How Does the Mass of the ISS Affect Its Orbital Motion?

Click For Summary
SUMMARY

The discussion centers on the orbital dynamics of the International Space Station (ISS), which orbits Earth at an altitude of 350 km. Key calculations involve determining the orbital period and velocity using Newton's law of universal gravitation and centripetal acceleration. The mass of the ISS does not affect its orbital speed, but any increase in mass requires careful consideration of momentum when adjusting the speed of the shuttle during component attachment. Additionally, for a geosynchronous orbit, the altitude must be approximately 35,786 km, where the orbital period matches that of Earth's rotation.

PREREQUISITES
  • Newton's law of universal gravitation
  • Circular motion principles
  • Centripetal acceleration concepts
  • Orbital mechanics fundamentals
NEXT STEPS
  • Calculate the orbital period using the formula T = 2π√(r³/GM)
  • Explore the relationship between mass and orbital velocity in circular motion
  • Research geosynchronous orbits and their altitude requirements
  • Study the implications of momentum conservation in orbital mechanics
USEFUL FOR

Aerospace engineers, physics students, and anyone interested in understanding the mechanics of orbital motion and the dynamics of space stations.

billybobay
Messages
13
Reaction score
0
I'm not asking for you to do my homework but can you help me on it?! I have no idea how to even attempt it. Any help would be greatly appreciated!

The International Space Station (ISS) just celebrated its 10th anniversary of human habitation. During that time it has been orbiting the Earth at an altitude of 350 Km.

a. If the radius of the Earth is 6,370 Km, what is the period of orbit for the ISS?
b. Does the orbiting speed of the ISS depend on its mass?
c. Suppose the ISS is in a stable orbit when the space shuttle brings in a new component for attachment. This increases the mass of the ISS. Do the astronauts have to adjust the speed of the shuttle to maintain the same orbit? (hint: momentum is always a factor in our universe) Explain your reason for your answer.
d. If the ISS were to be moved to a geosynchronous orbit (always staying above the same point on the earth), What would the new altitude of the ISS have to be?





2. The attempt at a solution

a. 6370+350=6720 km is the period of orbit? is that correct?
b. I need a lot of help!
c. I need a lot of help!
d. I need a lot of help!
 
Physics news on Phys.org
hmmm, if your teacher is setting you this homework, then I guess he/she has already taught you the relevant concepts? The important topics for this question are: Newton's law of universal gravitation, circular motion and centripetal acceleration. look back at your notes, and hopefully it will start to make sense. Also, has your teacher gone through these types of questions in class with you yet?
 
For a, the orbital period is the time it takes for the object to do 1 complete orbit.
 
a) period is the time it takes to complete a circle around the earth. It is in units of time. you just calculated the radius of the orbit, which you will need to calculate the orbital velocity.
Orbital velocity v=sqrt(Gm/r). Do you know G,m and r? When you have the velocity, you can calculate how long it takes to traverse a circle with radius 6720 km.
b) Is the mass of the ISS in the equation for the period?
c) what does the hint mean?
d) When the ISS is always above the same point above the earth, what is the period of the ISS compared to the period of the earth?
 

Similar threads

  • · Replies 2 ·
Replies
2
Views
2K
  • · Replies 4 ·
Replies
4
Views
2K
  • · Replies 4 ·
Replies
4
Views
2K
  • · Replies 1 ·
Replies
1
Views
2K
  • · Replies 8 ·
Replies
8
Views
2K
  • · Replies 27 ·
Replies
27
Views
4K
  • · Replies 6 ·
Replies
6
Views
2K
  • · Replies 4 ·
Replies
4
Views
5K
  • · Replies 4 ·
Replies
4
Views
3K
  • · Replies 4 ·
Replies
4
Views
2K