Content 2017 (1)

File of Issue № 1 (2017)
 

ISSN 2617-5525; e-ISSN 2617-5533

Issue № 1 (2017)

Date of publication: 22.03.2017

Authors of the issue

 

 

 

 

 

 

 

Contents:

1. Methodology for Measurement Uncertainty Evaluation during Metrological Certification of Measuring Instruments

Bondar М. А., Voloshina М. А., Yeres L. A., 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 А. 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

Gusarova I. А., Potapov А. М., Golubkov G. М., Kalinichenko D. S., Poluyan N. V., Man’ko 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., Guseva А. S., Yeres L. A., Kurako I. М., Petrenko Y. N., 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. N., Belousov К. G., Khoroshilov V. S., Bushanskaya А. 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. N., 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

Mulyar Yu. М., Fyodorov V. М., Tryasuchev 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

Oleinik V. P., Yelansky Y. А., 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., Zav’yalov 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 А. V., Sheiko А. F., Fomenko V. S., Kirichenko А. 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. N.

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. А., Khorolsky М. S., Skokov А. 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

Pozdeev G. L., Berezina Е. 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 А. 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. N., Kholoshnya I. S., Degtyareva Е. Y., Babich I. P.

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