Сontent 2016 (1)
File of Issue № 1 (2016)
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. G.
2. Experience of Testing SRM Thrust Vector Controls
Golubenko N. S., Kushnir B. I., Zenzerov V. A.
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.
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.
5. Scientific-Technical Base for Creation of Detonation Solid Rocket Motors
Kovalenko N. D., Kukushkin V. I., Ignat’yev A. D., Kirichenko А. О.
6. Ensuring Solid Rocket Motor Moisture Resistance by Design
Sirik Y. P., Lyakh Y. A., Babey Y. N., Pomin O. V.
7. Updated Design of SRM Test Rig
Bezkrovny I. B., Tregubenko О. О., Krivsun R. Y.
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.
9. Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method
Fomenko V. S., Kalnysh R. V., Popov V. A.
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.
11. Methodology of Design Evaluation of Main SRM Flowrate-Thrust Characteristics after Stage Separation
Ushkin N. P., Moroz V. G., Tikhaya M. V.
12. Increasing Effectiveness of Meteorological Rockets when Using Hybrid Motors
Orekhov K. N.
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.
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.
15. Calculation of Solid Propellant Grain Burning Surface Using Automated 3D-Modeling Systems
Toloch’yants G. E., Lepsky A. V.
16. Peculiarities of Development of SRM Thrust Vector Controls at DO-5
Slisarenko V. F.
17. Modeling of Solid Rocket Motor Starting Process
Tikhaya M. V., Bucharsky V. L., Orekhov K. N.
18. Method of Design Evaluation of SRM Lifetime and Ensuring its Long-Term Operation
Ushkin N. P.
19. Blade Geometry for Maximal Power Coefficient and Minimal Noise Level
Kalnysh R. V.
20. Determination of External Characteristic of Autonomous WPP for Regulation by Rotor Withdrawal from under Wind
Kalnysh R. V., Popov V. A.
21. Selection of Optimal Parameters of Wind Desalting System with Hydrogen Energy Storage Unit
