Content 2016 (2)

File of Issue № 2 (2016)
 

ISSN 2617-5525; e-ISSN 2617-5533

Issue № 2 (2016)

Date of publication: 19.09.2016

Authors of the issue

 

 

 

 

 

 

 

Contents:

1. On Minimal Aerodynamic Resistance of Rotation Body at Zero Angle of Attack in Hypersonic Non-Viscous Flow

Shekhovtsov V. S.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 3-8
 
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2. Normalization of Technical System Reliability Using Information Approach

Gladky E. G.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 9-16
 
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3. Selection of Optimal Trajectories of Spacecraft Launch Vehicles

Kompaniyets E. P., Dron’ N. M., Baranov E. Y., Litvin N. G.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 17-29
 
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4. Experimental Investigations of Possibility of Creating Impulse SRM with Short Operation Period

Oglikh V. V., Toloch’yants G. E., Mikhailov N. S., Popkov V. N.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 30-34
 
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5. Creation of Technological Tooling and Testing of Cocoon-Type Cases Manufacturing Technology

Potapov А. М., Kovalenko V. A., Shilina E. V., Shilin S. A., Alyoshin A. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 35-42
 
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6. Experimental Investigations into Results of Testing Cyclone-4 ILV Thermostating System Mating Points

Bigun S. A., Khorolsky M. S., Skokov A. I., Kaplun S. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 43-51
 
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7. Analysis of Operation Modes and Selection of Chemical Current Source Included in Autonomous Electric Power Supply Systems of Self-Propelled Launcher

Zemlyanoy K. N., Reva V. S., Frolov V. P., Bezruchko K. V., Azarnov A. L., Laznenko V. I., Kharchenko А. А.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 52-56
 
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8. Development and Validation of Program Module for Construction of Virtual Models of Real Structures in ANSYS System

Satokin V. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 57-59
 
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9. Metrological Support of Kinematic Model Testing on Zero-Gravity Test Stands

Bondar’ М. А., Yeres L. A., Kurako I. M., Petrenko Y.N., Goltsev A.S.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 60-64
 
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10. Mathematical Model of High-Flowrate Electropneumatic Valve

Boiko V. S.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 65-71
 
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11. Experimental Investigation into Power Characteristics of Fast-Flowrate Gas Jet Propulsion Systems

Anishchenko V. M.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 72-74
 
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12. The Use of Thermoelectric Technologies in Spacecraft Thermostatic Systems

Loza A. V., Yelansky Y. A., Pokatayev V. N., Karzova А. А.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 75-79
 
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13. Experience of Developing Thermometric Instruments Based on Nuclear Quadrupole Resonance

Karpenko V. D., Solod S. D., Kolesnichenko V. K., Pokatayev V. N., Suvorov A. G.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 80-84
 
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14. Investigation of Deformability of Carbon Plastic Panels in Moisture Absorption Process

Vaisero M. V., Kavun V. V., Kudrevatykh А. Т., Moskalyov S. I., Rozhkovsky V. F., Sokhach Y. V., Shchudro A. P.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 85-91
 
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15. A New Method of Testing Oil-Filled Current Transformers for Explosion-Proofness

Pakhomov S. N., Reznichenko V. I., Mostipan S. E.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 92-97
 
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16. Method of Coefficient for Optimization and Analysis of Operating State of Fine Filter Cases

Satokin V. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (2); 98-101
 
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