2. Ultimate Stability Stresses in Smooth Cylindrical Skins. Dynamic Problem
Kaplya P. G.
3. Development Strength Test of Modified Antares ILV
Klimenko D. V., Kuryachiy Е. V., Mishchenko А. I., Frolov V. P.
4. Basic Selection Criteria of Heat-Resistant and Thermal Protective Structures for High-Altitude Hypersonic Flying Vehicle
Gusarova I. А., Potapov А. М., Golubkov G. М., Kalinichenko D. S., Poluyan N. V., Man’ko Т. А.
5. Development of Working Liquid Discontinuity Measurement Procedure and Its Certification
Bondar М. А., Guseva А. S., Yeres L. A., Kurako I. М., Petrenko Y. N., Rozmaita N. Yu.
6. Drought Post-Effects Satellite Monitoring
Masley V. N., Belousov К. G., Khoroshilov V. S., Bushanskaya А. S., Mozgovoy D. К., Vasilyev V. V.
7. Static Approach Application in Analysis of Gas-Dynamic Parameters in Launch Vehicle Vented Bays
Sirenko V. N., Il’enko P. V., Semenenko P. V.
8. Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions
Mulyar Yu. М., Fyodorov V. М., Tryasuchev L. М.
9. Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles
Oleinik V. P., Yelansky Y. А., Kaluger L. G.
10. Features of Measurement System for Gas-Dynamic Model Tests of Rocket Complex Elements
Aksiuta О. А., Brynza S. I., Zav’yalov P. P.
11. Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors
Sokolov А. V., Sheiko А. F., Fomenko V. S., Kirichenko А. S.
12. Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator
Tsyganov V. N.
13. Reliability Evaluation of ILV Thermostating System Mating Hoses
Bigun S. А., Khorolsky М. S., Skokov А. I.
14. Design Studies into Dynamic and Structural Characteristics of Two-Stage Direct-Action Solenoid-Operated Hydraulic Valve
Boiko V. S.
15. Assessment of Liquid Equipment Neutralization Method Effectiveness
Pozdeev G. L., Berezina Е. М.
16. Principal Directions for Creation of Integrated Launch Vehicle Autonomous Onboard Flight Safety System
Deno О. N., Filonenko А. V., Didenko А. V., Tkalenko G. V.
17. Peculiarities of Design and Development Test of Dispenser Turning Actuator System for SHM with Iridium NEXT SC
