ISSN 2617-5525; e-ISSN 2617-5533
Issue № 2 (2018)
Date of publication: 14.09.2018
Contents № 2, 2018:
1. Design Office of Liquid Rocket Engines is 60
Shulga V. A., Dibrivny O. V.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 3-7
https://doi.org/10.33136/stma2018.02.003
Annotation | Full Text (PDF)2. Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines
Prokopchuk O. O., Shulga V. A., Strelchenko E. V., Dibrivny O. V., Kukhta A. S.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 8-15
https://doi.org/10.33136/stma2018.02.008
Annotation | Full Text (PDF)3. Possible Ways of Modernization of VEGA Launch Vehicle AVUM Stage Main Engine Assembly
Prokopchuk O. O., Shulga V. A., Strelchenko E. V., Konokh V. I., Kovalenko A. M., Dibrivny O. V., Lapin O. V., Kukhta A. S.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 16-24
https://doi.org/10.33136/stma2018.02.016
Annotation | Full Text (PDF)4. Turbopump Units of Rocket Engines Developed by DO-4
Ivanov Y. N., Badun O. P., Deshevykh S. O., Ivchenko L. F.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 25-33
https://doi.org/10.33136/stma2018.02.025
Annotation | Full Text (PDF)5. Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office
Konokh V. I., Boiko V. S., Troyak A. B., Ivashura A. V.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 34-48
https://doi.org/10.33136/stma2018.02.034
Annotation | Full Text (PDF)6. Introduction of Additive Technologies for LRE Parts Manufacturing
Kovalenko A. M., Ivchenko L. F., Blishun Y. V.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 49-56
https://doi.org/10.33136/stma2018.02.049
Annotation | Full Text (PDF)7. Theoretical Models of Sound Speed Increase Effects in Gas Duct with Corrugated Wall
Konokh V. I., Shevchenko S. A., Grigor’ev O. L.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 57-67
https://doi.org/10.33136/stma2018.02.057
Annotation | Full Text (PDF)8. Development of Nozzle Blocks New Manufacturing Technology without Blazing
Kovalenko A. M., Kirsanov D. V., Mirosidi M. A., Shelyagin V. D., Bernatsky A. V., Siora O. V.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 68-75
https://doi.org/10.33136/stma2018.02.068
Annotation | Full Text (PDF)9. The Impact of Worm Design on Power and Anti-Cavitation Properties of Worm-Centrifugal Pumps
Nazarenko G. V., Filippenko P. P., Strelchenko O. Y., Deshevykh S. O.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 76-82
https://doi.org/10.33136/stma2018.02.076
Annotation | Full Text (PDF)10. Calculation of Gas Flow in High-Altitude Engine Nozzle and Experience of Using Water-Cooled Nozzle Head during Tests
Nikitenko K. O.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 83-93
https://doi.org/10.33136/stma2018.02.083
Annotation | Full Text (PDF)11. Some Peculiarities of Ensuring LRE Guarantied Service Life in the Conditions of Replacement of Components of Interindustry Application
Patalakha V. A., Ryzhko O. V.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 94-100
https://doi.org/10.33136/stma2018.02.094
Annotation | Full Text (PDF)12. Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs
Aksenenko O. V., Baranov E. Y., Hurskyi O. I., Klochkov A. S., Morozov A. S., Alpatov A. P., Senkin V. S., Siutkina-Doronina S. V.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 101-116
https://doi.org/10.33136/stma2018.02.101
Annotation | Full Text (PDF)13. On an Approach to Constructing the Extremes in the Tasks of Optimal Solutions Search
Shekhovtsov V. S.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 117-126
https://doi.org/10.33136/stma2018.02.117
Annotation | Full Text (PDF)14. A Concept of Modular Transport Vehicle for Lunar Program
Psaryov A. I., Yerofeyev S. I., Nazarets V. S.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 127-131
https://doi.org/10.33136/stma2018.02.127
Annotation | Full Text (PDF)15. Topical Issues of Creation of Space Rocket Thermostatic System Mating Points
Bigun S. O., Khorolskyi M. S.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 132-138
https://doi.org/10.33136/stma2018.02.132
Annotation | Full Text (PDF)16. Design Solutions to Prevent Propellant Ingress into SRM Case Space behind Sealing Ring
Motylyov S. O., Malyi L. P., Kolos O. M., Faryat’eva N. P., Badakva L. M.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 139-142
https://doi.org/10.33136/stma2018.02.139
Annotation | Full Text (PDF)17. Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine
Usichenko V. I.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 143-150
https://doi.org/10.33136/stma2018.02.143
Annotation | Full Text (PDF)18. Angular Stabilization of an Object Rapidly Rotating around Longitudial Axis
Lapko O. M., Meleshko A. O.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 151-156
https://doi.org/10.33136/stma2018.02.151
Annotation | Full Text (PDF)19. Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles
Aksiuta О. А., Balyayev O. A., Konstantinov G. I., Sidoruk V. O.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 157-172
https://doi.org/10.33136/stma2018.02.157
Annotation | Full Text (PDF)20. The Use of Special Devices during Launch Pad Development Testing
Fedenko B. R., Onischenko S. M., Yerofeyev S. I.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 173-177
https://doi.org/10.33136/stma2018.02.173
Annotation | Full Text (PDF)21. Ensuring Aiming Accuracy of Ship’s Telemetry Reception Antenna Installation for Small Vessels
Lyalyuk S. M., Tikhonov V. L.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 178-183
https://doi.org/10.33136/stma2018.02.178
Annotation | Full Text (PDF)22. Uncertainty Calculation Procedure during Measuring Instrumentation Calibration
Voloshina M. O., Golovin O. S., Yeres L. O., Kurako I. М.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 184-189
https://doi.org/10.33136/stma2018.02.184
Annotation | Full Text (PDF)23. On the Role of Space in Origination of Inertia Force Field, Earth Gravity Force Field and Zero Gravity of Material Body
Muliar Yu. M., Fedorov V. M.Мова: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 190-206
https://doi.org/10.33136/stma2018.02.190
Annotation | Full Text (PDF)