A hyperbolic earth departure trajectory has a perigee


A hyperbolic earth departure trajectory has a perigee altitude of 250 km and a perigee speed of 11 km/s.

(a) Calculate the hyperbolic excess speed (kilometers per second).

(b) Find the radius (kilometers) when the true anomaly is 1000.

(c) Find vr and vt (kilometers per second) when the true anomaly is 1000.

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Physics: A hyperbolic earth departure trajectory has a perigee
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