Structures and Thermal Locomotion Phase

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Structures and Thermal Locomotion Phase Caitlyn McKay Structures and Thermal Locomotion Phase 1

Using a Crushable Material Honeycomb Length needed Mass needed Core for 10.05-g Landing 1/4-5056-.002p 1.48 m 321 kg 3/8-5056-.0007p 2.00 m 100 kg 1/4-5056-.0007p 0.904 m 74.0 kg 2 Caitlyn McKay Structures and Thermal

Structures and Thermal Updated Rover Component Mass in Kg Solar Panels 2.5 Drive System 0.3 Battery Cooling System 7.0 Space Blanket 1.6 Structure 1.7 Communications 2.3 Power (Extra) 1.9 Wheels Total Mass = 17.4 kg 3 Caitlyn McKay Structures and Thermal

Global Buckling Cylinder 4 Caitlyn McKay Structures and Thermal

Structures and Thermal 5 Caitlyn McKay Structures and Thermal

Structures and Thermal Impulse Momentum 6 Caitlyn McKay Structures and Thermal

Structures and Thermal 7 Caitlyn McKay Structures and Thermal

Load on Curve Beam (wheel spoke) 8 Caitlyn McKay Structures and Thermal

Structures and Thermal 9 Caitlyn McKay Structures and Thermal

Buckling of Aluminum Body Buckling Stress: 712 kg/m^2 10 Caitlyn McKay Structures and Thermal

Shear Stress on Motor Shaft 11 Caitlyn McKay Structures and Thermal

Structures and Thermal References: 2008. CES EduPack2008. Citrix Client. Purdue University, West Lafayette, IN. Grandt, Alten F. Fundamentals of Structural Integrity. 28-45. Hoboken, NJ: John Wiley & Sons, Inc., 2004. Gere, James M. Mechanics of Materials. 6th ed. Belmont: Brooks/Cole, 2003. 12 Caitlyn McKay Structures and Thermal

Structures and Thermal GonzaÂ´lez, Carlos, and Javier LLorca. "Stiffness of a curved beam subjected to axial load." International Journal of Solids and Structures: 1537-1545. Elsevier. 13 Oct. 2004. Science Direct. 14 Feb. 2009 <www.elsevier.com/locate/ijsolstr>. Wijker, Jacob Job. Spacecraft Structures. New York: Springer, 2008. Purdue University, West Lafayette, IN. 16 Feb. 2009 <http://http://www.springerlink.com/content/k4hv69/>. 13 Caitlyn McKay Structures and Thermal