Circular Motion of a space station Problem

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Homework Help Overview

The problem involves calculating the required rotation speed of a circular space station to simulate Earth's gravity. The diameter of the station is given as 1.30 km, and the goal is to determine the rotation speed in revolutions per day that would create a force equivalent to gravity.

Discussion Character

  • Exploratory, Conceptual clarification, Mathematical reasoning

Approaches and Questions Raised

  • Participants discuss various methods to derive the rotation speed, including using centripetal force equations and energy considerations. Questions arise regarding the correct units for time and the implications of substituting values into equations with multiple unknowns.

Discussion Status

The discussion is ongoing, with participants exploring different approaches to the problem. Some guidance has been offered regarding the use of variables before substituting numerical values, and there is a focus on ensuring correct unit conversions. Multiple interpretations of the problem setup are being examined.

Contextual Notes

Participants note the importance of checking units for the radius and the potential complexity introduced by having multiple unknowns in the equations. The problem is framed within the constraints of a homework assignment, emphasizing the need for careful reasoning and understanding of the concepts involved.

kye6338
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Hi,
I was hoping I could get some help on these problems. Here's the first problem:
1. A projected space station consists of a circular tube that is set rotating about its center (like a tubular bicycle tire). The circle formed by the tube has a diameter of about D = 1.30km. What must be the rotation speed (in revolutions per day) if an effect equal to gravity at the surface of the Earth (1g) is to be felt?

So here's what I did: I converted the diameter from km to m, then got the radius, which is 650 km. Then, I found the velocity of the station by doing v= sqrt r x g . I got 79.81 m/s. And then I used the formula T= 2PiR/V ...and I got 51.17. My question would be what are the units at this point? I assumed it was revolutions per second, then converted to revolutions per day, but that was not correct. Maybe I'm missing a step, so please help!
 
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It is easier so substitute the values you were given at the very end. Only consider the center of mass of the space station. This allows you to write the following:

[tex]v=\frac{\Delta x}{\Delta t} = \frac{C}{T} = \frac{2\pi (R + d)}{T}[/tex]

and

[tex]a=\frac{v^2}{(R+d)}[/tex]

where "R" is the radius of the Earth "d" is the distance from the surface of the Earth. I hope it helps.
 
Do you mean substituting the values given in the problem into those equations? If I did that, wouldn't I have two unknowns with v and T?
 
You can find V with some energy equations, and T is the time of one revolution of the satelite. Notice those are just the equations for average velocity and centripetal acceleration.

He was pointing out that it is easier (and less likely to induce error) if you solve the problem in terms of its variables first, THEN plug in numbers at the very end.
 
kye6338 said:
Hi,
I was hoping I could get some help on these problems. Here's the first problem:
1. A projected space station consists of a circular tube that is set rotating about its center (like a tubular bicycle tire). The circle formed by the tube has a diameter of about D = 1.30km. What must be the rotation speed (in revolutions per day) if an effect equal to gravity at the surface of the Earth (1g) is to be felt?
One is asked to find a rotational speed [itex]\omega[/itex] such that the force exerted on a mass (m) would be equivalent to mg, where g is the acceleration due to gravity at the Earth's surface, 9.81 m/sec2.

One could simply use a force balance mg = mv2/r = m[itex]\omega^2[/itex]r.

Also, check units on the radius.

For some insight, see -

angular velocity,
centripetal force, and
centripetal acceleration.
 
Last edited:

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