Centripetal acceleration on Earth

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SUMMARY

The discussion centers on calculating the centripetal acceleration of an object orbiting Earth at a radius of 6.38 x 106 m. The initial calculation yielded an acceleration of 3.37 x 10-2 m/s2, which is significantly different from the expected value of 0.006 m/s2. Participants highlighted the importance of using the correct velocity, which should be approximately 7.9 x 103 m/s for a satellite in low Earth orbit, as opposed to the equatorial rotation velocity of Earth. The correct formula for centripetal acceleration is a = ω2 * r, where ω is the angular velocity.

PREREQUISITES
  • Centripetal acceleration concepts
  • Angular velocity calculations
  • Understanding of gravitational force equations
  • Basic circular motion physics
NEXT STEPS
  • Study the derivation of centripetal acceleration using a = ω2 * r
  • Learn about gravitational force equations, specifically GMm/r2 = mv2/r
  • Research the differences between equatorial rotation velocity and orbital velocity
  • Explore the implications of centripetal acceleration equating to gravitational acceleration at ground level
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Students studying physics, particularly those focusing on mechanics and orbital dynamics, as well as educators seeking to clarify concepts related to centripetal acceleration and gravitational forces.

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Homework Statement


An object orbits the Earth at a constant speed in a circle of radius 6.38 x 106 m, very close to but not touching the Earth's surface. What is its centripetal acceleration?


Homework Equations


a = v2/r = 4\pi2v/T2
v = 2\pir/T

The Attempt at a Solution


I plugged in r = 6.38 x 106 m and T = 24.0 h = (24.0 h x 3600 s / 1 h) = 86,400 s into the equation above and found a = 3.37 x 10-2 m/s2. However, I looked up the centripetal acceleration on the Earth's surface and found out it is 0.006 m/s2. I can't understand why my answer is wrong. Can anyone point out the error in my logic?

Thanks!
 
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Try using this formula- 2\pi/\omega

\omega= 360/24*3600


Let me know if you got the answer.
 
Thanks for the suggestion RoughRoad but I don't really understand how I am supposed to use this equation.

I found that my calculation for the angular velocity (2piR/T) is approximately equal to the wikipedia value for angular velocity, so I really am confused now because I can't see what I'm doing wrong in just squaring that value and dividing by 6.38 x 106.
 
Is the mass of the satellite given?
 
No, it isn't.
 
try using the equation GMm/r^2=mv^2/r
m-mass of satellite
M-mass of earth
r-radius of orbit
v^2/r is the centripetal acceleration
 
gravitational frce of Earth is utilised for centripetal force
 
jyothsna pb said:
try using the equation GMm/r^2=mv^2/r
m-mass of satellite
M-mass of earth
r-radius of orbit
v^2/r is the centripetal acceleration

You are right. But what about the velocity?
 
you are asked to find the centripetal acceleration you just have to find the value of v^2/r which gives the centripetal acceleration
 
  • #10
jyothsna pb said:
you are asked to find the centripetal acceleration you just have to find the value of v^2/r which gives the centripetal acceleration


Oh yeah! How can I be so foolish. Thanks for helping!
 
  • #11
hope you got the answer
 
  • #12
u r welcome
 
  • #13
And reply to my visitor msg pls
 
  • #14
I didn't, though, and that's the source of my confusion. I know I have the right value for v but when I plug it into v^2/r, I get 3.37 x 10^-2 m/s^2. This answer is not equal to the answer I found for the actual acceleration, which is 0.006 m/s^2. My question is why is my answer different from the real value?
 
  • #15
what is the value of v?
 
  • #16
465.1 m/s
 
  • #17
there is some error in the velocity value
 
  • #18
we get acceleration value almost equal to g
 
  • #19
velocity in dis orbit must b approximately equal to 7.9*10^3m/s
 
  • #20
I don't understand why that is, especially since Wikipedia says it is 451 m/s
en.wikipedia.org/wiki/Earth
 
  • #21
it wud b easy if u jus show me dat particular part from d article
 
  • #22
It's on the sidebar, under "Physical Characteristics".
 
  • #23
it is equatorial rotation velocity of Earth while that mentioned here is the velocity of a satellite of Earth in an orbit very close to it both r different
 
  • #24
The centripetal acceleration must balance out the acceleration due to gravity (it is essentially at ground level, so 9.8 m/s^2).

*Force of gravity = mg
*Centripetal acceleration = a (not v^2/r, because you are solving for this total value, not any sub-values within a)

The centripetal acceleration when traveling in a constant circular orbit at ground level on Earth should be equal to gravity, or 9.8. You don't necessarily need velocity, radius, mass, time, etc.
 
  • #25
Try this-

Centripetal acceleration= \omega^2*r= (2\pi/T)*r

Let me know if you got the answer.
 
  • #26
RoughRoad said:
Try this-

Centripetal acceleration= \omega^2*r= (2\pi/T)*r

Let me know if you got the answer.
but the problem is that the period is unknown, i think
 
  • #27
Jokerhelper said:
but the problem is that the period is unknown, i think

The body moves with a constant speed, so it's T should be 24*3600. I may be wrong though.
 

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