1. Pre-Flight Briefing ANSR-78 Pima Community College 11/23/13 Robert Hendrickson Ling Bin Lu Levi Kerns Roger Page Alex Grebenchtchikov Team Members

2. Payload 1 Design Process Spacious while remaining light Include at least two different sensors Extra space for insulation Reduce unnecessary weight from the components Test all sensors Test pod and electronics at -50°C

3. Payload 1 Structure A simple box shape with plenty of room A large volume while remaining lightLeaves plenty of room for insulation

4. Payload 1 Data Inputs Temperature: One sensor on the inside Relative Humidity: one sensor on the outside

5. Payload 2 Launch a self-contained, self-powered video recording device Maintain minimum payload rotation by expanding on the use of bearings that were successfully used by the 2012 PCC team Minimize Weight View Angle Maintain safe operational temperature for the iPod Motivation: Styrofoam Polyester Winter Pants Aluminum Rod Carbon Fiber Fish-Eye Lens Temperature Recording Unit iPod Touch 5th Generation Side-View Cross Section

6. Payload 2 Design Benefits Model B Model A Balanced Rotation Cylindrical Shape Better Structural Integrity Hemispherical "Bullet Shape

7. Payload 2 Testing Results Properly counter-balanced bearing rotation Stronger Impact Resistance Higher Resistance to Cold Temperature Model A Chosen:

8. Payload 2 Final Product

9. Acknowledgements Special thanks to the following: Jack Crabtree and ANSR Susan Brew and NASA Space Grant Mike Sampogna Dr. Denise Meeks