Project Design Constraints: (from the SAE rule set)
The aircraft system container shall be a cardboard box with absolute maximum
outside dimensions of 12.125 inches X 3.625 inches X 13.875 inches maximum.
Minimum wall thickness of container is 0.125 inches.
Micro Class aircraft must use Lithium Polymer batteries. The maximum size
propulsion system battery allowed for Micro Class is a 3 cell 2200mAh lithium
polymer battery. Batteries having fewer cells and lower capacity are permitted.
Final Design Specs:
15 Degree Dihedral
Twin Boom
6.75” chord
Stall Speed: 40 Mph
Estimated Dry Weight: 1.75 lbs
Estimated Loaded Weight: 3.85 lbs
Budget:
Began with “$2000”
Changed unexpectedly to $750
Final budget updated to be $1500
Current remaining budget is $778.53
Timeline and Gantt Chart:
