RPM required to simulate Earth's gravity (Centrifugal acceleration)

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SUMMARY

The discussion centers on calculating the required RPM to simulate Earth's gravity in a rotating spacecraft section with a radius of 30 meters. The correct RPM to achieve 1 g (9.8 m/s²) is 14 RPM, as derived from the formula A = V²/R. The confusion arose from differing methods of calculation, where one participant mistakenly used the circumference instead of the radius in their calculations, leading to an incorrect answer of 5.5 RPM. The correct approach involves using the angular speed formula, which confirms that the instructor's method was flawed.

PREREQUISITES
  • Understanding of centrifugal acceleration and its relation to gravity.
  • Familiarity with the formula A = V²/R for circular motion.
  • Knowledge of angular velocity and its conversion to RPM.
  • Basic proficiency in algebra for manipulating equations.
NEXT STEPS
  • Study the relationship between angular velocity and linear velocity in circular motion.
  • Learn how to derive RPM from angular speed using the formula RPM = (60/2π) * ω.
  • Explore the implications of centrifugal force in spacecraft design for simulating gravity.
  • Investigate other methods for calculating forces in rotating systems, such as using centripetal acceleration.
USEFUL FOR

Aerospace engineers, physics students, and anyone involved in spacecraft design or studying rotational dynamics will benefit from this discussion.

jwlgrant
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Homework Statement



Here's the problem: "On a journey to Mars, one design is to have a section of the spacecraft rotate to simulate gravity. If the radius of this section is 30 meters, how many RPMs must it rotate to simulate one Earth gravity (1 g = 9.8 meters/sec^2)?"

Homework Equations



A = \frac{V^2}{R}

The Attempt at a Solution



I completed this problem, getting an answer of 5.5 RPM. Apparently I was wrong, and the answer should have been 14 RPM. I asked my instructor about it, and he showed me the calculations used to get 14 RPM, but it still didn't quite make sense to me.

Here's the process my instructor used to solve the problem:
Circumference is C = 2∏(30) = 188 meters.

1 rpm is like rotating 1 full circular rotation every minute, so 188/60 = 3.1 meters/sec.

Then V = 3.1 meters/sec x RPM.

Then A = (3.1 RPM)^2/188 = 0.05 x rpm^2.

So: 9.8 = 0.05rpm^2

RPM = 14

--

Here's my process:
A = 9.8 (m)/(s^2)
R = 30 m
V = √(AR)
V = 17.15 m/s

1 revolution = circumference = 2∏30 m
[1 revolution/(2∏30 m)] * [60s/1 min] (1 rev is equal to 2π30m and sixty seconds is equal to one minute)
V = (17.15 m/s)/∏ RPM
V = 5.5 RPM

--

I realize, of course, that we both used different methods to get the answer. I thought I did it wrong, so I solved the problem again, using his method, to try to get the correct answer. He used 188m for the radius component when solving for A=V^2/R, but when I used 30m I got an answer of 5.5RPM. The radius, 30m, should be used in that equation, not 188m, right?

I would greatly appreciate any help in understanding this problem. I can't tell where/how I went wrong in solving it.
 
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jwlgrant said:

Homework Statement



Here's the problem: "On a journey to Mars, one design is to have a section of the spacecraft rotate to simulate gravity. If the radius of this section is 30 meters, how many RPMs must it rotate to simulate one Earth gravity (1 g = 9.8 meters/sec^2)?"

Homework Equations



A = \frac{V^2}{R}

The Attempt at a Solution



I completed this problem, getting an answer of 5.5 RPM. Apparently I was wrong, and the answer should have been 14 RPM. I asked my instructor about it, and he showed me the calculations used to get 14 RPM, but it still didn't quite make sense to me.

Here's the process my instructor used to solve the problem:
Circumference is C = 2∏(30) = 188 meters.

1 rpm is like rotating 1 full circular rotation every minute, so 188/60 = 3.1 meters/sec.

Then V = 3.1 meters/sec x RPM.

Then A = (3.1 RPM)^2/188 = 0.05 x rpm^2.
Why is he dividing by 188 (circumference)?? Should be 30.

So: 9.8 = 0.05rpm^2

RPM = 14

--

Here's my process:
A = 9.8 (m)/(s^2)
R = 30 m
V = √(AR)
V = 17.15 m/s

1 revolution = circumference = 2∏30 m
[1 revolution/(2∏30 m)] * [60s/1 min] (1 rev is equal to 2π30m and sixty seconds is equal to one minute)
V = (17.15 m/s)/∏ RPM
V = 5.5 RPM

--

I realize, of course, that we both used different methods to get the answer. I thought I did it wrong, so I solved the problem again, using his method, to try to get the correct answer. He used 188m for the radius component when solving for A=V^2/R, but when I used 30m I got an answer of 5.5RPM. The radius, 30m, should be used in that equation, not 188m, right?

I would greatly appreciate any help in understanding this problem. I can't tell where/how I went wrong in solving it.
You are right and the instructor is wrong.

It is easier to use Ac = ω2r; so \omega = \sqrt{A/r} where ω is the angular speed in radians/sec.

Letting RPM = 60ω/2∏:

RPM = \frac{60}{2\pi}*\sqrt{A/r} = \frac{60}{2\pi}\sqrt{9.8/30} = 5.5

AM
 
Last edited:
Then A = (3.1 RPM)^2/188 = 0.05 x rpm^2.
I also agree, it must be divided by radius = 30 not circumference.
 

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