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// Chapter 11 example 7
//------------------------------------------------------------------------------
clc;
clear;
// Given data
m = 100; // mass of satellite
V = 8000; // orbital velocity in m/s
Re = 6370; // radius of earth in Km
H = 200; // satellite height above earth surface
// Calculations
CF = (m*V^2)/((Re+H)*10^3); //centrifugal force
// output
mprintf('Centrifugal Force = %d Newtons',CF);
//------------------------------------------------------------------------------
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