R., Zipunnikov N. N., Kotenko A. L.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 160-169
 
|

19. Pyrobolts: types, designs, development. A shear type pyrobolt developed in Yuzhnoye SDO

Samoilenko I. D., Voloshin V. V., Onofrienko V. I., Bezkorsyi D. N.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 170-176
 
|

20. Studying the possibility of alternating delivery of rocket propellant wastes to a common thermal neutralization facility

Shynkorenko О. I., Kostenko М. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 177-183
 
|

21. Contemporary approaches to the improvement of methods of space launch system operation for commercial launches of ILV

Hlechkov V. H.

Language: Russian
Kosm. teh. Raket. vooruž. 2020 (1); 184-192
 
|