ISSN 2617-5525; e-ISSN 2617-5533
Issue № 2 (2017)
Date of publication: 01.11.2017
Contents:
1. DO-2 – Semicentenary
Shevtsov E. I.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: 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.Language: Russian
Kosm. teh. Raket. vooruž. 2017 (2); 137-140
Annotation | Full Text (PDF)25. Vacuum Conditions Simulation Criteria
Logvinenko A. I.Language: 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.Language: Russian
Kosm. teh. Raket. vooruž. 2017 (2); 146-150
Annotation | Full Text (PDF)27. Solution of "Unsolvable" Problems
Pavlysh I. F.Language: Russian
Kosm. teh. Raket. vooruž. 2017 (2); 151-168
Annotation | Full Text (PDF)
