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This document outlines the conceptual design review team’s mission to stabilize a satellite for capturing clear images of stars during daylight. Key objectives include minimizing satellite rotation, thereby preventing damage and enabling successful photographic duties. The design incorporates a foam core structure, various cameras (CCD and HP digital), temperature monitoring systems, and motorized controls for stabilization. The proposals aim to enhance near-space exploration through innovative technology and strategic planning.
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Team Perfect 10 Conceptual Design Review Amanda Childress, Duane Goodfellow, Paul Judiscak, Tiana Miller-Jackson, Melissa Savage, Dan Wawrzyniak September 20, 2007
Overview • Mission Statement: To stabilize the satellite from rotating in order to capture clear pictures of stars during daylight, to avoid damage to the satellite during flight and to positively influence further near space exploration.
Overview • Plan to photograph stars during daylight hours • Plan to take clear pictures with use of stabilization of satellite on Y axis • Plan to reduce damage to the satellite through stabilization
Design • Parts: • Structure: Foam Core • HOBO Datalogger with Internal and External Temperature Probes • CCD Camera • HP Digital Camera • Timing Circuit to control cameras • ADAS • 2 Motors to control rotation • Heater
Design Heater Power Timer Power HP Camera Power HP Camera Timer Switch Switch CCD Camera CCD Camera Power Heater ADAS Power HOBO Motor 2 ADAS Internal Temp External Temp Motor 1