Consider a spacecraft moving in the orbit calculated in Example 8.1. At the point on the orbit given by the true anomaly 8A = 90°, a single impulse is applied to the spacecraft that transfers the spacecraft to a new orbit in the same plane with an eccentricity of0.8 and a of 10,000 km. Calculate the value 11Vofthis impulse. Example 8.1 At the end of a rocket launch of a space vehicle, the burnout velocity is 9 km/s in a direction due north and 3 ° above the local horizontal. The altitude above sea level is 500 mi. The burnout point is located at the 27th parallel (27°) above the equator. Calculate and plot the trajectory of the space vehicle.
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