2. Mathematical models for assessment of safety in the impact area of cluster ammunition of the warhead during missile complex testing
Hladkiy E. G.
3. Features of design and production of the technological aids for assembly of the spacecraft separation system of CLAMP BAND type
Kodenets D. A., Sencha S. A., Makarenko A. A.
4. Numerical simulation of behavior of elastic structures with local stiffening elements
Hudramovich V. S., Hart E. L., Strunin K. A.
5. Features of the development testing of the propellants deposition inside the tanks of launch vehicles
Sedykh I. V., Nazarenko D. S., Smolenskiy D. E.
6. Stabilization of gas reducers adjustment
Nazarenko Y. P., Reuta V. I., Makarov A. D.
7. On critical stress of the longitudinal stability of the stiffened cylindrical shells. Dynamic problem
Kaplya P. G.
8. Evaluation of the external acoustic loads, acting on the rocket when it passes the leg with maximum velocity head
Batutina T. Y., Bondar’ D. S., Grinchenko V. T., Olyinick V. N.
9. Gas-dynamic simulation of the supersonic stream in the pulsed wind tunnel
Sirenko V. N., Zhivotov A. Y.
10. Dynamic performance of the gas drive with jet motor
Oleinyk V. P., Kaluger L. G.
11. Winding the tubes of rectangular section using dowels
Lavreshov V. V., Maliy L. P., Kovalev Y. V., Kramarenko Y. N., Omelchenko D. S.
12. Procedure of acoustic loads measuring during the ILV launch
Batutina T. Y., Bondar’ D. S.
13. Study of the stress and strain state of the multilayer bellows
Vasilieva T. N., Strunin K. A., Onofrienko V. I.
14. Selection of the validation algorithm for the solid rocket motor trust measurement procedure
