A Systems Design for a Prototype Space Colony

Recall, 7.F6 !2 D a 2 7° [8 190xl0 8 F 2 - 4.870xl0 7 GP+ 2.56xlo 6 G 2 ]dy 11 0 . G 4 y F 12y 2 - 12ay + 2a 2 F 2 [12y 2 - 12ay + 2a 2 ] 2 144y 4 288ay 3 + 192a 2 y 2 [y4 - 2ay3 + a2y2]2 Substituting the above results into the plate strain energy equation, obtain: Uplate ½ D a 11 2 ;o[l.179xl0 11 y 4 2.359xlo 11 ay 3 + l.573xlo 11 a 2 y 2 3.93lxlo 10 a 3 y

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