Igrickii

pp. 459-476

The article describes aspects of the design analysis of strength of ground equipment truss structure loaded with the high temperature jet of launch vehicle engines. The reasonable limitations and calculating model development concepts for the thermal strength calculations were analyzed. Basics of the overall strength analysis were given. The truss structure local thermal strength analysis was considered by the example of joint of piped elements.

The article describes the aspects of small satellite attitude control system scaled-down simulation facility modular structure development. The rational methods of satellite attitude control system scaled-down simulation universal facility development are analyzed. Effective user interface design solutions are suggested. The reasonable limitations of the facility application field are considered. The principles of hardware real-time performance are proposed.