According to Keplers 3rd Law, how would a planets orbital period change if the planets...
a. eccentricity doubled?
b. mass halved?
c. distance from the sun quadrupled?
where is the orbital period of the planet and is the semi-major axis of the orbit.
if eccentricity is doubled
then e=c/a (a must be halved) 2e=c/a/2 let (a/2=a')
so
p^2/p'^2=a^3/a'^3 (p' and a' are new time periods and lengths)
solving we get
p'=p/2sqrt(2) or p/2.82
b)
For circular orbits, Kepler's 3rd Law is also commonly represented as
or simply
t^2=cr^3/m
where c=proportinality constant
let t' and r' and m' be new constants
t^2/t'^2=(cr^3/m)/(cr^3/m') but (r=r')
t^2/t'^2=m'/m and m'=m/2
t'=sqrt(2)*t or 1.41(t)
c)
t^2=cr^3
let t' and r' be new constants
r'=4r
t^2/t'^2=r^3/r'^3
t^2/t'^2=r^3/64r^3
t'=8t
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