ISSN 2617-5525; e-ISSN 2617-5533
Issue № 2 (2016)
Date of publication: 19.09.2016
Contents:
1. On Minimal Aerodynamic Resistance of Rotation Body at Zero Angle of Attack in Hypersonic Non-Viscous Flow
Shekhovtsov V. S.Мова: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 3-8
Annotation | Full Text (PDF)2. Normalization of Technical System Reliability Using Information Approach
Hladkyi Ye. H.Мова: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 9-16
Annotation | Full Text (PDF)3. Selection of Optimal Trajectories of Spacecraft Launch Vehicles
Kompaniyets E. P., Dron’ M. M., Baranov E. Y., Litvin M. G.Мова: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 17-29
Annotation | Full Text (PDF)4. Experimental Investigations of Possibility of Creating Impulse SRM with Short Operation Period
Oglikh V. V., Toloch’yants G. E., Mikhailov M. S., Popkov V. M.Мова: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 30-34
Annotation | Full Text (PDF)5. Creation of Technological Tooling and Testing of Cocoon-Type Cases Manufacturing Technology
Potapov O. М., Kovalenko V. O., Shilina K. V., Shilin S. O., Alyoshin O. V.Мова: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 35-42
Annotation | Full Text (PDF)6. Experimental Investigations into Results of Testing Cyclone-4 ILV Thermostating System Mating Points
Bigun S. O., Khorolskyi M. S., Skokov O. I., Kaplun S. V.Мова: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 43-51
Annotation | Full Text (PDF)7. Analysis of Operation Modes and Selection of Chemical Current Source Included in Autonomous Electric Power Supply Systems of Self-Propelled Launcher
Zemlyanoy K. M., Reva V. S., Frolov V. P., Bezruchko K. V., Azarnov O. L., Laznenko V. I., Kharchenko А. А.Мова: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 52-56
Annotation | Full Text (PDF)8. Development and Validation of Program Module for Construction of Virtual Models of Real Structures in ANSYS System
Satokin V. V.Мова: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 57-59
Annotation | Full Text (PDF)9. Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands
Bondar’ М. А., Yeres L. O., Kurako I. М., Petrenko Y. M., Goltsev O. S.Мова: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 60-64
Annotation | Full Text (PDF)10. Mathematical Model of High-Flowrate Electropneumatic Valve
Boiko V. S.Мова: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 65-71
Annotation | Full Text (PDF)11. Experimental Investigation into Power Characteristics of Fast-Flowrate Gas Jet Propulsion Systems
Anishchenko V. M.Мова: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 72-74
Annotation | Full Text (PDF)12. The Use of Thermoelectric Technologies in Spacecraft Thermostatic Systems
Loza O. V., Yelansky Y. A., Pokatayev V. M., Karzova O. O.Мова: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 75-79
Annotation | Full Text (PDF)13. Experience of Developing Thermometric Instruments Based on Nuclear Quadrupole Resonance
Karpenko V. D., Solod S. D., Kolesnichenko V. K., Pokatayev V. M., Suvorov O. G.Мова: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 80-84
Annotation | Full Text (PDF)14. Investigation of Deformability of Carbon Plastic Panels in Moisture Absorption Process
Vaisero M. V., Kavun V. V., Kudrevatykh O. Т., Moskalyov S. I., Rozhkovsky V. F., Sokhach Y. V., Shchudro A. P.Мова: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 85-91
Annotation | Full Text (PDF)15. A New Method of Testing Oil-Filled Current Transformers for Explosion-Proofness
Pakhomov S. M., Reznichenko V. I., Mostipan S. E.Мова: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 92-97
Annotation | Full Text (PDF)16. Method of Coefficient for Optimization and Analysis of Operating State of Fine Filter Cases
Satokin V. V.Мова: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 98-101
Annotation | Full Text (PDF)