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ETA beginning of December
RSU:
Tasks:
Find out distance between bottom of aero body and chassis tube
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Apply loading to nodal and make changes where needed
RSU:
Short meeting, mostly wanted to touch base and get a direction for us to move forward.
Discussed MS15 nodal, investigated how varying parameters such as arm length has an impact on performance
Went over design constraints for MS16
Looked into a good location to place the global system datum: settled on using one of the welded tabs, this might change later but will be locked in soon.
Tasks:
Work on creating a new parametric nodal diagram based on MS15’s RSU. We will make adjustments to this as needed for MS16.
The key is to move the part origin to where we want our system datum to be, i.e. if we want it on the welded tab for the shock, make the origin up there.
Make use of as many equations as possible (make it parametric) so it’s easier to adjust later