Problem 1: Consider a spacecraft in an elliptical orbit. In its perigee at 2,000 km altitude above sea level, it has a speed of 9 km/s. If its speed at apogee is reduced to 6 km/s, what is the corresponding altitude above sea level? Note: altitude above sea level ‡ orbital radius! Problem 2: What is the orbital period of the spacecraft in the aforementioned orbit?

College Physics
11th Edition
ISBN:9781305952300
Author:Raymond A. Serway, Chris Vuille
Publisher:Raymond A. Serway, Chris Vuille
Chapter1: Units, Trigonometry. And Vectors
Section: Chapter Questions
Problem 1CQ: Estimate the order of magnitude of the length, in meters, of each of the following; (a) a mouse, (b)...
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Problem 1:
Consider a spacecraft in an elliptical
orbit. In its perigee at 2,000 km altitude above sea level, it
has a speed of 9 km/s. If its speed at apogee is reduced to 6
km/s, what is the corresponding altitude above sea level?
Note: altitude above sea level ‡ orbital radius!
Problem 2:
What is the orbital period of the
spacecraft in the aforementioned orbit?
Transcribed Image Text:Problem 1: Consider a spacecraft in an elliptical orbit. In its perigee at 2,000 km altitude above sea level, it has a speed of 9 km/s. If its speed at apogee is reduced to 6 km/s, what is the corresponding altitude above sea level? Note: altitude above sea level ‡ orbital radius! Problem 2: What is the orbital period of the spacecraft in the aforementioned orbit?
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