Input interpretation
![hypsometric equation](../image_source/9bb1a59fcadbc8b90c4e2430f826bf8a.png)
hypsometric equation
Equation
![P_2 = P_r exp(-(g (H_2 - H_r))/(287.003 T_r)) | P_2 | final pressure P_r | reference pressure T_r | reference temperature H_r | reference altitude H_2 | altitude g | standard acceleration due to gravity on the surface of the earth (≈ 9.807 m/s^2) (only valid if temperature constant between altitude levels)](../image_source/cdd1540da9f97456391cc3a6e736a1dc.png)
P_2 = P_r exp(-(g (H_2 - H_r))/(287.003 T_r)) | P_2 | final pressure P_r | reference pressure T_r | reference temperature H_r | reference altitude H_2 | altitude g | standard acceleration due to gravity on the surface of the earth (≈ 9.807 m/s^2) (only valid if temperature constant between altitude levels)
Units
Input values
![reference pressure | 0.5 atm (atmospheres) reference temperature | 220 K (kelvins) reference altitude | 5 km (kilometers) altitude | 20 km (kilometers)](../image_source/b71181c7002e97b567008506563d571d.png)
reference pressure | 0.5 atm (atmospheres) reference temperature | 220 K (kelvins) reference altitude | 5 km (kilometers) altitude | 20 km (kilometers)
Result
![final pressure | 48.66 matm (milliatmospheres) = 4.931 kPa (kilopascals) = 4931 Pa (pascals) = 0.7151 psi (pounds-force per square inch) = 103 lbf/ft^2 (pounds-force per square foot) = 0.04866 atm (atmospheres) = 36.98 mmHg (millimeters of mercury) = 49.31 mbar (millibars)](../image_source/a94af95b165583b4aa106db038f8d690.png)
final pressure | 48.66 matm (milliatmospheres) = 4.931 kPa (kilopascals) = 4931 Pa (pascals) = 0.7151 psi (pounds-force per square inch) = 103 lbf/ft^2 (pounds-force per square foot) = 0.04866 atm (atmospheres) = 36.98 mmHg (millimeters of mercury) = 49.31 mbar (millibars)