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A research satellite of mass 200 kg circles the earth in an 3R orbit of average radiuswhere R is the radius of earth. Assuming the gravitational pull on a mass of 1 kg on the earth's surface to be 10 N, the pull on the satellite will be (a) 880 N (c) 885 N (b) 889 N (d) 892 N

User Oscfri
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1 Answer

4 votes

Answer: (b) 889N

The given options do not match with the given data. However, working with an orbit of radius 3R/2 the answer is 889N.

Step-by-step explanation:

According to Newton's law of Gravitation, the force
F exerted between two bodies of masses
M and
m and separated by a distance
R is equal to the product of their masses and inversely proportional to the square of the distance:


F=G(Mm)/(R^2)

Where
Gis the gravitational constant,
M is the mass of the Earth in this case

.

If we are told the gravitational pull on a mass of
m_(1)=1 kgon the earth's surface to be 10 N, this means the force at the surface is:


F=10N=G(Mm)/(R^2) (1)

Assuming the mass of the Earth and its radius constant that we will name
g, we can say:


G(M)/(R^2)=g (2)

Then:


10N=g.m_(1)=g.(1kg) (3)

Finding
g:


g=(10N)/(1kg)=10m/s^2 (4)

Now, the gravitational pull at a certain height
h over the surface is:


F_(h)=G\frac{Mm_(2)}{{(R+h)}^2} (5)

Where
m_(2) is the mass of the satellite.

If we are told the radius of the orbit of the research satellite is
3R/2, this means
R+h=3R/2:


F_(h)=G\frac{Mm_(2)}{{(3R/2)}^2}=G(M)/(R^2).(4m_(2))/(9) (7)

Substituting (4) in (7):


F_(h)=g(4m_(2))/(9) (8)

Knowing the mass of the research satellite is 200kg:


F_(h)=10m/s^2((4)(200kg))/(9) (9)

Finally:


F_(h)=888.888N\approx 889N This is the gravitational pull on the satellite with an orbit of radius 3R/2

User Piotr Kalinowski
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