Use the script shown as a starting point. Be sure to include iterative equations.

Required information The pressure and temperature of the atmosphere change constantly based on a number of factors including altitude, latitude/longitude, time of day, and season. To take all these variations into account when considering the design and performance of flight vehicles is impractical. Therefore, a standard atmosphere is frequently used to provide engineers and scientists with a common reference for their research and development. The International Standard Atmosphere is one such model of how conditions of the earth's atmosphere change over a wide range of altitudes or elevations. The following table shows the values of temperature and pressure at selected altitudes. Layer Index, i Layer Name Base Geopotential Altitude Above MSL, h (km) Lapse Rate (C/km) Base Temperature T("C) Base Pressure. p (Pa) 1 O -6.5 15 2. 11 O 3. 20 1 2.8 4 Troposphere Troposphere Stratosphere Stratosphere Stratosphere Mesosphere Mesosphere Mesospause -56.5 -56.5 _-44.5 -2.5 -2.5 -58.5 101325 22632 5474.9 868.02 110.91 66.939 3.9564 5 47 O 6 51 -2.8 -2.0 7 71 8 84.852 -86.28 0.3734 The temperature at each altitude can then be computed as T(h) =T; + vi(h - hi) hi