2. Overview Project Schedule Competition Technology Report Construction Progress Future Work Conclusion

3. Project Schedule

4. Competition Technology Report http://dasp.mem.odu.edu:8080/~aero_sp15/TechReport.pdf

5. Competition Technology Report

6. Von-Mises Stress of 1.43 ksi Maximum vertical displacement of 0.017 inches

7. 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

8. Truss Fuselage Wing Motor Mount Tail Section Construction Progress

12. Nose cone Gussets and ply sections for the fuselage Tail section/fuselage integration Wing/fuselage integration Main Wheel Fabrication Monokote Future Work

13. 1/8 th inch Ply Sections Gusset Sections

14. Questions?