Newtons Laws EX 36

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The shuttle was placed into a circular orbit of radius r=(6.37×106)+(3.15×105)=6.685×106 while the satellite was in the orbit of radius r=(6.37×106)+(3.60×105)=6.73×106. The shuttle was initially on the opposite side of the satellite and we want to know how long will it take to be beneath the satellite. We need to find the period for both of these satellites. To get this we will use the formula for the velocity.

v=2πrT

Substitute the formula for the velocity into the expression for the Newton's second law:

GMEMSr2=MSv2r

GMEMSr2=MS(2πrT)2r

GMEr3=4π2T2

(6.67×1011)(6×1024)(6.685×106)3=4π2T2

and find the period of the shuttle to be 5458s.

Similarly, for Westar, we obtain the equation

(6.67×1011)(6×1024)(6.73×106)3=4π2T2

and solve it to find the period of the Westar to be 5499s.

Since at the beginning the two satellites were on the opposite side of the Earth, the shuttle has to make more revolutions than the satellite. Let's assume that in some time Δt the shuttle is beneath the satellite. Given the period of the shuttle (5458s), we deduce that the number of revolutions made by the shuttle is given by

N=ΔtT=Δt5458

It has moved through an angle of

ΔθS=2πN=2π(Δt5458)

During the same time the Westar moved through an angle

ΔθW=2π(Δt5499)

The shuttle needs to "catch up" with Westar. Therefore, the angle ΔθS is larger than ΔθW. Since they were initially on the opposite side of Earth:

ΔθS=ΔθW+π

or

2π(Δt5458)=2π(Δt5499)+π

Solving for Δt we find Δt=3.66×105s.