The zero-velocity value of the Jacobi integral at the L2 point of the Earth-Moon system is C= -1.59411. Suppose a spacecraft is newar Earth (r2=1/60 in our descriptions). Approximately waht speed must the craft have realtive to the rotating system if it is able to reach the L2 point? In considering the problem, you may ignore all terms in the expression for the Jacobi integral that are "small", which for the purposes of this problem we will take to mean that they are of the order of u (mew) or smaller. (Note that you must explain why they are small)

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