A particle moves in a horizontal circle of radius \(r\) with constant speed \(v\). Derive an expression for the centripetal force in terms of mass \(m\), \(v\) and \(r\). A satellite of mass \(250\,\mathrm{kg}\) orbits the Earth at a height of \(400\,\mathrm{km}\) above the surface. Radius of Earth \(= 6400\,\mathrm{km}\), \(g=9.8\,\mathrm{m\,s}^{-2}\) at surface. Calculate the orbital speed assuming \(g\) varies as \(1/r^{2}\).
Acceleration \(a = v^{2}/r\) (from \(a = \omega^{2}r\) or geometry of velocity change). Force \(F = ma = mv^{2}/r\).
Orbital radius \(r = 6800\,\mathrm{km} = 6.80\times10^{6}\,\mathrm{m}\).
\(g(r) = g_{0}(R/r)^{2} = 9.8\times(6400/6800)^{2} = 8.68\,\mathrm{m\,s}^{-2}\).
\(v = \sqrt{gr} = \sqrt{8.68\times6.80\times10^{6}} = 7680\,\mathrm{m\,s}^{-1}\).