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Caitlyn McKay

Caitlyn McKay. Structures and Thermal Locomotion Phase. 1. Mass. Total Mass of Rover = 29.1259 kg Dimensions of Rover = .407 m x .497 m x .456 m. 2. Stress of Rover on Motor Shaft. 3. Stress of Rover on Shaft. 4. Stress of Rover on Shaft.

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Caitlyn McKay

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  1. Caitlyn McKay Structures and Thermal Locomotion Phase 1

  2. Mass Total Mass of Rover = 29.1259 kg Dimensions of Rover = .407 m x .497 m x .456 m 2 Caitlyn McKay Structures and Thermal

  3. Stress of Rover on Motor Shaft 3 Caitlyn McKay Structures and Thermal

  4. Stress of Rover on Shaft 4 Caitlyn McKay Structures and Thermal

  5. Stress of Rover on Shaft Maximum mass for the shaft of .01 m diameter while on the moon: 61.4 kg 5 Caitlyn McKay Structures and Thermal

  6. Diameter of Shaft Needed to Support Rover on Earth Assumption: gravitational force=9.80665 m/s^2 6 Caitlyn McKay Structures and Thermal

  7. Diameter of Shaft Needed to Support Rover during Launch Assumption: gravitational force = 9.80665 m/s^2 gravitational force = 7.5 7 Caitlyn McKay Structures and Thermal

  8. Diameter of Shaft Needed to Support Rover during Soft Landing Assumption: gravitational force = 9.80665 m/s^2 gravitational force = 10 8 Caitlyn McKay Structures and Thermal

  9. Diameter of Shaft Needed to Support Rover on Moon Assumption: gravitational force=9.80665/6 m/s^2 9 Caitlyn McKay Structures and Thermal

  10. Buckling of Aluminum Body Buckling Stress: 82,300 kg/m^2 10 Caitlyn McKay Structures and Thermal

  11. Energy Usage 11 Caitlyn McKay Structures and Thermal

  12. Operating Temperatures 12 Caitlyn McKay Structures and Thermal

  13. References: 13 Caitlyn McKay Structures and Thermal 2008. CES EduPack2008. Citrix Client. Purdue University, West Lafayette, IN. Grandt, Alten F. Fundamentals of Structural Integrity. Hoboken, NJ: John Wiley & Sons, Inc., 2004.

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