The Earth atmosphere is a very dynamic environment depending upon many variables such as location, time, weather conditions, etc. The International Standard Atmosphere $($ISA$)$ is a mathematically defined quantity based on actual measurements. Measurements indicate that the atmospheric properties are strongly dependent upon the altitude. The forces acting on a flying vehicle such as aircraft and rockets depend the Earth Atmosphere $($basically the air density$),$ and it is important for aerospace engineers to understand the ISA.

$\backslash$table$[[$Altitude$,$Density,Temperature,Pressure,Speed of Sound$],[0,,,,],[500,,,,],[1000,,,,],[...,,,,],[...,,,,],[59500,,,,]]$

Using a spreadsheet, make the International Standard Atmospheric $($ISA$)$ table as follows $($altitude increment of $500$ meters up to $59,500$ meters $),$ and draw graphs of $($i$)$Altitude $($y$-$axis$)$ vs$.$ Density $($x$-$ axis$),($ii$)$ Altitude vs$.$ Temperature, $($iii$)$ Altitude vs$.$ Pressure