Space station angular rotation

In summary, a space station with a mass of 6.0 × 10^4 kg is being constructed in the shape of a thin annular cylinder with an inner radius of 100 m and outer radius of 105 m. Artificial gravity will be implemented by rotating the hoop through its central axis. Two rockets with a thrust of 102 N will be fired tangentially to opposite points on the hoop to set it into rotation. To achieve the desired rotation, the rockets must be fired for a certain time interval, which is being asked to calculate in minutes. The calculation of the moment of inertia assumes equal mass on both the inner and outer tube, and the difference in mass is assumed to be negligible. The issue of whether the rockets
  • #1
ft92
19
1

Homework Statement


A space station of mass 6.0 × 104-kg is to be constructed in the shape of a thin annular cylinder (or ring). The inner radius of the annular cylinder is 100-m, and the outer radius (and location of the floor) is 105-m. Artificial gravity equivalent to free-fall acceleration, g, will be implemented by rotating the hoop through its central axis. Once the space station is constructed, two small rockets attached tangentially to opposite points on the hoop will be fired to set the space station into rotation. If each of the rockets produces a thrust of 102-N, for what time interval, in minutes, must they be fired to achieve the desired rotation? Assume the mass of the space station will be distributed uniformly within the annular ring.

I'm asked to find t in minutes.

Homework Equations

The Attempt at a Solution


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  • #2
The floor is at the outer radius. So it seems to me that you need to set the acceleration equal to g at the outer radius rather than the inner radius. This would not make a big difference.

Did you account for the fact that there are two rockets?

Otherwise, your work looks good to me.
 
  • #3
Can you explain your calculation of the moment of inertia of the space station in more detail? In particular, why do you add the squares of the two radii?
 
  • #4
The inertia calculation assumes that there is equal mass on both the inner and the outer tube. Thus, the total inertia is (1/2)MR_1^2 + (1/2)MR_2^2, which he factored. That assumption should be valid, since the difference in mass wouldn't be much. ft92, what is the actual issue here? How far off are you from the correct answer?
 
  • #5
Torus moment of inertia is a bit more subtle (there is more mass at the outside), but it doesn't make a big difference. Do the rockets deliver 102 N or 102 N of thrust ?
 

Related to Space station angular rotation

1. What is space station angular rotation?

Space station angular rotation refers to the movement of the space station around its own axis. This rotation is responsible for creating artificial gravity within the space station.

2. How fast does a space station rotate?

The speed of rotation for a space station varies depending on its size and distance from Earth, but most space stations rotate at a rate of about 10-15 times per hour.

3. Why is angular rotation important for a space station?

Angular rotation is important for a space station because it creates a sense of gravity for the astronauts living and working on board. This helps them maintain their physical health and perform tasks more easily.

4. Can the angular rotation of a space station be adjusted?

Yes, the angular rotation of a space station can be adjusted by using thrusters or gyroscopes. This allows astronauts to change the speed or direction of rotation if needed.

5. Is there any danger associated with space station angular rotation?

No, space station angular rotation is carefully monitored and controlled to ensure the safety of the astronauts on board. Any changes in rotation are carefully planned and executed by the ground control team.

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