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2) A satellite of mass m is in circular orbit of radius ro in a potential of the form V(r) --kr-3/2 (a) Use the Viral Theorem

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Answer #1

a) The Viral Theorem indicates the following:

«T>= Σ< F, ή >(1)

Where

< T>: is the average kinetic energy on k particles
vec{F_{k}: is the force of attraction between the particles
vec{r_{k}}:is the radial distance between the particles

In our case, we have one particle, then

T=-*<Ēr> (2)

The radial force exerted on the satellite is expressed as a function of the potential

(1) 4-= (3)

Where

+1+z/5-145 = ZAP = 14 (4)

In magnitude

ا = سنت انا - s/ (5)

but the satellite position vector and the radial force are opposite, therefore when making the dot product between these vectors, the angle is 180 degrees

T=-*<Ēr>

T = Firicos180 (6)

T = \frac{3}{2}kr^{-5/2}r=\frac{3}{2}kr^{-3/2} (7)

Now

T= -01 m (8)

V =

Therefore

3 v=1-kr-2 V 2m

b)The effective potential is defined as the potential due to the radial force, plus the potential due to the centrifugal force, whose force moves the satellite away from the mass that attracts it

Vefs = V(r) +m! (9)

Where:

l: is the angular momentum

Vefp = -kr-3/2+ 2r2

Adding the fractions of the previous equation we have:

Vefs = -2krém12,3/2 2r7/2 (10)

c)

For the realization of the previous graph we assume from equation 10, the following:

l=1

m = 1

k=1

-2r2 + 3/2 Veff = 277/2 (11)

when graphing expression 11, we have:

0 2 4 6 8 10 12 Eeff radius

 
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