Gravitational Force on satellite orbits

Now, to summarize: In summary, a satellite is orbiting Earth at a distance of 4.0 x 10^{7} m and the force of gravity between them is 228 N. Using the equation Fg = (Gm1m2)/(r^{2}), the mass of the satellite can be calculated.
  • #1
temaire
279
0

Homework Statement


A satellite orbits Earth 4.0 x 10[tex]^{7}[/tex] m away. The force of gravity between the satellite and Earth is 228 N. What is the mass of the satellite?


Homework Equations


Fg = (Gm1m2)/(r[tex]^{2}[/tex])


The Attempt at a Solution


http://img218.imageshack.us/img218/7876/satellitemk0.jpg​
[/URL]

Is my answer right?
 
Last edited by a moderator:
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  • #2
temaire said:

Homework Statement


A satellite orbits Earth 4.0 x 10[tex]^{7}[/tex] m away. The force of gravity between the satellite and Earth is 228 N. What is the mass of the satellite?

Homework Equations


Fg = (Gm1m2)/(r[tex]^{2}[/tex])

The Attempt at a Solution


http://img218.imageshack.us/img218/7876/satellitemk0.jpg​
[/URL]

Is my answer right?

Looks good.
 
Last edited by a moderator:
  • #3


Your attempt at a solution is on the right track, but there are a few errors in your calculation. First, the value for the gravitational constant G is 6.67 x 10^-11 Nm^2/kg^2, not 6.67 x 10^-11 Nm/kg^2. Also, the radius r should be squared in the denominator, as shown in the equation. So the correct calculation would be:

m = (Fg * r^2)/(G * M)

Where m is the mass of the satellite, Fg is the force of gravity, r is the distance between the satellite and Earth, G is the gravitational constant, and M is the mass of Earth.

Plugging in the given values, we get:

m = (228 N * (4.0 x 10^7 m)^2)/(6.67 x 10^-11 Nm^2/kg^2 * 5.97 x 10^24 kg)

m = 1.9 x 10^3 kg

So the mass of the satellite is approximately 1,900 kg. However, it's always important to double check your units and make sure they are consistent. In this case, the units for the gravitational constant cancel out, leaving only kg as the unit for mass. So the final answer should be just 1.9 x 10^3, without any units attached.

Overall, your approach and understanding of the concept is correct, but be sure to double check your calculations and units to ensure accuracy.
 

What is the gravitational force on a satellite?

The gravitational force on a satellite is the force of attraction between the satellite and the object it is orbiting, which is typically a planet or a star. This force is responsible for keeping the satellite in orbit.

How does the mass of a satellite affect its orbit?

The mass of a satellite does not affect its orbit. The gravitational force is dependent on the mass of the object it is orbiting, not the mass of the satellite itself. Therefore, a satellite with a larger mass will experience the same gravitational force as a satellite with a smaller mass, as long as they are orbiting the same object.

What is the relationship between the distance of a satellite from the object it is orbiting and the gravitational force?

The gravitational force on a satellite is inversely proportional to the square of the distance between the satellite and the object it is orbiting. This means that as the distance increases, the gravitational force decreases.

How does the shape of a satellite's orbit affect the gravitational force?

The shape of a satellite's orbit does not affect the gravitational force. The gravitational force is dependent on the mass of the object being orbited and the distance between the two objects, not the shape of the orbit. However, the shape of the orbit does affect the speed of the satellite and the time it takes to complete one orbit.

Can the gravitational force on a satellite be altered?

The gravitational force on a satellite cannot be altered unless there is a change in the mass of the object being orbited or the distance between the satellite and the object. However, the speed and direction of the satellite can be altered by external forces such as thrusters or gravitational pulls from other objects.

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