The take home project was to design a concept for internal bracketry for a satellite bus. The bracketry had to structurally isolate the nadir panel which had communication devices that had high pointing accuracy requirements. The brackets must also be able to react a launch load of 10g's. Consider thermal expansion as well.
Explain the work process you would do once you get a package in a project.
Imagine a strut connecting an antenna to a satellite. What are all of the possible failure modes?
I was in sae club of our college so they asked about it like what you have done there.
How would you athermalize a lens system?
With your experience can you actually do the engineering calculations, or do you just design by your experience?
Tell me one thing you physically built by hands either for your university project or outside of university.
Can you tell me about yourself?
What are your aspirations for the role?
Are you okay with working 50-70 hours per week?
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