Answer to Question #26253 in Mechanics | Relativity for zameer
circular orbit at a height of 250 km from the earth’s surface, where the acceleration due to earth’s
gravity is 0.93 g. Calculate the period of its orbit. Take g = 9.8 ms−2 and the radius of the earth
R = 6.37 × 106m.
F=ma, F - force of gravity, m - satellite's mass, a - acceleration of satellite.
According to the problem statement, F=mg1 and g1=0.93g, so F=0.93mg
Satellite moves in a circle with a constant angular velocity around the Earth, so a=w^2*(R+r) where w - angular velocity, R - radius of the Earth, r - height of satellite's orbit.
The result if:
It's obvious that w=2pi/T, so
T=2*3.14*sqrt((6.37*10^6+0.25*10^6)/(0.93*9.8))=5.355*10^3(s)=1 hour 29 minutes and 15 seconds
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