the time period of satellite of earth in a circular orbit of radius r is t. the period of another satellite of earth in a circular orbit of radius 4r is
ishu146:
so what's yr question
I don't understand
you have to solve the answer.. which one of these is correct? 1) √2GM/R 2) √2GM/r-r 3) √2GM(R-R) 4)Zero
sorry I can't do this
that's okay! thanks
wlc
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according to Kepler's law T is proportional to r^(3/2)
T1/T2= (r1/r2)^3/2
T2= 8 T1
Therfore answer is 8t
T1/T2= (r1/r2)^3/2
T2= 8 T1
Therfore answer is 8t
thanks you so much
my pleasure :)
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