Putting a Satellite into Orbit The strength of Earth's gravitational field
varies with the distance \(r\) from Earth's center, and the magnitude of the
gravitational force experienced by a satellite of mass \(m\) during and after
launch is
$$F(r)=\frac{m M G}{r^{2}}$$
Here, \(M=5.975 \times 10^{24} \mathrm{kg}\) is Earth's mass, \(G=6.6726 \times
10^{-11} \mathrm{N} \cdot \mathrm{m}^{2} \mathrm{kg}^{-2}\) is the universal
gravitational constant, and \(r\) is measured in meters. The work it takes to
lift a 1000 -kg satellite from Earth's surface to a circular orbit \(35,780
\mathrm{km}\) above Earth's center is therefore given by the integral
Work $$=\int_{6,370,000}^{35.780,000} \frac{1000 M G}{r^{2}} d r$$ joules.
The lower limit of integration is Earth's radius in meters at the launch site.
Evaluate the integral. (This calculation does not take into account energy
spent lifting the launch vehicle or energy spent bringing the satellite to
orbit velocity.)