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A space vehicle in a circular orbit at an altitude of 310 km above the earth...

A space vehicle in a circular orbit at an altitude of 310 km above the earth executes a Hohmann transfer to a 1050 km altitude circular orbit. Calculate the total delta-v requirement.

a. dv = 423.391 m/sec

b. dv =394.3629 m/sec

c. dv = 396.3939 m/sec

d. dv = 391.39039 m/sec

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