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Question #75080
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Question
What is the change in total energy required to transfer the satellite from 2RE to 4RE orbit?
A. ∆E = -GME m / (8RE)
B. ∆E = GME m / (8RE)
C. ∆E = GME m / (4RE)
D. ∆E = -GME m / (4RE)
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