UYARI T EAM PRELIMINARY DESIGN R EPORT - PowerPoint PPT Presentation

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UYARI T EAM PRELIMINARY DESIGN R EPORT

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  1. UYARI TEAMPRELIMINARY DESIGN REPORT Cansat 2011 PDR (UYARI)

  2. Contents • Quick Overview • Technical Presentation • Missions • Budgets • Emissions Cansat 2011 PDR (UYARI)

  3. 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)

  4. 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)

  5. Mechanic • One servo to control parachute • One servo toseperate parachutesystem • Airbag • TerraformingEquipments • RFAntennaDeploying Mechanism Cansat 2011 PDR (UYARI)

  6. Electronic • Microcontroller • GPS Module • RF Module, Antenna • CameraModule(SeparateunitfromRF Module) • Humidity Sensor Cansat 2011 PDR (UYARI)

  7. 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)

  8. Costs Cansat 2011 PDR (UYARI)

  9. 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)