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0.5U ADCS Cubesat

MY DELIVERABLE (School Project)
- Use SolidWorks to design and manufacture a 0.5U ADCS Cubesat chasis
- This Involves creating fittings, and fastening methods for the reaction wheel motors.

CONSTRANTS
- Use formfactor baseplate dimensions provided by NASA AMES
- Fit motors and electronics in a 10x10x5cm volume
- 3D printed chasis due to funding

END GOAL
- Integrate our 0.5U ADCS into a NASA AMES 12U TechEdSat to be used as the ADCS system

FASTENING METHOD
- Implement heated threaded inserts into PLA Plastic
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Radio Controlled Quadcopter Drone

MY DELIVERABLE (Personal Project)
- Use SolidWorks to design a chassis, arms, legs, and landing gear
- Use a 3D printer to print the chassis, arm, legs, and landing gear
- Integrate power supply, motors, ESCs (electronic speed controllers), flight computer, GPS, and RF transmitter.
- Soldered power supply, voltage regulator, and ESCs (electronic speed controllers) to the power distribution board.

CONSTRANTS
- Limited to a 25cm x 25cm printing bed

END GOAL
- Design, build, and integrate a radio controlled quadcopter drone.

SPECS:
-11.1v, 2200mAh Lipo Battery
-915 MHz Radio Telemetry 
-DC 7-12V, 920 KV Volts Brushless Motor (Motor will spin 920 rpms for every volt applied to it.) [ Max RPM = 11,040] (x4)
-Electronic speed controller: Input voltage 2-4v, BEC 5v 3A ( Battery Eliminator Circuit) : steps Down Voltage from battery (x4)
-Power Module/Voltage regulator: Input voltage 6-30v, Output voltage 5.3v ± 0.1v, Maximum output current 3A
-Pixhawk Px4 Flight Controller
- 3.1 lbs or 1.4 kg
​-Software: Mission Planner by ArduPilot

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