logo_ua
Desktop EN 2023
logo_ua
logo_ua
File of Issue № 2 (2018)

ISSN 2617-5525; e-ISSN 2617-5533
Issue № 2 (2018)
Date of publication: 14.09.2018

ZBORNIK_2018_2

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)
File of Issue № 2 (2018)
File of Issue № 2 (2018)
File of Issue № 2 (2018)
Visits:98