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File of Issue № 1 (2016)

ISSN 2617-5525; e-ISSN 2617-5533
Issue № 1 (2016)
Date of publication: 23.03.2016

ZBORNIK_2016_1

ISSN 2617-5525; e-ISSN 2617-5533

Issue № 1 (2016)

Date of publication: 23.03.2016

Contents:

1. Solid Rocket Motors Developed by DO-5

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

Мова: Russian

Kosm. teh. Raket. vooruž. 2016 (1); 4-12.

Annotation | Full Text (PDF)

2. Experience of Testing SRM Thrust Vector Controls

Golubenko M. S., Kushnir B. I., Zenzerov V. O.

Мова: 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., Rohulin V. V., Chepel G. N., Tutov M. I.

Мова: 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., Bezkrovny І. B., Krivsun R. Y., Rohulin V. V.

Мова: 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 M. D., Kukushkin V. I., Ignat’yev O. D., Kirichenko O. O.

Мова: Russian

Kosm. teh. Raket. vooruž. 2016 (1); 34-45

Annotation | Full Text (PDF)

6. Ensuring Solid Rocket Motor Moisture Resistance by Design

Sirik Y. P., Lyakh Y. O., Babey Y. M., Pomin O. V.

Мова: Russian

Kosm. teh. Raket. vooruž. 2016 (1); 46-51

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7. Updated Design of SRM Test Rig

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

Мова: Russian

Kosm. teh. Raket. vooruž. 2016 (1); 52-54

Annotation | Full Text (PDF)

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.

Мова: Russian

Kosm. teh. Raket. vooruž. 2016 (1); 55-58

Annotation | Full Text (PDF)

9. Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method

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

Мова: 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., Malyi L. P., Lavreshov V. V., Kramarenko O. M., Burkun S. V.

Мова: 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 M. P., Moroz V. G., Tikhaya M. V.

Мова: Russian

Kosm. teh. Raket. vooruž. 2016 (1); 68-75

Annotation | Full Text (PDF)

12. Increasing Effectiveness of Meteorological Rockets when Using Hybrid Motors

Orekhov K. M.

Мова: 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. O., Oglikh V. V., Toloch’yants G. E., Magdin E. K.

Мова: 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. O., Kirichenko A. S., Kosenko M. G.

Мова: 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.

Мова: 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.

Мова: 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. M.

Мова: Russian

Kosm. teh. Raket. vooruž. 2016 (1); 105-109

Annotation | Full Text (PDF)

18. Method of Design Evaluation of SRM Lifetime and Ensuring its Long-Term Operation

Ushkin M. P.

Мова: Russian

Kosm. teh. Raket. vooruž. 2016 (1); 110-116

Annotation | Full Text (PDF)

19. Blade Geometry for Maximal Power Coefficient and Minimal Noise Level

Kalnysh R. V.

Мова: 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.

Мова: Russian

Kosm. teh. Raket. vooruž. 2016 (1); 122-127

Annotation | Full Text (PDF)

21. Selection of Optimal Parameters of Wind Desalting System with Hydrogen Energy Storage Unit

Kalnysh R. V., Los’ S. I.

Мова: Russian

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

Annotation | Full Text (PDF)
File of Issue № 1 (2016)
File of Issue № 1 (2016)
File of Issue № 1 (2016)
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