Сontent 2016 (1)

File of Issue № 1 (2016)
 

ISSN 2617-5525; e-ISSN 2617-5533

Issue № 1 (2016)

Date of publication: 23.03.2016

Authors of the issue

 

 

 

 

 

 

 

Contents:

1. Solid Rocket Motors Developed by DO-5

Kirichenko A. S., Kushnir B. I., Yenotov V. G.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 4-12
 
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2. Experience of Testing SRM Thrust Vector Controls

Golubenko N. S., Kushnir B. I., Zenzerov V. A.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 13-18
 
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3. On Peculiarities of Life Testing and Safe Storage of Solid Rocket Motors

Kirichenko A. S., Balitsky I. P., Rogulin V. V., Chepel G. N., Tutov N. I.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 19-25
 
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4. The Company’s Experience in Designing and Operating Special Bench Equipment for SRM Ground Tests

Kirichenko A. S., Beskrovny I. B., Krivsun R. Y., Rogulin V. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 26-33
 
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5. Scientific-Technical Base for Creation of Detonation Solid Rocket Motors

Kovalenko N. D., Kukushkin V. I., Ignat’yev A. D., Kirichenko А. О.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 34-45
 
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6. Ensuring Solid Rocket Motor Moisture Resistance by Design

Sirik Y. P., Lyakh Y. A., Babey Y. N., Pomin O. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 46-51
 
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7. Updated Design of SRM Test Rig

Bezkrovny I. B., Tregubenko О. О., Krivsun R. Y.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 52-54
 
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8. Assessment of Validity of Hypothesis of Constancy of Specific Vacuum Thrust Pulse during SRM Designing and Testing

Kalnysh R. V., Kirichenko A. S., Fomenko V. S.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 55-58
 
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9. Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method

Fomenko V. S., Kalnysh R. V., Popov V. A.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 59-62
 
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10. Development of Winding Pattern during Calculation of Composite Case Winding Programs

Borisenko S. V., Maly L. P., Lavreshov V. V., Kramarenko E. N., Burkun S. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 63-67
 
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11. Methodology of Design Evaluation of Main SRM Flowrate-Thrust Characteristics after Stage Separation

Ushkin N. P., Moroz V. G., Tikhaya M. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 68-75
 
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12. Increasing Effectiveness of Meteorological Rockets when Using Hybrid Motors

Orekhov K. N.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 76-81
 
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13. The Impact of Diaphragm’s Shape on Gas Dynamic Flow Characteristics in Small-Size SRM Combustion Chamber

Vakhromov V. A., Oglikh V. V., Toloch’yants G. E., Magdin E. K.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 82-87
 
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14. Development of Powder Pressure Accumulators for Rocket Cold Start - the Most Important Condition of its Successful Realization

Oglikh V. V., Vakhromov V. A., Kirichenko A. S., Kosenko M. G.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 88-92
 
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15. Calculation of Solid Propellant Grain Burning Surface Using Automated 3D-Modeling Systems

Toloch’yants G. E., Lepsky A. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 93-96
 
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16. Peculiarities of Development of SRM Thrust Vector Controls at DO-5

Slisarenko V. F.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 97-104
 
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17. Modeling of Solid Rocket Motor Starting Process

Tikhaya M. V., Bucharsky V. L., Orekhov K. N.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 105-109
 
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18. Method of Design Evaluation of SRM Lifetime and Ensuring its Long-Term Operation

Ushkin N. P.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 110-116
 
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19. Blade Geometry for Maximal Power Coefficient and Minimal Noise Level

Kalnysh R. V.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 117-121
 
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20. Determination of External Characteristic of Autonomous WPP for Regulation by Rotor Withdrawal from under Wind

Kalnysh R. V., Popov V. A.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 122-127
 
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21. Selection of Optimal Parameters of Wind Desalting System with Hydrogen Energy Storage Unit

Kalnysh R. V., Los’ S. I.

Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 128-132
 
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