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Get Full Access to Physics For Scientists And Engineers: A Strategic Approach With Modern Physics - 3 Edition - Chapter 8 - Problem 29p
Get Full Access to Physics For Scientists And Engineers: A Strategic Approach With Modern Physics - 3 Edition - Chapter 8 - Problem 29p

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# Communications satellites are placed in circular orbits

ISBN: 9780321740908 69

## Solution for problem 29P Chapter 8

Physics for Scientists and Engineers: A Strategic Approach with Modern Physics | 3rd Edition

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Problem 29P

Communications satellites are placed in circular orbits where they stay directly over a fixed point on the equator as the earth rotates. These are called geosynchronous orbits. The altitude of a geosynchronous orbit is $$3.58 \times 10^{7} \mathrm{~m}$$ ( $$\approx 22,000$$ miles).

a. What is the period of a satellite in a geosynchronous orbit?

b. Find the value of $$g$$ at this altitude.

c. What is the weight of a $$2000 \mathrm{~kg}$$ satellite in a geosynchronous orbit?

Step-by-Step Solution:

Step 1 of 3

Part a

A geosynchronous satellite takes 24 hours to orbit once around the Earth. This is the same as the Earth takes to complete one rotation about its axis.

Step 2 of 3

Step 3 of 3

##### ISBN: 9780321740908

Physics for Scientists and Engineers: A Strategic Approach with Modern Physics was written by and is associated to the ISBN: 9780321740908. This textbook survival guide was created for the textbook: Physics for Scientists and Engineers: A Strategic Approach with Modern Physics, edition: 3. This full solution covers the following key subjects: geosynchronous, orbit, satellite, altitude, orbits. This expansive textbook survival guide covers 17 chapters, and 1439 solutions. The full step-by-step solution to problem: 29P from chapter: 8 was answered by , our top Physics solution expert on 08/30/17, 04:34AM. Since the solution to 29P from 8 chapter was answered, more than 10599 students have viewed the full step-by-step answer. The answer to “?Communications satellites are placed in circular orbits where they stay directly over a fixed point on the equator as the earth rotates. These are called geosynchronous orbits. The altitude of a geosynchronous orbit is $$3.58 \times 10^{7} \mathrm{~m}$$ ( $$\approx 22,000$$ miles).a. What is the period of a satellite in a geosynchronous orbit?b. Find the value of $$g$$ at this altitude.c. What is the weight of a $$2000 \mathrm{~kg}$$ satellite in a geosynchronous orbit?” is broken down into a number of easy to follow steps, and 74 words.

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