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

  • Thread starter Thread starter sillybean
  • Start date Start date
  • Tags Tags
    Homework Laws
AI Thread Summary
The discussion revolves around calculating the acceleration due to gravity on an asteroid and determining its rotational period before loose rocks fly off its surface. The correct acceleration due to gravity was found to be 2.1 x 10^-3 m/s^2. For the rotational period, the initial approach using escape velocity was incorrect; instead, centripetal acceleration must equal gravitational acceleration. The final calculation yielded a rotational period of approximately 2.8 hours after correcting the method. The conversation highlights the importance of using appropriate formulas for rotational motion in astrophysics.
sillybean
Messages
18
Reaction score
0
[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?
 
Physics news on Phys.org
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?
 
Thread 'Variable mass system : water sprayed into a moving container'
Starting with the mass considerations #m(t)# is mass of water #M_{c}# mass of container and #M(t)# mass of total system $$M(t) = M_{C} + m(t)$$ $$\Rightarrow \frac{dM(t)}{dt} = \frac{dm(t)}{dt}$$ $$P_i = Mv + u \, dm$$ $$P_f = (M + dm)(v + dv)$$ $$\Delta P = M \, dv + (v - u) \, dm$$ $$F = \frac{dP}{dt} = M \frac{dv}{dt} + (v - u) \frac{dm}{dt}$$ $$F = u \frac{dm}{dt} = \rho A u^2$$ from conservation of momentum , the cannon recoils with the same force which it applies. $$\quad \frac{dm}{dt}...
Back
Top