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UYARI T EAM PRELIMINARY DESIGN R EPORT. C ontents. Quick O ve r view Technical P resentation M ission s Budgets Emissions. Quick Overview. Open Class Diameter 80 mm Height 200mm Mass < 1Kg Volume < 1lt. Parachute. Missions: Atmospheric Sounding Deploying of RF Antenna
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UYARI TEAMPRELIMINARY DESIGN REPORT Cansat 2011 PDR (UYARI)
Contents • Quick Overview • Technical Presentation • Missions • Budgets • Emissions Cansat 2011 PDR (UYARI)
QuickOverview • OpenClass • Diameter80 mm • Height200mm • Mass< 1Kg • Volume < 1lt Parachute • Missions: • Atmospheric Sounding • Deploying of RF Antenna • Taking Photo • Airbag • Terraforming Mechanic Electronic Airbag Cansat 2011 PDR (UYARI)
LandingSystem • Wewilluseautonomous structure in our landing system • Our system aimed at stroke to ten-meter diameter of landing point will be controlled by the servo, using software • Theparachute system is designed to leave the satellitewhenthesatellite neared the ground • Parachute • Parachute’sarea is 48cm2 • Designed to freeparachute-typehas seven cells Cansat 2011 PDR (UYARI)
Mechanic • One servo to control parachute • One servo toseperate parachutesystem • Airbag • TerraformingEquipments • RFAntennaDeploying Mechanism Cansat 2011 PDR (UYARI)
Electronic • Microcontroller • GPS Module • RF Module, Antenna • CameraModule(SeparateunitfromRF Module) • Humidity Sensor Cansat 2011 PDR (UYARI)
Missions • Atmospheric Sounding • Degree of humidity • Altitude value • Deploying of a RF antenna after landing • Communicationwithgroundstation • Photo • Taking enough quality photo • Airbag • Airbags openwhen altitude is less than 4 meters • Terraforming • Drilling a hole andleaving a crop Cansat 2011 PDR: (UYARI)
Costs Cansat 2011 PDR (UYARI)
Emissions: RF Module is CC1110EMK433 Apparentradiatingpower (ARP) (dBW) calculation: APR = 10*log10(Pe) + Ge - 2.14Pe =1mW = 0.001 WGe= 1 (maximum) APR = 10*log (10*0.001) + 1 - 2.14 APR = - 20 + 1 - 2.14 APR = - 21.14 dbW 10mW = -2 dbW -21.14 dbW< -2dbW Cansat 2011 PDR (UYARI)