7. At the point where the forces balance 2212//esGM m rGM m r=, where Meis the mass of Earth,Msis the mass of the Sun, mis the mass of the space probe, r1is the distance from the center of Earth to the probe, and r2is the distance from the center of the Sun to the probe. We substitute r2= d−r1, where dis the distance from the center of Earth to the
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This note was uploaded on 05/17/2011 for the course PHY 2049 taught by Professor Any during the Spring '08 term at University of Florida.