Speed of International Space Station

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SUMMARY

The International Space Station (ISS) operates at a speed of 7.7 km/s due to its orbital height of approximately 412 km above sea level. This speed is derived from the equation v ≈ √(G M/r), where G is the gravitational constant, M is the mass of the Earth, and r is the radius of orbit. Slowing the ISS would necessitate a higher orbit to maintain a stable trajectory; otherwise, it risks falling into the Earth's atmosphere. The distinction between escape velocity and stable orbital speed is crucial for understanding orbital mechanics.

PREREQUISITES
  • Understanding of gravitational forces and orbital mechanics
  • Familiarity with the equation v ≈ √(G M/r)
  • Knowledge of the concept of escape velocity
  • Basic physics principles related to circular motion
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  • Research the implications of orbital height on satellite speed
  • Study the gravitational constant and its role in orbital calculations
  • Explore the differences between escape velocity and orbital velocity
  • Learn about the effects of atmospheric drag on low Earth orbit satellites
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Aerospace engineers, astrophysicists, students of physics, and anyone interested in the mechanics of satellite orbits and space travel.

Israr
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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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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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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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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.
 
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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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 ≈?
 
I don't, that was e.bar.goum.
 
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
 
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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.
 
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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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