Geosynchronous Satellite Concepts
Interactive Video
•
Physics, Mathematics, Science
•
9th - 12th Grade
•
Practice Problem
•
Hard
Patricia Brown
FREE Resource
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10 questions
Show all answers
1.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What force provides the centripetal force necessary for a satellite to maintain its circular orbit?
Electromagnetic force
Gravitational force
Magnetic force
Nuclear force
2.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
Which of the following is used to calculate the gravitational force between the Earth and a satellite?
Mass of the satellite only
Distance between the satellite and the Earth's surface
Universal gravitational constant, mass of the Earth, and mass of the satellite
Speed of the satellite
3.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the formula for the speed of a satellite in a circular orbit?
V = G * M * R
V = sqrt(G * M / R)
V = G * M / R
V = sqrt(G / M * R)
4.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
How is the period of a satellite's orbit calculated?
By multiplying the speed of the satellite by the radius of the orbit
By subtracting the speed of the satellite from the gravitational constant
By dividing the circumference of the orbit by the speed of the satellite
By adding the radius of the Earth to the height of the satellite
5.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the period of a geosynchronous satellite in seconds?
24,000 seconds
43,200 seconds
12,000 seconds
86,400 seconds
6.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the difference between rotation and revolution in the context of satellites?
Rotation is about an external axis, revolution is about an internal axis
Rotation is about an internal axis, revolution is about an external axis
Rotation and revolution are unrelated to satellite motion
Both rotation and revolution are about the same axis
7.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
How do you calculate the height of a geosynchronous satellite above the Earth's surface?
By dividing the orbital radius by the mass of the Earth
By multiplying the orbital radius by the gravitational constant
By adding the radius of the Earth to the orbital radius
By subtracting the radius of the Earth from the orbital radius
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