1. Evan Akselrad, Chris Anaya, Natalie Bixler, Melanie Dubin, Logan Finch, Ted Maritz, and Scott Williams November 11, 2008

2. Mission Overview  The BalloonSat Flight Club shall ascend to an altitude of 30 kilometers to image the curvature and surface of the Earth, and to measure the light intensity at different altitudes to determine if commercial aviation has an impact on light intensity levels. This shall be accomplished by measuring current using solar panels attached to the payload.

3. Design Overview These pictures and technical diagrams show the construction and design of the BallonSat, Flight Club.

4. Test Results Science Mission Testing This graph shows the first successful test of the science mission. This was after we had to redesign the circuit to be parallel. This shows the raw data gathered from the logger.

5. Test Results Continued This graph show the data after we have employed the equation V=IR, and taken into account the 0.5V lost in the diodes. Therefore this graph shows current. We expect current to increase with light intensity as the payload ascends to altitude.

6. Test Results Continued Structural Testing Drop Test Cold Test The structural tests showed that the payload for Team Flight Club is structurally sound and ready for launch.

7. Prediction of Actual Flight Results  Find noticeable discrepancy in the rate of change of light intensity at the altitude at which commercial jets fly. Such a discrepancy will indicate that the exhaust and contrails produced by jets affect the amount of light that reaches the Earth’s surface.

8. Worries and Concerns…  At this point we feel that our biggest worry is that something will happen on launch day, such as switch not getting flipped correctly.  We are concerned that connections could come loose during takeoff/the flight  The HOBO taking correct readings

9. Mission RequirementsCompleted Design shall have one additional experiment that collects science data.The design shall implement a light intensity experiment. After flight, BalloonSat shall be turned in working and ready to fly again.The BalloonSat has been tested to ensure that the BalloonSat shall survive flight. Flight string interface tube shall be a non-metal tube through the center of the BalloonSat and shall be secured to the box so it will not pull through the BalloonSat or interfere with the flight string. A non-metal tube has been installed into the BalloonSat. Internal temperature of the BalloonSat shall remain above 0ºC during the flight.Several cold tests have been conducted to ensure that the internal temperature shall not fall below 0ºC during flight. Total weight shall not exceed 1000 grams.The BalloonSat weighs 881.24 grams. Each team shall acquire (not necessarily measure) ascent and descent rates of the flight string. The Helium Balloon operator shall be contacted to retrieve ascent and descent rates. Design shall allow for a HOBO H08-004-02 68x48x19 mm and 29 grams.The HOBO has been implemented into the design. Design shall allow for external temperature cable.The external temp. cable has been implemented into the design. Design shall allow for a Canon A570IS Digital Camera 45x75x90 mm and 220 grams. The digital camera has been implemented into the design. BalloonSat shall be made of foam core.The BalloonSat has been constructed with foam core. Parts list and budget shall include spare parts.Spare parts have been included into the budget. All BalloonSats shall have contact information written on the outside along with a US Flag. Contact information and a US Flag has been attached to the BalloonSat. Units shall be in metric.Units are in metric. Launch is on November 15, 2008. Time and location: 7:30 AM in Windsor, CO. Launch schedule will be given later. Everyone is expected to show up for launch. Only one team member is required to participate on the recovery. Launch and recovery should be completed by 3:00 PM. Due to recent changes in FAA regulations, the launch will most likely occur at sunrise. All other requirements shall be followed. No one shall get hurt.No one has gotten hurt. All hardware is the property of the Gateway to Space program and must be returned at the end of the semester. All hardware shall be returned following flight and analysis. All parts shall be ordered and paid by Chris Koehler’s CU Mastercard by appointment to minimize reimbursement paperwork. All teams shall keep detailed budgets on every purchase and receipts shall be turned in within 48 hours of purchase with team name written on the receipt. All parts have been ordered using Chris Koehler’s CU Mastercard with proper documentation. A detailed budget has been kept. All purchases made by team individuals shall have receipts and must be submitted within 60 days of purchase or reimbursement will be subject to income taxes. All purchases made by team individuals have been properly documented. Have fun and be creative.All team individuals have been having fun and being creative throughout the project. Absolutely nothing alive will be permitted as payloads with the exception of yellow jackets, mosquitoes, fire ants, earwigs, roaches, or anything you would squish if you found it in your bed. No live animals shall be present during flight. Completion of final report (extra credit if team video is included)The final report shall be completed. Proposal Compliance Matrix