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Dionysus Final Presentation 12/01/09

Dionysus Final Presentation 12/01/09. Alijah Smith Josh Tiras Chris Koncilja Mike Beach Elise Kowalski Becca Seigel. ESAM. Mission Overview. ESAM’s mission is to send a balloon satellite to an altitude of 30 kilometers in order to collect wattage data of the electromagnetic spectrum.

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Dionysus Final Presentation 12/01/09

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  1. DionysusFinal Presentation 12/01/09 Alijah Smith Josh Tiras Chris Koncilja Mike Beach Elise Kowalski Becca Seigel ESAM

  2. Mission Overview • ESAM’s mission is to send a balloon satellite to an altitude of 30 kilometers in order to collect wattage data of the electromagnetic spectrum. • An infrared sensor and an ultraviolet sensor will be used in order to determine the flux of infrared and ultraviolet light throughout the troposphere and lower stratosphere. • The sensors will collect data in the ranges of 210-380nm in the ultraviolet and 750-1400 in the infrared. • We expect to see an increase in both infrared and Ultraviolet intensity as a function of altitude.

  3. Proposed 1 UV sensor Square structure Sensors without extra hardware X-ray photodiode Actual 3 UV sensors Triangular prism with some slanted sides Resistors for UV sensors, opperational amplifier for IR sensor No X-ray photodiode Differences

  4. Design Overview Hardware • 3 UV sensors • 1 IR sensor • AVR and misc. • Camera • Structure

  5. Ultraviolet Sensor

  6. Infrared Sensor

  7. All Sensors

  8. Everything!

  9. Structure

  10. Results and Analysis • Predicted: Ultraviolet and infrared light intensity will increase as altitude increases • Actual: • Ultraviolet intensity increases as altitude increases • Infrared light intensity did not continuously increase

  11. Internal Temp

  12. External Temp

  13. Pressure

  14. UV Sensor 1

  15. UV Sensor 2

  16. UV Sensor 3

  17. IR Sensor

  18. Failure Analysis • AVR camera activation failed • When plugged in, the camera immediately turned on. • Several attempts to unplug and re-plug. • Camera now fixed, polarity of wires reversed. • Not actually a big deal, didn’t effect pictures… • ready for re-fly!

  19. Conclusions • UV light increases with altitude • Ground flux: ~0 W/m^2 • Max flux: ~1.4 W/m^2 • IR light more complicated • Possible sensor malfunction.

  20. IR graph

  21. Lessons Learned What we would have done differently. • Time management (baseline testing, opp amp) • Better understanding of opp amp hardware • Better understanding of parsing data. • Use two more IR sensors for more accurate data If we could change it… • Better time management • Debugging AVR sooner, rather than later

  22. Re-fly • Storage: taped shut but not sealed to store it until the next flight. • Activated for next flight: Payload should: • be carefully sliced open • have the batteries replaced • be armed • be sealed shut before it will be fully ready to fly again.

  23. Minimum Temperature: .28889 C˚ Weight: 931 g

  24. Message to Next Semester Some people seemed to dislike this class but we really liked it. We had a good group that worked well together and has diverse talents/knowledge coming into the project. We were fortunate enough to have people with backgrounds in computing, astronomy, business, and leadership. Be prepared to work a lot but…it’s really not that bad, just manage your time well. Expect to work more than once a week; we met three times a week and still ran out of time. Even if you think you’re ahead of schedule, don’t take a week off, keep working. Also learn as much about your hardware as much as you can so that when “the sh*t hits the fan” you know how to fix it. Team leader, don’t be afraid to tell your team what to do. Assign them different sections of the DD and make sure they get done when you want them done. Overall this class was a valuable learning experience in more ways than just launching a satellite. And it was fun!

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