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.

Language: Russian

Kosm. teh. Raket. vooruž. 2017 (1); 3-7

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2. Ultimate Stability Stresses in Smooth Cylindrical Skins. Dynamic Problem

Kaplya P. G.

Language: Russian

Kosm. teh. Raket. vooruž. 2017 (1); 8-17

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3. Development Strength Test of Modified Antares ILV

Klimenko D. V., Kuryachiy Е. V., Mishchenko O. I., Frolov V. P.

Language: Russian

Kosm. teh. Raket. vooruž. 2017 (1); 18-22

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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.

Language: Russian

Kosm. teh. Raket. vooruž. 2017 (1); 23-29

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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.

Language: Russian

Kosm. teh. Raket. vooruž. 2017 (1); 30-34

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6. Drought Post-Effects Satellite Monitoring

Masley V. M., Belousov К. G., Khoroshilov V. S., Bushanskaya O. S., Mozgovoy D. К., Vasilyev V. V.

Language: Russian

Kosm. teh. Raket. vooruž. 2017 (1); 35-42

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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.

Language: Russian

Kosm. teh. Raket. vooruž. 2017 (1); 43-47

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8. Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions

Muliar Yu. M., Fedorov V. M., Triasuchov L. М.

Language: Russian

Kosm. teh. Raket. vooruž. 2017 (1); 48-58

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9. Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles

Oliinyk V. P., Yelanskyi Yu. A., Kaluger L. G.

Language: Russian

Kosm. teh. Raket. vooruž. 2017 (1); 59-66

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10. Features of Measurement System for Gas-Dynamic Model Tests of Rocket Complex Elements

Aksiuta О. А., Brynza S. I., Zavialov P. P.

Language: Russian

Kosm. teh. Raket. vooruž. 2017 (1); 67-69

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11. Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors

Sokolov O. V., Sheiko А. F., Fomenko V. S., Kirichenko A. S.

Language: Russian

Kosm. teh. Raket. vooruž. 2017 (1); 70-77

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12. Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator

Tsyganov V. M.

Language: Russian

Kosm. teh. Raket. vooruž. 2017 (1); 78-83

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13. Reliability Evaluation of ILV Thermostating System Mating Hoses

Bigun S. O., Khorolskyi M. S., Skokov O. I.

Language: Russian

Kosm. teh. Raket. vooruž. 2017 (1); 84-87

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14. Design Studies into Dynamic and Structural Characteristics of Two-Stage Direct-Action Solenoid-Operated Hydraulic Valve

Boiko V. S.

Language: Russian

Kosm. teh. Raket. vooruž. 2017 (1); 88-94

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15. Assessment of Liquid Equipment Neutralization Method Effectiveness

Pozdieiev H.L., Berezina K. М.

Language: Russian

Kosm. teh. Raket. vooruž. 2017 (1); 95-99

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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.

Language: Russian

Kosm. teh. Raket. vooruž. 2017 (1); 100-106

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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.

Language: Russian

Kosm. teh. Raket. vooruž. 2017 (1); 107-110

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