Speed of International Space Station

In summary, the speed of an object in orbit is determined by its orbital height and the mass of the body it is orbiting around. For a circular orbit, this can be calculated using the equation v ≈ √(GM/r). The ISS needs to run at a high speed of 7.7 km/s in order to maintain a stable orbit around the Earth, and reducing its speed would require it to be pushed further away from the Earth.
  • #1
Israr
2
1
Why ISS need to run on such high speed 7.7km/s ?
What will affect if it made to run on very slower speed.

thanks
 
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  • #2
Hi Israr. :smile: http://img96.imageshack.us/img96/5725/red5e5etimes5e5e45e5e25.gif

Good luck with your study of science.

Technical questions belong in the technical forums. I've moved your thread to a suitable forum where it can be appropriately discussed.
 
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  • #3
Israr said:
Why ISS need to run on such high speed 7.7km/s ?
What will affect if it made to run on very slower speed.

thanks

Hi Israr, welcome to PF.

The speed of any object in orbit in a gravitational field (planets around stars, moons around planets, the ISS around the Earth) is determined by the orbital height of the object.

For a circular orbit, and something of negligable mass compared to the other body (e.g. the ISS around the Earth, or the Earth around the sun) this is roughly equal to

##v \approx \sqrt{\frac{G M}{r}}##.

Where G is the gravitational constant, M the mass of the body being orbited around, and r the radius. If you plug in the mass of the earth, and the radius of orbit of the ISS (~412 km above sea level) into that equation, you see that you get 7.7 km/s!

So, you see that if you wanted the ISS to go at a much slower speed, you'd have to push it much further away from the Earth!
 
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  • #5
Israr said:
What will affect if it made to run on very slower speed.

If the ISS were to fire its thrusters and slow down, it would fall into the Earth's atmosphere.
 
  • #6
paisiello2 said:

The speed to completely escape Earth's gravity is something very different from the speed to be in a stable orbit.

@Israr , the ISS *could* fly slower, but in order to still have a stable orbit (i.e. neither falling towards Earth nor flying away from it) the station would have to be in a higher orbit. The higher the orbit, the slower the speed necessary (as evidenced by the formula e.bar.goum quoted)
 
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  • #7
rumborak said:
The speed to completely escape Earth's gravity is something very different from the speed to be in a stable orbit.
You're absolutely right, I erroneously thought they were the same thing. Why do you use ≈?
 
  • #8
I don't, that was e.bar.goum.
 
  • #9
paisiello2 said:
...Why do you use ≈ ?

Did you read the sentence immedialy prior to that equation that e.bar.goum wrote ?
it answers that question

Dave
 
  • #10
The equation is derived by equating the centrifugal force to the gravitational force. The small mass m cancels out so I don't why it needs to be "negligible mass".

For a circular orbit, which the ISS is pretty close to, this is exact.
 
  • #11
paisiello2 said:
The equation is derived by equating the centrifugal force to the gravitational force. The small mass m cancels out so I don't why it needs to be "negligible mass".

For a circular orbit, which the ISS is pretty close to, this is exact.

Yes, but you can only make that equality for stable, well behaving orbits. If the masses of the bodies are similar, and the orbits are eccentric you'll get into trouble.

As you say, for the ISS it's pretty much exact, but I didn't want to give the impression that this is true in general for all orbits, hence the caveats.
 
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  • #12
e.bar.goum said:
Hi Israr, welcome to PF.

The speed of any object in orbit in a gravitational field (planets around stars, moons around planets, the ISS around the Earth) is determined by the orbital height of the object.

For a circular orbit, and something of negligable mass compared to the other body (e.g. the ISS around the Earth, or the Earth around the sun) this is roughly equal to

##v \approx \sqrt{\frac{G M}{r}}##.

Where G is the gravitational constant, M the mass of the body being orbited around, and r the radius. If you plug in the mass of the earth, and the radius of orbit of the ISS (~412 km above sea level) into that equation, you see that you get 7.7 km/s!

So, you see that if you wanted the ISS to go at a much slower speed, you'd have to push it much further away from the Earth!
Thanks
 
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What is the speed of the International Space Station?

The International Space Station (ISS) travels at an average speed of approximately 17,500 miles per hour (28,000 kilometers per hour). This speed allows the ISS to orbit the Earth every 90 minutes.

Why does the International Space Station need to travel at such a high speed?

The ISS needs to travel at a high speed in order to counteract the Earth's gravitational pull and maintain its orbit. If the ISS were to slow down, it would begin to fall towards the Earth.

How is the speed of the International Space Station measured?

The speed of the ISS is measured using a variety of instruments, including GPS systems, radar, and laser ranging devices. These instruments track the ISS's position and calculate its speed based on its distance traveled over a certain amount of time.

Does the speed of the International Space Station ever change?

Yes, the speed of the ISS can change due to a variety of factors such as atmospheric drag, adjustments made by thrusters, and gravitational forces from other objects in space. However, these changes are small and typically do not significantly impact the ISS's overall speed.

Can the speed of the International Space Station be increased or decreased?

Yes, the ISS's speed can be increased or decreased by using thrusters to adjust its orbit. However, changes to the ISS's speed must be carefully planned and executed in order to maintain its orbit and avoid collisions with other objects in space.

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