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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)8. Analysis Method of Nitrogen Tetroxide Tanks Generating Pressurization Systems
Petrenko R. М.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (2); 41-48
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)18. Development Test of Payload Fairing Separation Dynamics under Ground Conditions
Shevtsov E. I.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (2); 102-106
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)25. Vacuum Conditions Simulation Criteria
Logvinenko A. I.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (2); 141-145
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)27. Solution of "Unsolvable" Problems
Pavlysh I. F.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (2); 151-168
Annotation | Full Text (PDF)