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Suppose you want to move a spacecraft from a circular orbit at 500 km altitude to a circular orbit at 150 km altitude to ensure
Suppose you want to move a spacecraft from a circular orbit at 500 km altitude to a circular orbit at 150 km altitude to ensure that its orbit will naturally decay over a few years. What velocity change (V1) is needed to go from the initial circular orbit into the transfer orbit? What velocity change (V2) is needed to go from the transfer orbit to the final circular orbit? What is the time (TOF) required for the transfer
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