Problem 3: During assembly of a space facility near the Earth, a partially finished structure (m < < Me) has a shape that resembles a *V* consisting of thin rods (L < < R) with the open side facing away from the Earth. Note that (L Let = 65. Now compare the principal directions & with the orbit-fixed directions a Where are they each in the sketch? Compute the approximate gravity moment about B if R = 6503 km. The moment will cause the structure to rotate in which direction? Is this direction consistent with your discussion of "stability" in (c)? Why or why not?