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Cansat 2011 Preliminary Design Report (UYARI) - Mission, Budgets, and Emissions

Explore the technical details, missions, and budget breakdown of the Cansat 2011 project in this comprehensive preliminary design report. Learn about its innovative features and landing system design. Discover the electronic components and missions it was designed to accomplish. Dive into the calculation of emissions and radiating power.

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Cansat 2011 Preliminary Design Report (UYARI) - Mission, Budgets, and Emissions

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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)

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