A hyperbolic earth departure trajectory has a perigee altitude of 350 km and a perigee speed of 11.5 km/s. Calculate a. the hyperbolic excess speed b. the radius when the true anomaly is 110° c. vr and v⊥ when the true anomaly is 110° d. the turn angle of the hyperbolic trajectory
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A hyperbolic earth departure trajectory has a perigee altitude of 350 km and a perigee speed of 11.5...
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