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.Language: 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.Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 13-18
Annotation | Full Text (PDF)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.Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 19-25
Annotation | Full Text (PDF)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.Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 26-33
Annotation | Full Text (PDF)5. Scientific-Technical Base for Creation of Detonation Solid Rocket Motors
Kovalenko M. D., Kukushkin V. I., Ignat’yev O. D., Kirichenko O. O.Language: 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.Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 46-51
Annotation | Full Text (PDF)7. Updated Design of SRM Test Rig
Bezkrovny І. B., Tregubenko О. О., Krivsun R. Y.Language: 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.Language: 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.Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 59-62
Annotation | Full Text (PDF)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.Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 63-67
Annotation | Full Text (PDF)11. Methodology of Design Evaluation of Main SRM Flowrate-Thrust Characteristics after Stage Separation
Ushkin M. P., Moroz V. G., Tikhaya M. V.Language: 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.Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 76-81
Annotation | Full Text (PDF)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.Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 82-87
Annotation | Full Text (PDF)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.Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 88-92
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)17. Modeling of Solid Rocket Motor Starting Process
Tikhaya M. V., Bucharsky V. L., Orekhov K. M.Language: 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.Language: 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.Language: Russian
Kosm. teh. Raket. vooruž. 2016 (1); 117-121
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)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
Annotation | Full Text (PDF)
