Speed of International Space Station

AI Thread Summary
The International Space Station (ISS) orbits at a speed of 7.7 km/s due to its altitude of approximately 412 km above Earth, as determined by gravitational forces. Slowing the ISS would necessitate a higher orbit to maintain a stable trajectory; otherwise, it would descend into the atmosphere. The orbital speed is derived from the balance of gravitational and centrifugal forces, which is specific to circular orbits. If the ISS were to reduce speed without changing its altitude, it would risk falling back to Earth. Thus, maintaining its current speed is essential for its operational stability in orbit.
Israr
Messages
2
Reaction score
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
 
Physics news on Phys.org
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.
 
Last edited by a moderator:
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!
 
  • Like
Likes Israr
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)
 
  • Like
Likes Israr
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
 
  • #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.
 
  • Like
Likes davenn
  • #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
 
  • Like
Likes e.bar.goum
Back
Top