What is the gravitational force on the satellite?

Click For Summary
SUMMARY

The gravitational force on a satellite in a circular orbit can be calculated using the formula F_g = (G*m*m_e)/(r_e+h)^2, where G is the gravitational constant, m is the satellite's mass, m_e is the Earth's mass, and r_e+h is the distance from the Earth's center to the satellite. To determine the fraction of this gravitational force relative to the satellite's weight at the Earth's surface, the equation Fraction = F_g / W can be used, leading to Fraction = (G*m_e)/(r_e+h)^2 / g, where g is the acceleration due to gravity. This analysis utilizes Newton's Law of Universal Gravitation to establish the relationship between gravitational force and weight.

PREREQUISITES
  • Understanding of Newton's Law of Universal Gravitation
  • Knowledge of gravitational constant (G)
  • Familiarity with the concepts of mass (m, m_e) and radius of Earth (r_e)
  • Basic grasp of gravitational acceleration (g)
NEXT STEPS
  • Study the implications of gravitational force variations with altitude
  • Learn about orbital mechanics and satellite dynamics
  • Explore the concept of weightlessness in orbit
  • Investigate the effects of gravitational forces on different celestial bodies
USEFUL FOR

Students in physics, aerospace engineers, and anyone interested in satellite technology and gravitational physics will benefit from this discussion.

lollypop
Messages
33
Reaction score
0
hello everybody:

A satellite of mass m used in a cellular telephone network is in a circular orbit at a height of h above the surface of the earth.

What is the gravitational force on the satellite? Take the gravitational constant to be G , the mass of the Earth to be m_e , and the radius of the Earth to be r_e.
for this question i get the following:
F_g= (G*m*m_e)/(r_e+h)^2

now, for this question
What fraction is this of its weight at the surface of the earth? Take the free fall acceleration to be g.
i'm going to use just the mass of the Earth not the one from the satellite right? but what does it mean "what fraction"?? what formula do i use?
 
Physics news on Phys.org
They want you to find the ratio of the force of gravity acting on the satellite in orbit to the force of gravity acting on the satellite on the surface of the Earth, i.e.

[tex]\frac{F_g(r_e + h)}{F_g(r_e)}[/tex]

cookiemonster
 



Hello there,

To answer your first question, the gravitational force on the satellite can be calculated using Newton's Law of Universal Gravitation, which states that the force between two objects is directly proportional to the product of their masses and inversely proportional to the square of the distance between them. In this case, the satellite is in orbit around the Earth, so the equation would be:

F_g = (G*m*m_e)/(r_e+h)^2

Where G is the gravitational constant, m is the mass of the satellite, m_e is the mass of the Earth, and r_e+h is the distance between the satellite and the center of the Earth.

Now, for your second question, "what fraction" is referring to the ratio of the gravitational force on the satellite to its weight at the surface of the Earth. The weight of an object is the force of gravity acting on it, and it is given by the equation:

W = m*g

Where m is the mass of the object and g is the acceleration due to gravity. So to find the fraction, we can divide the gravitational force on the satellite by its weight at the surface of the Earth:

Fraction = F_g / W

= (G*m*m_e)/(r_e+h)^2 / (m*g)

= (G*m_e)/(r_e+h)^2 / g

Hope this helps clarify things for you. Let me know if you have any other questions.
 

Similar threads

  • · Replies 7 ·
Replies
7
Views
3K
Replies
5
Views
3K
  • · Replies 16 ·
Replies
16
Views
3K
Replies
1
Views
2K
  • · Replies 28 ·
Replies
28
Views
2K
Replies
5
Views
3K
  • · Replies 8 ·
Replies
8
Views
2K
  • · Replies 14 ·
Replies
14
Views
2K
  • · Replies 4 ·
Replies
4
Views
3K
Replies
37
Views
4K