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File of Issue № 2 (2017)

ISSN 2617-5525; e-ISSN 2617-5533
Issue № 2 (2017)
Date of publication: 01.11.2017

ZBORNIK_2017_2

ISSN 2617-5525; e-ISSN 2617-5533

Issue № 2 (2017)

Date of publication: 01.11.2017

Contents:

1. DO-2 – Semicentenary

Shevtsov E. I.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 3-4

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2. Creation of Universal System of Launch Vehicle Space Head Modules for Cluster Spacecraft Missions

Agalakov S. O., Makarenko A. O., Silkin O. Y., Shevtsov E. I.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 5-11

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3. Creation of Advanced Facilities for Spacecraft / Launch Vehicle Integration

Makarenko A. O., Mashchenko O. M., Shevtsov E. I.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 12-18

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4. Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics

Logvinenko A. I.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 19-24

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5. Structural Perfection of Cyclone-4 Integrated Launch Vehicle

Zhuk N. P., Makarenko A. O., Shevtsov E. I.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 25-28

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6. Set of Actions on Enhancement of Launch Vehicle Payload Capability

Voloshin M. L., Kuda S. А., Mikhalchishin R. V.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 29-34

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7. Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants

Mikhalchishin R. V., Kuda S. А., Golovin D. Y., Brezgin М. S.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 35-40

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8. Analysis Method of Nitrogen Tetroxide Tanks Generating Pressurization Systems

Petrenko R. М.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 41-48

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9. Peculiarities of Development of Cryogenic Propulsion System Circulating Cooling System

Golovin D. Y., Ermolenko I. M., Kuda S. А., Lomskoy D. А.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 49-52

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10. Analysis Method of Hydraulic Parameters of Circular Intake Device in Limit Operating Modes

Ivanov О. М., Smolenskyi D. E.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 53-56

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11. Remote Monitoring Method of Pneudraulic System Structural Elements Integrity

Babii H. M., Tishchenko Y. S., Mogilevtsev O. А.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 57-59

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12. Determination Procedure for Pneudraulic System and Its Components No-Failure Operation Probability

Nazarenko O. P., Yakimets S. V.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 60-64

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13. Experience in Development of Isolating Fuel Valve with Pneumatic Drive and Hydraulic Brake for Operation under Cryogenic Conditions

Makarenko A. O., Mashchenko O. M., Nazarenko O. P., Skochko V. V., Ustich V. V., Shevtsov E. I.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 65-69

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14. Development Test of Isolating Valve Operation under Cryogenic Conditions

Makarenko A. O., Udovichenko D. O.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 70-76

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15. Oxidizer Feedline Structural Optimization Results

Veskov E. V., Nazarenko O. P., Sedykh I. V., Shevchenko B. А.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 77-82

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16. Determination of Spherical Flange Connections Gasket Clamping Site Width

Onofriienko V. I., Shevtsov E. I., Makarenko A. O.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 83-89

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17. Development Test of Spacecraft Separation Dynamics under Ground Conditions

Gontarovsky V. А., Makarenko A. O., Shevtsov E. I.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 90-101

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18. Development Test of Payload Fairing Separation Dynamics under Ground Conditions

Shevtsov E. I.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 102-106

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19. Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation

Kabakova Zh. V., Kuda S. А., Logvinenko A. I., Khomyak V. O.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 107-111

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20. Research Support for Development of Launch Vehicle Payload Unit Composite Load-Bearing Compartments

Potapov O. М., Kovalenko V. O., Kondrat’ev А. V., Gaidachuk V. Е.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 112-120

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21. Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft

Husarova I. O., Potapov O. М., Shevtsov E. I., Onofriienko V. I., Husev V. V., Manko Т. А.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 121-126

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22. Advanced Aluminum Alloys for Launch Vehicle Pipeline Parts Manufacture

Bondarenko О. V., Mogilevtsev O. А., Tishchenko Y. S.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 127-130

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23. Optimization Technique for Mass of Locally Loaded Rocket Bays with Wafer Structure

Danchenko V. G., Shevtsov E. I., Husev V. V.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 131-136

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24. Method of Supercooled Cryogenic Liquid Production

Gudymenko D. I., Kuda S. А., Logvinenko A. I., Porubaimekh V. I.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 137-140

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25. Vacuum Conditions Simulation Criteria

Logvinenko A. I.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 141-145

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26. State of the Art and Prospects for Nuclear-Quadrupole Resonance Thermometry in Ukraine

Karpenko V. D., Kovalchuk N. О., Lenovenko А. М., Solod S. D., Suvorov O. G.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 146-150

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27. Solution of "Unsolvable" Problems

Pavlysh I. F.

Мова: Russian

Kosm. teh. Raket. vooruž. 2017 (2); 151-168

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File of Issue № 2 (2017)
File of Issue № 2 (2017)
File of Issue № 2 (2017)
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