ISSN 2617-5525; e-ISSN 2617-5533
Issue № 1 (2017)
Date of publication: 22.03.2017
Contents:
1. Methodology for Measurement Uncertainty Evaluation during Metrological Certification of Measuring Instruments
Bondar’ М. А., Voloshina M. O., Yeres L. O., Kurako I. М., Noskov S. I.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (1); 3-7
Annotation | Full Text (PDF)2. Ultimate Stability Stresses in Smooth Cylindrical Skins. Dynamic Problem
Kaplya P. G.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (1); 8-17
Annotation | Full Text (PDF)3. Development Strength Test of Modified Antares ILV
Klimenko D. V., Kuryachiy Е. V., Mishchenko O. I., Frolov V. P.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (1); 18-22
Annotation | Full Text (PDF)4. Basic Selection Criteria of Heat-Resistant and Thermal Protective Structures for High-Altitude Hypersonic Flying Vehicle
Husarova I. O., Potapov O. М., Golubkov G. М., Kalinichenko D. S., Poluyan M. V., Manko Т. А.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (1); 23-29
Annotation | Full Text (PDF)5. Development of Working Liquid Discontinuity Measurement Procedure and Its Certification
Bondar’ М. А., Huseva H. S., Yeres L. O., Kurako I. М., Petrenko Y. M., Rozmaita N. Yu.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (1); 30-34
Annotation | Full Text (PDF)6. Drought Post-Effects Satellite Monitoring
Masley V. M., Belousov К. G., Khoroshilov V. S., Bushanskaya O. S., Mozgovoy D. К., Vasilyev V. V.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (1); 35-42
Annotation | Full Text (PDF)7. Static Approach Application in Analysis of Gas-Dynamic Parameters in Launch Vehicle Vented Bays
Sirenko V. M., Il’enko P. V., Semenenko P. V.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (1); 43-47
Annotation | Full Text (PDF)8. Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions
Muliar Yu. M., Fedorov V. M., Tryasuchev L. М.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (1); 48-58
Annotation | Full Text (PDF)9. Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles
Oliinyk V. P., Yelansky Y. A., Kaluger L. G.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (1); 59-66
Annotation | Full Text (PDF)10. Features of Measurement System for Gas-Dynamic Model Tests of Rocket Complex Elements
Aksiuta О. А., Brynza S. I., Zavialov P. P.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (1); 67-69
Annotation | Full Text (PDF)11. Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors
Sokolov O. V., Sheiko А. F., Fomenko V. S., Kirichenko A. S.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (1); 70-77
Annotation | Full Text (PDF)12. Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator
Tsyganov V. M.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (1); 78-83
Annotation | Full Text (PDF)13. Reliability Evaluation of ILV Thermostating System Mating Hoses
Bigun S. O., Khorolskyi M. S., Skokov O. I.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (1); 84-87
Annotation | Full Text (PDF)14. Design Studies into Dynamic and Structural Characteristics of Two-Stage Direct-Action Solenoid-Operated Hydraulic Valve
Boiko V. S.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (1); 88-94
Annotation | Full Text (PDF)15. Assessment of Liquid Equipment Neutralization Method Effectiveness
Pozdieiev H.L., Berezina K. М.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (1); 95-99
Annotation | Full Text (PDF)16. Principal Directions for Creation of Integrated Launch Vehicle Autonomous Onboard Flight Safety System
Deno О. N., Filonenko А. V., Didenko O. V., Tkalenko G. V.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (1); 100-106
Annotation | Full Text (PDF)17. Peculiarities of Design and Development Test of Dispenser Turning Actuator System for SHM with Iridium NEXT SC
Zhilenkova N. M., Kholoshnya I. S., Degtyareva O. Y., Babich I. P.Мова: Russian
Kosm. teh. Raket. vooruž. 2017 (1); 107-110
Annotation | Full Text (PDF)