Please , just the part C A satellite of mass 220 kg is placed into Earth orbit at a height of 350 km above the surface.(a) Assuming a circular orbit, how long does the satellite take to complete one orbit?1.52(b) What is the satellite's speed?7.703e3V m/s(c) Starting from the satellite on the Earth's surface at the equator, what is the minimum energy input necessary to place this satellite in orbit? Ignore air resistance but includethe effect of the planet's daily rotation.

Given that Mass of satellite (m)= 220 kg Height of satellite (h)= 350 km Mass of earth(Me)= 5.97×…

(c) Starting from the satellite on the Earth's surface at the equator, what is the minimum energy input necessary to place this satellite in orbit? Ignore air resistance but include the effect of the planet's daily rotation.

(c) Starting from the satellite on the Earth's surface at the equator, what is the minimum energy input necessary to place this satellite in orbit? Ignore air resistance but include the effect of the planet's daily rotation.

Classical Dynamics of Particles and Systems

5th Edition

ISBN:9780534408961

Author:Stephen T. Thornton, Jerry B. Marion

Publisher:Stephen T. Thornton, Jerry B. Marion

Chapter8: Central-force Motion

Section: Chapter Questions

Problem 8.42P

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Concept explainers

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The theory of special relativity explains the connection between space and time to objects that move in a straight line at a constant speed. The objects move at the speed of light. When an object approaches light speed, its mass is endless and cannot move faster than light. The most crucial postulate of Einstein's special relativity is that the laws of nature do not change in each frame of reference.

Question

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Please , just the part C

A satellite of mass 220 kg is placed into Earth orbit at a height of 350 km above the surface.
(a) Assuming a circular orbit, how long does the satellite take to complete one orbit?
1.52
(b) What is the satellite's speed?
7.703e3
V m/s
(c) Starting from the satellite on the Earth's surface at the equator, what is the minimum energy input necessary to place this satellite in orbit? Ignore air resistance but include
the effect of the planet's daily rotation.

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