A satellite of mass M is revolving around the earth at a height R (R=radius of the earth ). If get is the gravitational field intensity,the kinetic energy of the satellite is

4 views

3 Answers

what is "get" in question?

4 views

TE = GMm/2(R+h) = -GMm/2(R+h) R2/R2 = g0mR2/2(R+h)

4 views

I will go with option (C)

Taking m = mass of satellite

M = mass of earth

g = gravitational field intensity

G = Gravitational constant

v = velocity of satellite at height R from surface of the earth, where R = radius of earth

here GM= gR^2

Here centripetal force = gravitational pull

=> (mv^2)/(2R) = (GMm)/(2R)^2

=> (1/2 mv^2) /R = (gR^2m)/(4R^2)= mg/4

=> KE = mgR/4

4 views