Kepler's Laws: Escape Velocity and Rotational Period of Asteroid

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Homework Help Overview

The discussion revolves around a problem involving Kepler's Laws, specifically focusing on an asteroid's gravitational acceleration and its rotational period. The asteroid is defined by its radius and mass, and participants are exploring the implications of these parameters on the motion of objects on its surface.

Discussion Character

  • Mixed

Approaches and Questions Raised

  • Participants discuss calculating the acceleration due to gravity on the asteroid's surface and the relationship between angular speed and rotational period. There is an exploration of using centripetal acceleration in relation to gravitational acceleration to find the correct period of rotation.

Discussion Status

Some participants have provided guidance on the relationship between centripetal acceleration and gravitational acceleration, suggesting a different approach to the problem. There is an ongoing exploration of the reasoning behind the use of certain equations and the implications of the asteroid's characteristics on the calculations.

Contextual Notes

Participants are questioning the validity of using escape velocity equations in this context, considering the proximity to the asteroid's surface and the definitions involved. There is also a mention of the need to convert units appropriately in the calculations.

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[SOLVED] Kepler's Laws

Homework Statement



Consider an asteroid with a radius of 11 km and a mass of 3.8×1015 kg.
Assume the asteroid is roughly spherical.

a) What is the acceleration due to gravity on the surface of the asteroid?
b)Suppose the asteroid spins about an axis through its center, like the Earth, with a rotational period T.
What is the smallest value T
can have before loose rocks on the asteroid's equator begin to fly off the surface? (answer in hours)

Homework Equations



gA = G(MA/RA^2)

w (angular velocity) = v esc (escape speed)/RA

*note just some notational stuff: MA = mass of asteroid and RA = its radius

T=2pi/w (angular velocity)

The Attempt at a Solution



I got part A just fine. Its just a good ol' plug and chug. I got gA= 2.1x10^-3 m/s^2 which is right.

For part B however, I was thinking that if i calculated the angular speed (since its rotational motion) and then just used the formula for a period of rotational motion I could get the seconds and then just easily convert that into hours. Anyway here's my work.

w = sq root (2GM/RA)/RA

since GM/RA is just equal to gA

w=sq root (2gA/RA)

w= sq root(2*2.1X10^-3/11000)= sq root (3.81E-7) = 6.179E-4 rad/s

then i plugged that number into T=2pi/w

T= 2pi/6.179E-4 = 10168.375 s

10168.375 (1/3600) = 2.8 hours

Unfortunately, that answer is wrong. What am i doing wrong?
 
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sillybean said:
For part B however, I was thinking that if i calculated the angular speed (since its rotational motion) and then just used the formula for a period of rotational motion I could get the seconds and then just easily convert that into hours. Anyway here's my work.

w = sq root (2GM/RA)/RA

since GM/RA is just equal to gA

w=sq root (2gA/RA)

What do you mean with "the formula for a period of rotational motion"

I'd use the fact that gA must be equal to the centripetal acceleration, which gives something ldifferent from: w=sq root (2gA/RA)
 
I meant the period of rotation formula T=2pi/w (angular acceleration)
 
ah that worked. genius! thanks.
 


sillybean said:
ah that worked. genius! thanks.



What worked? I've been trying to figure out how you went wrong for an hour...what did you change?
 


What they meant was that you get the right answer if you set the centripetal acceleration equal to the acceleration due to gravity of the asteroid, solve for velocity, find angular momentum, divide by 3600.
I still don't understand why you couldn't use the equation for escape velocity. Because it's too close to the surface?
 

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