Overview Project Schedule Competition Technology Report Construction Progress Future Work Conclusion
Project Schedule
Competition Technology Report
Competition Technology Report
Von-Mises Stress of 1.43 ksi Maximum vertical displacement of inches
Competition Technology Report 10 lbf applied to the front of the mount for a range of frequencies Test flights show that vibrations induced by the motor did not excite natural frequencies of the motor mount
Truss Fuselage Wing Motor Mount Tail Section Construction Progress
Nose cone Gussets and ply sections for the fuselage Tail section/fuselage integration Wing/fuselage integration Main Wheel Fabrication Monokote Future Work
1/8 th inch Ply Sections Gusset Sections
Questions?