STICE ANOTHER A telescope satelite is launched into circular orbit around the Earth, at an altitude A. The sateinite's mass is m, and it was launched from Earth's surface. (Use the following as necessary for the rad of the Earth, M, for the mass of the Earth, G for the gravitational constant, m, and ) (a) How long does the satelite take to complete one circular orbit? T- (b) What is the satellite's speed? G-M The gravitational force suppled the needed centripetal acceleration, so equate the expression for Newter's law of universal grevitation to the centripetal force, and solve for (c) What is the minimum energy input necessary to place this satelite in orbit? Ignore air resistance but include the effect of the planet's daily rotation (Use the following as necessary R. My, m h, and T for the period of Earth's rotation) Ar . min Need Help? Road
STICE ANOTHER A telescope satelite is launched into circular orbit around the Earth, at an altitude A. The sateinite's mass is m, and it was launched from Earth's surface. (Use the following as necessary for the rad of the Earth, M, for the mass of the Earth, G for the gravitational constant, m, and ) (a) How long does the satelite take to complete one circular orbit? T- (b) What is the satellite's speed? G-M The gravitational force suppled the needed centripetal acceleration, so equate the expression for Newter's law of universal grevitation to the centripetal force, and solve for (c) What is the minimum energy input necessary to place this satelite in orbit? Ignore air resistance but include the effect of the planet's daily rotation (Use the following as necessary R. My, m h, and T for the period of Earth's rotation) Ar . min Need Help? Road
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Transcribed Image Text:CTICE ANOTHER
A telescope satelite is launched into circular artit around the Earth, at an altitude . The satelite's mass is m, and it was launched from Earth's surface. (Use the following as necessary for the rad
of the Earth, M, for the mass of the Earth, G for the gravitational constant, m, and f.)
(a) How long does the satelite take to complete one circular orbit?
T=
(b) What is the satellite's speed?
GM
The gravitational force suppled the needed centripetal acceleration, so equate the expression for Newter's law of universal gravitation to the centripetar force, and solve for
(c) What is the minimum energy input necessary to place this satelite in orbit? Ignore air resistance but include the effect of the planet's daily rotation. (Use the following as necessary A. M, G, m
h, and T for the period of Earth's rotation)
Ar .
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