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Team Dionysus Critical Design Review

Team Dionysus Critical Design Review. Alijah Smith, Chris Koncilja, Elise Kowalski, Josh Tiras, Mike Beach, Becca Seigel 10/06/09. Organization Chart. Mission Overview. Mission Overview

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Team Dionysus Critical Design Review

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  1. Team DionysusCritical Design Review Alijah Smith, Chris Koncilja, Elise Kowalski, Josh Tiras, Mike Beach, Becca Seigel 10/06/09

  2. Organization Chart

  3. Mission Overview • Mission Overview • Objective: Use infrared sensor and an ultraviolet sensor to determine the flux of infrared and ultraviolet light throughout the troposphere and lower stratosphere • We expect to prove that UV and IR light intensity increase with altitude • Hypothesis: UV and IR light intensity increase with altitude • Understanding penetration of light can help protect people from radiation from the sun. Large amounts of radiation can damage people’s skin and have other negative effects on other life on earth.

  4. Requirements Flow Down

  5. Design • Use sensors attached to top of cube and convert the data received from amps to volts. • Parts • Ultraviolet Sensor – ordered • Infrared Sensor – ordered • Expected to arrive Oct. 6th, 2009

  6. Budget

  7. Mass Bugdet

  8. Schedule • October • 4th – Team Meeting: start construction if possible, Finish DD Rev A/B, CDR slides • 5th – Team meeting: Finish CDR slides, practice presentation • 6th – DD rev A/B due, CDR slides due • 8th – Present CDR • 11th – Team meeting: Construction • 12th – Team meeting: Construction, empty shell/ mass simulator tests, start DD Rev C • 13th – Team meeting: Construction, sensor tests, DD Rev C • 18th – Team meeting: Construction, payload tests • 19th – Team meeting: finish DD Rev C, start LRR slides • 20th – Team meeting: construction, sensor and structure tests, LRR slides • 25th – Team meeting: All Testing Complete • 26th – Team meeting: Final touches, Rev C and/or LRR slides • 27th – Pre Launch Inspection • 29th – Mission Simulation • November • 1st – Team meeting: LRR slides, start team video • 2nd – Team meeting: finish LRR slides, practice • 3rd – DD Rev C due, LRR Slides due, present • 6th – BalloonSat weigh-in by 2:00 pm • 7th – LAUNCH!!! • 9th – Team meeting: Work on data and/or team video • 10th – Team meeting: Data, start final presentation/report • 12th – bring raw flight data to class • 15th – Team meeting: data, team video, start DD rev D • 16th – Team meeting: final report/ presentation, DD rev D • 17th – Team meeting: final report/presentation, DD rev D • 22nd-28th – individual work on report and video, if needed, and DD Rev D • 30th – Team meeting: finish final report/presentation, practice • December • 1st – Data Due Final Team Presentations and Report due, all data due, present, • Team meeting: finish DD rev D • 5th – Design Expo, DD rev D due, team video due

  9. Test Plan • Payload Testing: Whip, Drop, Cold, Stair Tests • Sensor Testing: AVR test, Calibration, Blacklight, Heat lamp • Schedule • 11th – Team meeting: Construction • 12th – Team meeting: Construction, empty shell/mass sim. test • 13th – Team meeting: Construction, sensor tests • 18th – Team meeting: Construction, payload tests • 20th – Team meeting: construction, sensors and structure tests • 25th – Team meeting: All Testing Complete • 27th – Pre Launch Inspection • 29th – Mission Simulation

  10. Expected Results • We expect to see an increase in radiation as altitude increases. • UV: 0 - 0.6 Watts per m^2 per nanometer • IR Ground: 0.5-1 Watts per m^2 per nanometer • IR at altitude: 1-1.5 Watts per m^2 per nanometer

  11. Biggest Worries • Sensor Accuracy/Error • Severity of Impact • Parachute Failing • Finding proper resistor for amps to volts conversion

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