kilopascals $[$kPa$].$ Use the following information where $H$ is altitude in meters, $T$ is temperature in $C,$ and $P$ is pressure in kilopascals:

Troposphere: Altitude

$T=15\mathrm{.}04-0\mathrm{.}00649H$

$P=101\mathrm{.}29(\frac{T+273\mathrm{.}1}{288\mathrm{.}08}{)}^{5\mathrm{.}256}$

Lower Stratosphere: Altitude

$T=-56\mathrm{.}46$

$P=22\mathrm{.}65e^{(1\mathrm{.}73-0\mathrm{.}000157H)}$

Upper Stratosphere: Altitude

$T=-131\mathrm{.}21+0\mathrm{.}00299H$

$P=2\mathrm{.}488(\frac{T+273\mathrm{.}1}{216\mathrm{.}6}{)}^{-11\mathrm{.}388}$

These formulae come from the atmosphere model provided by NASA at:

http:$//$www$.$grc$.$nasa.gov$/$WWW$/$K$-12/$airplane$/$atmosmet$.$html$.$

Sample Input$/$Output

Altitude $=500$ meters

An altitude of $500$ is in the troposphere with a temperature of $12$ degrees $C$ and pressure of $96$kPa.