- #1
matteo446
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- Homework Statement
- A comet of mass m is orbiting around the Sun in a parabolic orbit. Assume that Earth's orbit is circular with radius rT and that it's coplanar with the orbit of the comet.
Determine the time T that the comet spends inside Earth's orbit if the periaster (nearest point to the Sun) of the comet is rP=rT/3.
Determine the maximum time that the comet can spend inside Earth's orbit tMax.
- Relevant Equations
- U(r) = L^2/(2mr^2) - GmM/r where L is angular momentum of the body from P, m is the mass of the body orbiting r(θ) = ed/(1+ecos(θ)) where e is the eccentricity and d is the distance from the directrix
I tried in the first place to use the effective potential of a parabolic orbit which is 0 to get the angular momentum L.
Evaluating the function U(r) at r = rP i get U(rP) = L^2/(2m(rP)^2) - GmM/rP = 0.
Here I get L = m√(2GMrP).
Now the relationship between angular momentum L and areal velocity α is L/2m = √((1/6)GMrT) which is a constant of motion.
My idea is to find an area and use this value of α to obtain time T.
With respect to a polar frame of reference centered at S i used the general equation for a conic in polar coordinates r(θ) = ed/(1+ecos(θ)) with e=1 for a parabola so r(θ)=d/(1+cos(θ)).
I know r(0) = rP so replacing rP = d/2 and d = 2rP.
So the comet follows the orbit of equation r(θ) = 2rP/(1+cos(θ)).
Now I want to find the angle λ to replace in the equation to get rT as the point of intersection between the orbits satisfies also the equation for the orbit of the Earth r(θ) = rT.
I get λ = arcos(-1/3) ≈ 1.9 rad.
So (here i think I made mistakes as i don't know polar integration) integrating from 0 to 1.9 and multiplying by 2 because of symmetry the area A is 2*(1/2 ∫(2rP/1+cosθ)^2dθ) ≈ 1.9rP^2 = (1.9/9)*rT^2.
Now simply T = A/α = ((1.9/9)*rT^2)/√((1/6)GMrT) ≈ 9.5*10^-3s which is very wrong.
I don't know how to start for the second question.