Content 2017 (2)

File of Issue № 2 (2017)
 

ISSN 2617-5525; e-ISSN 2617-5533

Issue № 2 (2017)

Date of publication: 01.11.2017

Authors of the issue

 

 

 

 

 

 

 

Contents:

1. DO-2 – Semicentenary

Shevtsov Е. I.

Language: 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. А., Makarenko А. А., Silkin А. Y., Shevtsov Е. I.

Language: Russian
Kosm. teh. Raket. vooruž. 2017 (2); 5-11
 
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3. Creation of Advanced Facilities for Spacecraft / Launch Vehicle Integration

Makarenko А. А., Mashchenko А. N., Shevtsov Е. I.

Language: 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 А. I.

Language: 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 А. А., Shevtsov Е. I.

Language: 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 М. L., Kuda S. А., Mikhalchishin R. V.

Language: 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.

Language: 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.

Language: 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. N., Kuda S. А., Lomskoy D. А.

Language: 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., Smolensky D. E.

Language: Russian
Kosm. teh. Raket. vooruž. 2017 (2); 53-56
 
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11. Remote Monitoring Method of Pneudraulic System Structural Elements Integrity

Babiy А. N., Tishchenko Y. S., Mogilevtsev А. А.

Language: 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 Е. P., Yakimets S. V.

Language: 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 А. А., Mashchenko А. N., Nazarenko Е. P., Skochko V. V., Ustich V. V., Shevtsov Е. I.

Language: Russian
Kosm. teh. Raket. vooruž. 2017 (2); 65-69
 
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14. Development Test of Isolating Valve Operation under Cryogenic Conditions

Makarenko А. А., Udovichenko D. А.

Language: Russian
Kosm. teh. Raket. vooruž. 2017 (2); 70-76
 
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15. Oxidizer Feedline Structural Optimization Results

Veskov Е. V., Nazarenko Е. P., Sedykh I. V., Shevchenko B. А.

Language: Russian
Kosm. teh. Raket. vooruž. 2017 (2); 77-82
 
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16. Determination of Spherical Flange Connections Gasket Clamping Site Width

Onofrienko V. I., Shevtsov Е. I., Makarenko А. А.

Language: 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 А. А., Shevtsov Е. I.

Language: 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 Е. I.

Language: 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 А. I., Khomyak V. А.

Language: 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 А. М., Kovalenko V. А., Kondrat’ev А. V., Gaidachuk V. Е.

Language: Russian
Kosm. teh. Raket. vooruž. 2017 (2); 112-120
 
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21. Mass Parameter Optimization of Thermal Protective Structure for Reusable Spacecraft

Gusarova I. А., Potapov А. М., Shevtsov Е. I., Onofrienko V. I., Gusev V. V., Manko Т. А.

Language: 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 А. А., Tishchenko Y. S.

Language: 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 Е. I., Gusev V. V.

Language: 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 А. I., Porubaimekh V. I.

Language: Russian
Kosm. teh. Raket. vooruž. 2017 (2); 137-140
 
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25. Vacuum Conditions Simulation Criteria

Logvinenko А. I.

Language: 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 А. G.

Language: Russian
Kosm. teh. Raket. vooruž. 2017 (2); 146-150
 
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27. Solution of "Unsolvable" Problems

Pavlysh I. F.

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