Space station rotation problem

In summary, the conversation discusses two physics problems, one involving a rotating space station and the other involving a coin on a rotating record. The first problem asks for the frequency at which the space station must rotate to simulate Earth's gravity, while the second problem asks for the maximum distance the coin can be placed from the center without slipping off. The conversation also includes a hint for the first problem and a clarification question for the second problem.
  • #1
Purduenub03
11
0
Quick physics help please

First off, I'm new to the board and want to say hi to everyone! I hope i can give and take from this site, i should be helpful in the chem forums, but physics is not my best. I have 2 quick questions if you could help me that'd be great.

A space station is shaped like a ring and rotates to simulate gravity. If the radius of the space station is 120 m, at what frequency must it rotate so that it simulates Earth's gravity? [Hint: The apparent weight of the astronauts must be the same as their weight on Earth.] - in rev/s

I did the following and got it wrong
9.8 = V^2/120, found v = 34.29m/s
34.29 / 2*pi*120 = .045 rev / s

Where have i gone wrong?/

A coin is placed on a record that is rotating at 33.3 rpm. If the coefficient of static friction between the coin and the record is 0.3, how far from the center of the record can the coin be placed without having it slip off?

I'm plain lost on this one.
 
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  • #2
Purduenub03 said:
First off, I'm new to the board and want to say hi to everyone! I hope i can give and take from this site, i should be helpful in the chem forums, but physics is not my best. I have 2 quick questions if you could help me that'd be great.

A space station is shaped like a ring and rotates to simulate gravity. If the radius of the space station is 120 m, at what frequency must it rotate so that it simulates Earth's gravity? [Hint: The apparent weight of the astronauts must be the same as their weight on Earth.] - in rev/s

I did the following and got it wrong
9.8 = V^2/120, found v = 34.29m/s
34.29 / 2*pi*120 = .045 rev / s

Where have i gone wrong?/

Looks okay to me. How do you know you're wrong ? Do you know what the answer should be ?

A coin is placed on a record that is rotating at 33.3 rpm. If the coefficient of static friction between the coin and the record is 0.3, how far from the center of the record can the coin be placed without having it slip off?

I'm plain lost on this one.

How much force would you need to exert on a body to overcome friction, and cause it to slide? In the rest frame of the coin, this force would be provided by the centrifugal force. Remember, the linear velocity depends on the distance of the coin from the record center.

PS : Welcome to PF. It's a great place to be ! :biggrin:
 
  • #3


Hi there! Welcome to the board. In regards to your first question about the space station rotation problem, you have the right idea but there are a few things you need to consider. First, the equation you used (9.8 = V^2/120) is the equation for centripetal acceleration, not frequency. To find the frequency, you need to use the equation w = v/r, where w is angular velocity, v is linear velocity, and r is the radius. So in this case, w = 34.29/120 = 0.285 rev/s. This is the angular velocity, not the frequency. To find the frequency, you need to divide the angular velocity by 2*pi, so the frequency would be 0.045 rev/s, just like you calculated. However, you need to convert this to Hz (Hertz), which is the unit for frequency. To do this, you need to multiply by 60, since there are 60 seconds in a minute. So the final answer would be 0.045*60 = 2.7 Hz.

For your second question about the coin on the record, you need to use the equation for centripetal force, which is Fc = mv^2/r. In this case, the force is equal to the coefficient of static friction (0.3) times the normal force (which is the weight of the coin, mg). So the equation would be 0.3mg = mv^2/r. You can rearrange this to solve for r, which would be r = mv^2/0.3mg. Since you are given the angular velocity (33.3 rpm), you can use the equation v = wr, where w is the angular velocity in radians per second. So w = 33.3*2*pi/60 = 3.49 rad/s. Plug this into the equation and you should be able to solve for r.

I hope this helps! Don't hesitate to ask for clarification if needed. Good luck!
 

What is the space station rotation problem?

The space station rotation problem refers to the issue of maintaining the orientation and stability of a space station in orbit. Due to various factors such as gravitational forces, atmospheric drag, and solar radiation, space stations can experience changes in their rotational speed and tilt, which can affect their functionality.

What causes the space station rotation problem?

The space station rotation problem is primarily caused by external forces acting on the space station, such as gravitational pull from celestial bodies, atmospheric drag, and solar radiation pressure. These forces can cause changes in the space station's rotational speed and tilt, leading to potential stability issues.

How do scientists address the space station rotation problem?

Scientists address the space station rotation problem by using a combination of methods, including thruster firings, reaction wheels, and gyroscopes. These systems can adjust the space station's orientation and rotational speed to counteract the effects of external forces and maintain stability.

What are the potential consequences of the space station rotation problem?

The space station rotation problem can have various consequences, such as affecting the functioning of equipment on the space station, causing communication disruptions, and potentially endangering the lives of astronauts on board. It can also impact the overall mission objectives and result in costly repairs or replacements.

How is the space station rotation problem being addressed in future space missions?

In future space missions, the space station rotation problem is being addressed by designing more advanced and reliable systems for maintaining the orientation and stability of space stations. This includes the use of artificial intelligence and autonomous control systems to make real-time adjustments and reduce the need for human intervention.

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