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1. At the end of a rocket launch of a space vehicle from earth, the burnout velocity is 13 km/s in a direction due south and 10° above the local horizontal. The burnout point is directly over the equator at an altitude of 400 mi above sea level. Calculate the trajectory of the space vehicle. 2. Calculate and compare the escape velocities from Venus, Earth, Mars, and Jupiter, given the following information:
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