1 / 12

Team Flight Club Conceptual Design Review

Fall 2008 Rev A 09-23-08. Evan Akselrad, Chris Anaya, Natalie Bixler, Melanie Dubin, Logan Finch, Ted Maritz, and Scott Williams September 23, 2008. Team Flight Club Conceptual Design Review. Mission Overview.

wilda
Télécharger la présentation

Team Flight Club Conceptual Design Review

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript

  1. Fall 2008 Rev A 09-23-08 Evan Akselrad, Chris Anaya, Natalie Bixler, Melanie Dubin, Logan Finch, Ted Maritz, and Scott Williams September 23, 2008 Team Flight ClubConceptual Design Review

  2. Mission Overview • The Balloon Sat Flight Club shall ascend to an altitude of 30 kilometers in order to: • Image the curvature of the earth and the celestial sky in the daylight • Measure the light intensity as a function of altitudes.

  3. Mission Purpose • The team shall image the curvature of the earth and the celestial sky in order to demonstrate the capacities of high altitude imaging. • The team shall measure light intensity as a function of altitude to determine whether there is a discontinuity at the flight level of commercial aircraft. troposphere and the surface of the earth. • Search for a correlation between commercial aviation and global warming, which is known to be caused by increased light intensity.

  4. Design: Hardware • Foam Core- lightweight outer layer • Thermal Sheets- gold colored foil to assist in overcoming the subzero temperatures • Hobo Data Logger- 4 channel data collection and processing system to perform the science mission during the flight. • External/Internal Temperature Probe-To take internal and external temperature readings during flight • Cannon Digital Camera- Will be used to image the curvature of the earth • Heating System- To keep the payload above 0 degrees Celsius • Timing Circuit- Circuit that commands camera to take pictures • Batteries- Powers satellite • Solar Panel- The solar panel is a sheet of solar cells that attaches to the outside of the satellite in order to measure the voltage created by the varying intensities of light as a function of altitude. The voltage data can be interpreted as a measure of light intensity.

  5. Design: Illustration Light Intensity Experiment (solar panel) Heater External Temperature Sensor HOBO Data Recorder Digital Camera Attachment Tube

  6. Power Systems Switch 1 Hobo Data Logger 4 Channel Switch 2 Heating System Timing Circuit Digital Camera Internal Temperature Probe Light Intensity Sensor External Temperature Probe Design: Functional Block Diagram

  7. Project Manager Natalie Bixler C&DH Structures Thermal ADCS C&DH Power Electrical Science Scott Williams Logan Finch Ted Maritz Evan Akselrad Chris Anaya Melanie Dubin Natalie Bixler Management

  8. Schedule

  9. Budget: Weight

  10. Budget: Money

  11. Biggest Worries • Biggest Worries… • Hobo Data Logger will not take complex enough data for light intensity science experiment. • Solar Panels will malfunction, become detached, or break • Digital Camera will not work at altitude

  12. Questions…?

More Related