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need help {Slat} A spacecraft in orbit around the Earth is at apoapsis in an elliptical orbit with semjmajor axis a = 15000km and eccentricity
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{Slat} A spacecraft in orbit around the Earth is at apoapsis in an elliptical orbit with semjmajor axis a = 15000km and eccentricity e = 0.4. Find the t? required (and direction) for a single burn to circularize the orbit at apoapsisStep by Step Solution
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