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For the phase II airframe element design, are the teams expected to modify the basline CAD assemblies by creating their own payload and power supply elements in CREO and adding them to the airframe assembly? What kind of performance analysis are they to perform in MATHCAD?
You can actually modify the basic airframe design in Phase I. There are design parameters within the MATHCAD worksheets that you can modify, and then files are output that can be used to show your new design in CREO