A gravitational field is a region of space surrounding a body that has the property of mass. Sir Isaac Newton, in 1666, propounded the universal law of gravitation.
The law states that, ” the force of attraction between two given particles of masses M and m is directly proportional to the product of the masses and inversely proportional to the square of their distance of separation”.
Mathematically,
Fg∝MmandFg∝1r2∴Fg∝Mmr2
∴Fg=GMmr2 ——-(1)
Hence, G=Fgr2Mm
Where Fg is the gravitational force in Newton,N,
Gis the universal or gravitational constant of value 6.7 × 10-11 and expressed in Nm2/kg2
The gravitational field strength, also called acceleration due to gravity, ‘g’ is given by:
g=Fgm ——-(2)
But Fg=GMmr2∴g=GMmr2÷m=GMmr2×1m
Hence, g=GMr2 ——-(3)
This is the relationship between gravitational constant G and acceleration due to gravity g.
Therefore, we define gravitational field strength ‘g’ as force per unit mass. It is a vector quantity.
Gravitational Potential Vg
The gravitational potential Vg at a point is the work done in taking a unit mass from infinity to that point on the surface of the earth.
Vg=gr ——-(4)
Vg=GMr2×r
∴ Vg=GMr ——-(5)
Where M is the mass of the earth and r is the radius of the earth of value 6.4 × 106m or 6400km
At any point, distance r from the centre of the earth, the gravitational potential experienced by a body of mass m is given by:
∴Vg=−Gmr ——-(6)
Since the potential at infinity is taken to be zero. (i.e, ∆potential =0−Vg=−Vg=−Gmr
The negative sign indicates that potential at infinity is higher than the potential close to the mass, that is, Vg decreases as r increases.
Escape Velocity V0
Consider a rocket of mass m placed at the centre of the earth’s surface O. If it is fired from that point so that it just escapes the earth’s gravitational field, it has a kinetic energy, k.e given as:
k.e=12mV20 ——-(7)
But work is done(WD) in taking this rocket to a distance R so great that the gravitational field is negligibly weak.
∴ Work done =mg×distance
This work done must be equal to the kinetic energy of the rocket at the point of take off
Work done =12mV20
∴ Work done =mg×R=mgR
but gravitational intensity g=GMR2
Work done =m(GMR2)R
Work done =GMmR
But k.e = WD
∴12mV20=GMmR∴V20=2GMR
∴ V0=2GMR−−−−√ ——-(8)
But gR=GMR
Hence, V0=2gR−−−−√ ——-(8)
We thus define the escape velocity V0 as the velocity which is sufficient enough for a body to just escape the earth’s gravitational field.
Since g = 9.8m/s2, and R = 6,400,000m
Thus V0=2×9.8×6.4×106−−−−−−−−−−−−−−−√=11,200m/s(40,320km/h)
EVALUATION (POST YOUR ANSWERS USING THE QUESTION BOX BELOW FOR EVALUATION AND DISCUSSION):
Worked Examples
Solution:
F=Gm1m2r2=6.67×10−11×1024×1027(1020)2=6.67N
Solution:
F=Gm1m2r2=6.67×10−11×1.67×10−27×9.11×10−31(10−10)2=1.01×10−47N
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