Mass of the earth = M = 5.98 x 1024 kg.
Mass of the satellite = m = 1900 kg.
Distance of the orbit from the center of the earth = R
= Radius of the earth Ro + Height of the orbit
= 6.37 x 106 m + 800 km = 6.37 x 106 m + 8 x 105 m = 7.17 x 106 m.
Hence, work done required to move the satellite from a distance r to ( r + dr ) is dW = F . dr,
where, gravitational force = F = GMm / r2, at a distance r from the center of the earth.
So, total work done to move the satellite from the surface of the earth to R is :
W = dW. This integration is calculated below :
So, plugging the known values in the above equation :
W = 6.67 x 10-11 x 5.98 x 1024 x 1900 { 1 / ( 6.37 x 106 ) - 1 / ( 7.17 x 106 ) } J
or, W = 1.33 x 1010 J.
Newton's Law of Gravitation states that two bodies with masses my and m2 attract each other...
Learning Goal: To understand Newton's law of gravitation and the distinction between inertial and gravitational masses. In this problem, you will practice using Newton's law of gravitation. According to that law, the magnitude of the gravitational force Fg between two small particles of masses m1 and m2 separated by a distance r, is given by m1m2 T2 where G is the universal gravitational constant, whose numerical value (in SI units) is 6.67 x 10-11 Nm2 kg2 This formula applies not...