Content 2018 (2)

File of issue 2018 (2)
 

ISSN 2617-5525; e-ISSN 2617-5533

Issue № 2 (2018)

Date of publication: 14.09.2018

Authors of the issue

 

 

 

 

 

 

 

Content № 2, 2018

1. Design Office of Liquid Rocket Engines is 60

Shulga V. A., Dibrivny A. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 3-7
 
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2. Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines

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

Language: Russian
Kosm. teh. Raket. vooruž. 2018, (2), 8-15
 
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3. Possible Ways of Modernization of VEGA Launch Vehicle AVUM Stage Main Engine Assembly

Prokopchuk A. A., Shulga V. A., Strelchenko E. V., Konokh V. I., Kovalenko A. N., Dibrivny A. V., Lapin A. V., Kukhta A. S.

Language: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 16-24
 
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4. Turbopump Units of Rocket Engines Developed by DO-4

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

Language: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 25-33
 
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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
 
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6. Introduction of Additive Technologies for LRE Parts Manufacturing

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

Language: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 49-56
 
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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 A. L.

Language: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 57-67
 
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8. Development of Nozzle Blocks New Manufacturing Technology without Blazing

Kovalenko A. N., Kirsanov D. V., Mirosidi N. A., Shelyagin V. D., Bernatsky A. V., Siora A. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 68-75
 
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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 A. Y., Deshevykh S. A.

Language: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 76-82
 
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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. A.

Language: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 83-93
 
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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 A. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 94-100
 
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12. Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs

Aksyonenko A. V., Baranov E. Y., Gursky A. I., Klochkov A. S., Morozov A. S., Alpatov A. P., Sen’kin V. S., Syutkina-Doronina S. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 101-116
 
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13. Of 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
 
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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
 
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15. Topical Issues of Creation of Space Rocket Thermostatic System Mating Points

Bigun S. A., Khorolsky M. S.

Language: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 132-138
 
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16. Design Solutions to Prevent Propellant Ingress into SRM Case Space behind Sealing Ring

Motylyov S. A., Maly L. P., Kolos A. M., Faryat’eva N. P., Badakva L. N.

Language: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 139-142
 
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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
 
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18. Angular Stabilization of an Object Rapidly Rotating around Longitudinal Axis

Lapko A. N., Meleshko A. A.

Language: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 151-156
 
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19. Control of Validity and Assessment of Accuracy of Telemetry Results during Full-Scale Test of Launch Vehicles

Aksyuta O. A., Balyayev O. A., Konstantinov G. I., Sidoruk V. O.

Language: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 157-172
 
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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
 
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21. Ensuring Aiming Accuracy of Ship’s Telemetry Reception Antenna Installation for Small Vessels

Lyalyuk S. N., Tikhonov V. L.

Language: Russian
Kosm. teh. Raket. vooruž. 2018 (2); 178-183
 
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22. Uncertainty Calculation Procedure during Measuring Instrumentation Calibration

Voloshina M. A., Golovin A. S., Eres L. A., Kurako I. M.

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

Mulyar Y. M., Fedorov V. M.

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