Cubesat by MANISH DHIMAN
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The document discusses CubeSat satellites. It describes their size comparison to other satellites, typical weight, internal structure using aluminum, use of solar cells and lithium-ion batteries for power, and methods of launch including from the International Space Station. CubeSats offer advantages of low cost, small size, less development time, and lower launch costs compared to larger satellites.
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- 1. MANISH DHIMAN BCA FINAL YEAR CUBESAT SATELLITE
- 2. 1. SPUTNIK 1 2. INTERNATIONAL SPACE STATION 3. INTRODUCTION 4. SIZE COMPERISION OF CUBEST 5. WEIGHT OF A CUBESAT 6. INSIDE CUBESAT SATELLITE 7. STRUCTURE 8. POWER 9.LAUNCH & WORKING 11.ADVANTAGES 12. RIFATH SHAROOK
- 6. CUBE SAT
- 7.
- 8. WEIGHT OF CUBE SAT
- 10. STRUCTURE • Most commonly material used in cube-sat structure is aluminum.
- 11. POWER • CubeSats use solar cells to convert solar light to electricity that is then stored in rechargeable Lithium-ion batteries that provide power during eclipse as well as during peak load times. • Lithium-ion batteries feature high energy-to-mass ratio. • Higher power requirements can make use of attitude control to ensure the solar panels remain in their most effective orientation toward the Sun
- 12. LAUNCH • Unlike full-sized spacecraft, CubeSats have the ability to be delivered into space as cargo and then deployed by the International Space Station. This presents an alternative method of achieving orbit apart from launch and deployment by a launch vehicle. • PSLV-C37 Successfully Launches 104 Satellites in a Single Flight. In this launch 103 satellite are nano satellite in which two of them are Indian satellite .
- 14. Synchronization
- 15. Low cost Small size Less development time Less launch cost ADVANTAGE