A satellite of mass m is in a circular orbit around the Earth (mass M) at a distance R from the center of the earth. (a) What is the speed of the satellite? (b) From your answer in part (a), how long does it take to complete one orbit? This is a special case of Kepler's third law. (Hint: the speed is equal to the distance (circumference of the circular orbit) divided by the time to complete one orbit) (c) From your answer in part (a), what is the KE of the satellite?
A satellite of mass m is in a circular orbit around the Earth (mass M) at a distance R from the center of the earth. (a) What is the speed of the satellite? (b) From your answer in part (a), how long does it take to complete one orbit? This is a special case of Kepler's third law. (Hint: the speed is equal to the distance (circumference of the circular orbit) divided by the time to complete one orbit) (c) From your answer in part (a), what is the KE of the satellite?
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3 answer parts a-c
![Question 3.
A satellite of mass m is in a circular orbit around the Earth (mass M) at a distance R from the center of
the earth.
(a) What is the speed of the satellite?
(b) From your answer in part (a), how long does it take to complete one orbit? This is a special case
of Kepler's third law. (Hint: the speed is equal to the distance (circumference of the circular orbit)
divided by the time to complete one orbit)
(c) From your answer in part (a), what is the KE of the satellite?
(d) What is the total mechanical energy of the satellite?
(e) How much work would be required to put the satellite into an orbit of radius 2R?](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F2bbbe76c-8abf-4b35-a964-ca5975ae64aa%2F222dfbc4-8273-489f-97cb-037dcfd74553%2Ffwbehpj_processed.jpeg&w=3840&q=75)
Transcribed Image Text:Question 3.
A satellite of mass m is in a circular orbit around the Earth (mass M) at a distance R from the center of
the earth.
(a) What is the speed of the satellite?
(b) From your answer in part (a), how long does it take to complete one orbit? This is a special case
of Kepler's third law. (Hint: the speed is equal to the distance (circumference of the circular orbit)
divided by the time to complete one orbit)
(c) From your answer in part (a), what is the KE of the satellite?
(d) What is the total mechanical energy of the satellite?
(e) How much work would be required to put the satellite into an orbit of radius 2R?
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