For European Space Agency (ESA) needs the work done for Wroclaw University of Technology:
- experimental modal analysis for satellite transmitter with eigenfrequencies and eigenmodes identification,
- detailed numerical model of casing and electronics was developed,
- based on experimental results correctness of numerical model was verified and confirmed
Numerical simulation
Based on verified numercial model the simulation was done:
- design response on random excitation
- design response on harmonic excitation within applied frequency spectrum
- design response on impact excitation
Assessment
Based on simulation results assessment was done:
- technical design correctness of device fixation at satellite panel with included breakdown accidents
- structural static and fatigue strength of the emitter casing
- structural static and fatigue strength of electronic components, printed circuit boards and solder joints
- device compliance with launching system requirements
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