1 / 33

Team Members: Tony Guzzo Eric Jacob Bill Liewehr Alex Schlaupitz

Design of a Level 2 Rocket for the Wisconsin Space Grant Consortium. Team Members: Tony Guzzo Eric Jacob Bill Liewehr Alex Schlaupitz. Advisor: Dr. William Farrow. Project Summary. Engineer a Rocket for the WSGC Capable of lifting Payloads Efficiency in Design

brook
Download Presentation

Team Members: Tony Guzzo Eric Jacob Bill Liewehr Alex Schlaupitz

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


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

  4. Prediction Software

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

  6. 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

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

  8. 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

  9. Fin Design

  10. Motor Selection • K1275-W • 2132.31 lbf*sec

  11. Electronics Section

  12. Electronics

  13. Nose Cone Section

  14. Payload Bay

  15. Payload Bay

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

  17. Recovery Systems

  18. Full System

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

  20. Rope G-Force Testing

  21. Phenolic Tube Compression

  22. Composite Tube Compression

  23. Parachute Rings

  24. Launch Pad

  25. Thanks • WSGC • Dr. Farrow

More Related