Calculate the total Av required to transfer between two coplanar circular Earth orbits of radii r 1 = 12,750 km and r2 = 31,890 km, respectively, using a transfer ellipse having parameters p = 13,457 km and e = Ans.: 7.086 km/s = 0.76.

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Calculate the total Av required to transfer between two coplanar circular Earth orbits
of radii r 1
parameters p = 13,457 km and e = 0.76.
Ans.: 7.086 km/s
12,750 km and r2 = 31,890 km, respectively, using a transfer ellipse having
Transcribed Image Text:Calculate the total Av required to transfer between two coplanar circular Earth orbits of radii r 1 parameters p = 13,457 km and e = 0.76. Ans.: 7.086 km/s 12,750 km and r2 = 31,890 km, respectively, using a transfer ellipse having
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