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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.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 3-7

https://doi.org/10.33136/stma2018.02.003

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2. Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines

Prokopchuk O. O., Shulga V. A., Strelchenko E. V., Dibrivny O. V., Kukhta A. S.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 8-15

https://doi.org/10.33136/stma2018.02.008

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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.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 16-24

https://doi.org/10.33136/stma2018.02.016

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4. Turbopump Units of Rocket Engines Developed by DO-4

Ivanov Y. N., Badun O. P., Deshevykh S. O., Ivchenko L. F.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 25-33

https://doi.org/10.33136/stma2018.02.025

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5. Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office

Konokh V. I., Boiko V. S., Troyak A. B., Ivashura A. V.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 34-48

https://doi.org/10.33136/stma2018.02.034

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6. Introduction of Additive Technologies for LRE Parts Manufacturing

Kovalenko A. M., Ivchenko L. F., Blishun Y. V.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 49-56

https://doi.org/10.33136/stma2018.02.049

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7. Theoretical Models of Sound Speed Increase Effects in Gas Duct with Corrugated Wall

Konokh V. I., Shevchenko S. A., Grigor’ev O. L.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 57-67

https://doi.org/10.33136/stma2018.02.057

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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.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 68-75

https://doi.org/10.33136/stma2018.02.068

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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.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 76-82

https://doi.org/10.33136/stma2018.02.076

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10. Calculation of Gas Flow in High-Altitude Engine Nozzle and Experience of Using Water-Cooled Nozzle Head during Tests

Nikitenko K. O.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 83-93

https://doi.org/10.33136/stma2018.02.083

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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.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 94-100

https://doi.org/10.33136/stma2018.02.094

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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.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 101-116

https://doi.org/10.33136/stma2018.02.101

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13. On an Approach to Constructing the Extremes in the Tasks of Optimal Solutions Search

Shekhovtsov V. S.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 117-126

https://doi.org/10.33136/stma2018.02.117

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14. A Concept of Modular Transport Vehicle for Lunar Program

Psaryov A. I., Yerofeyev S. I., Nazarets V. S.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 127-131

https://doi.org/10.33136/stma2018.02.127

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15. Topical Issues of Creation of Space Rocket Thermostatic System Mating Points

Bigun S. O., Khorolskyi M. S.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 132-138

https://doi.org/10.33136/stma2018.02.132

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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.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 139-142

https://doi.org/10.33136/stma2018.02.139

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17. Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine

Usichenko V. I.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 143-150

https://doi.org/10.33136/stma2018.02.143

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18. Angular Stabilization of an Object Rapidly Rotating around Longitudial Axis

Lapko O. M., Meleshko A. O.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 151-156

https://doi.org/10.33136/stma2018.02.151

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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.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 157-172

https://doi.org/10.33136/stma2018.02.157

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20. The Use of Special Devices during Launch Pad Development Testing

Fedenko B. R., Onischenko S. M., Yerofeyev S. I.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 173-177

https://doi.org/10.33136/stma2018.02.173

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21. Ensuring Aiming Accuracy of Ship’s Telemetry Reception Antenna Installation for Small Vessels

Lyalyuk S. M., Tikhonov V. L.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 178-183

https://doi.org/10.33136/stma2018.02.178

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22. Uncertainty Calculation Procedure during Measuring Instrumentation Calibration

Voloshina M. O., Golovin O. S., Yeres L. O., Kurako I. М.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 184-189

https://doi.org/10.33136/stma2018.02.184

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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.

Language: Russian

Kosm. teh. Raket. vooruž. 2018 (2); 190-206

https://doi.org/10.33136/stma2018.02.190

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File of Issue № 2 (2018)
File of Issue № 2 (2018)
File of Issue № 2 (2018)
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