1. Team Members:Tony Guzzo Eric Jacob Bill Liewehr Alex Schlaupitz Design of a Level 2 Rocket for the Wisconsin Space Grant Consortium Advisor: Dr. William Farrow

2. Project Summary Engineer a Rocket for the WSGC Capable of lifting Payloads Efficiency in Design Ease of use

3. Design Overview

6. Prediction Software

12. Internal Motor Section Components Motor Bulkhead Motor Mount Tube Centering Rings Rear Motor Ring

13. Internal Structural Design Parachute Rings –6061 Aluminum –0.13 in. thickness –1.06 oz. weight –0.60 in. holes Centering Rings –Yellow Birch –0.125 in. thickness –0.12 oz. weight

14. Internal Structural Design Motor Mount Tube Bulkhead –6061 Aluminum –0.08 in. thickness –0.45 oz. weight

15. Internal Structural Design Parachute Rings –Max Stress 39,350 psi –Factor of Safety of 1.5 Motor Mount Bulkhead –Max Stress 15,010 psi –Factor of Safety of 2.66

16. Fin Design

18. Motor Selection K1275-W 2132.31 lbf*sec

19. Electronics Section

20. Electronics

21. Nose Cone Section

22. Payload Bay

24. Main Body and Coupler Tubing Composite Tubing –0.028 in. thickness –2.696 oz./ft. Epoxies and Fillers

25. Recovery Systems

26. Full System

27. Testing Rope G-Force Compression of Tubing Parachute Ring Strength

28. Rope G-Force Testing

29. Phenolic Tube Compression

30. Composite Tube Compression

31. Parachute Rings

32. Launch Pad

33. Thanks WSGC Dr. Farrow