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.

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Presentation transcript:

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

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

Design Overview

Prediction Software

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

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

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

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

Fin Design

Motor Selection K1275-W lbf*sec

Electronics Section

Electronics

Nose Cone Section

Payload Bay

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

Recovery Systems

Full System

Testing Rope G-Force Compression of Tubing Parachute Ring Strength

Rope G-Force Testing

Phenolic Tube Compression

Composite Tube Compression

Parachute Rings

Launch Pad

Thanks WSGC Dr. Farrow

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