ISSN 2617-5525; e-ISSN 2617-5533
Issue № 1 (2020)
Date of publication: 20.07.2020
Content № 1, 2020:
1. Solving a problem of optimum curves of descent using the enhanced Euler equation
Horbulin V. P., Degtyarev O. V., Shekhovtsov V. S.Language: Russian
Kosm. teh. Raket. vooruž. 2020, (1); 3-12
https://doi.org/10.33136/stma2020.01.003
Annotation | Full Text (PDF)2. Analysis of development trends of design parameters and basic characteristics of missiles for the advanced multiple launch rocket systems
Aksenenko O. V., Hurskyi O. I., Klochkov A. S., Kondratiuk Ye. A., Senkin V. S., Siutkina-Doronina S. V.Language: Russian
Kosm. teh. Raket. vooruž. 2020, (1); 13-25
https://doi.org/10.33136/stma2020.01.013
Annotation | Full Text (PDF)3. Analysis of the unsteady stress-strain behavior of the launch vehicle hold-down bay at liftoff
Degtiarov М. O., Avramov K. V.Language: Russian
Kosm. teh. Raket. vooruž. 2020, (1); 26-33
https://doi.org/10.33136/stma2020.01.026
Annotation | Full Text (PDF)4. Terminal guidance of the aircraft being maneuvering while descending in the atmosphere under conditions of aerodynamic balancing
Sirenko V. M., Levin O. S., Mashtak I. V., Sheptun A. D.Language: Russian
Kosm. teh. Raket. vooruž. 2020, (1); 34-43
https://doi.org/10.33136/stma2020.01.034
Annotation | Full Text (PDF)5. Strength and stability of inhomogeneous structures of space technology, consid-ering plasticity and creep
Hudramovych V. S., Sirenko V. M., Klimenko D. V., Hart Ye. L.Language: Russian
Kosm. teh. Raket. vooruž. 2020, (1); 44-56
https://doi.org/10.33136/stma2020.01.044
Annotation | Full Text (PDF)6. Mechanics of a satellite cluster. Methods for estimating the probability of their maximal approach in flight
Degtyarev O. V., Sheptun A. D.Language: Russian
Kosm. teh. Raket. vooruž. 2020, (1); 57-75
https://doi.org/10.33136/stma2020.01.057
Annotation | Full Text (PDF)7. Mechanics of a satellite cluster. Methods for estimating the probability of their maximal approach in flight
Holubek O. V.Language: Russian
Kosm. teh. Raket. vooruž. 2020, (1); 76-84
https://doi.org/10.33136/stma2020.01.076
Annotation | Full Text (PDF)8. Determining the main parameters of transport aircraft modifications considering the fuel efficiency
Los' O. V.Language: Russian
Kosm. teh. Raket. vooruž. 2020, (1); 85-89
https://doi.org/10.33136/stma2020.01.085
Annotation | Full Text (PDF)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 O. V., Husarova I. O., Derevianko I. I., Kharchenko V. M., Litot O. V.Language: Russian
Kosm. teh. Raket. vooruž. 2020, (1); 90-98
https://doi.org/10.33136/stma2020.01.090
Annotation | Full Text (PDF)10. Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM
Yenotov V. H., Pustovharova O. V.Language: Russian
Kosm. teh. Raket. vooruž. 2020, (1); 99-106
https://doi.org/10.33136/stma2020.01.099
Annotation | Full Text (PDF)11. Some results of strength calculations relying on analytical and FEM approaches. Trends of using contemporary machine learning strategies
Gryshchak V. Z.Language: Russian
Kosm. teh. Raket. vooruž. 2020, (1); 107-113
https://doi.org/10.33136/stma2020.01.107
Annotation | Full Text (PDF)12. Modification of technology as the main course in the military transport aircraft development
Los' O. V.Language: Russian
Kosm. teh. Raket. vooruž. 2020, (1); 114-120
https://doi.org/10.33136/stma2020.01.114
Annotation | Full Text (PDF)13. Mathematical models of hydraulic servomechanisms of space technologynt
Kozak L. R., Shakhov М. I.Language: Russian
Kosm. teh. Raket. vooruž. 2020, (1); 121-132
https://doi.org/10.33136/stma2020.01.121
Annotation | Full Text (PDF)14. On the problem of optimum control
Zavialov P. P., Sidoruk V. O.Language: Russian
Kosm. teh. Raket. vooruž. 2020, (1); 133-136
https://doi.org/10.33136/stma2020.01.133
Annotation | Full Text (PDF)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
https://doi.org/10.33136/stma2020.01.137
Annotation | Full Text (PDF)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
https://doi.org/10.33136/stma2020.01.149
Annotation | Full Text (PDF)17. Acoustic problems of rocket launch
Hrinchenko V. T.Language: Russian
Kosm. teh. Raket. vooruž. 2020, (1); 155-159
https://doi.org/10.33136/stma2020.01.155
Annotation | Full Text (PDF)18. Development of autonomous power engineering systems with hydrogen energy storage
Shevchenko A. A., Kozak L. R., Zipunnikov M. M., Kotenko A. L.Language: Russian
Kosm. teh. Raket. vooruž. 2020, (1); 160-169
https://doi.org/10.33136/stma2020.01.160
Annotation | Full Text (PDF)19. Pyrobolts: types, design, development. Shear type pyrobolt developed at Yuzhnoye SDO
Samoilenko I. D., Voloshin V. V., Onofriienko V. I., Bezkorsyi D. M.Language: Russian
Kosm. teh. Raket. vooruž. 2020, (1); 170-176
https://doi.org/10.33136/stma2020.01.170
Annotation | Full Text (PDF)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
https://doi.org/10.33136/stma2020.01.177
Annotation | Full Text (PDF)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
https://doi.org/10.33136/stma2020.01.184
Annotation | Full Text (PDF)
