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ZachWeiner
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Hey, does anyone have an equation that roughly models atmospheric density from sea level to about 200 km up?
aniketp said:Hi ZachWeiner,
Pressure at a height "h" is given by :
P=(Patm)*e^(-Mgh/RT) [Patm is the pressure at sea level]
And D=PM/RT
But there is an assumption that T is const. this formula will only enable you to calculate the density roughly. So do not use it if you want accurate answers.
Atmospheric density is the measure of the mass of air particles per unit volume in Earth's atmosphere. It is affected by factors such as altitude, temperature, and air pressure.
The equation used to model atmospheric density from sea level to 200km is called the Barometric formula. It takes into account the variation in air pressure with altitude and is based on the ideal gas law.
Studying atmospheric density is important for understanding the behavior of Earth's atmosphere and how it affects weather patterns and climate change. It also has practical applications in fields such as aviation and space exploration.
As altitude increases, atmospheric density decreases. This is because there is less air above, causing lower air pressure and therefore fewer air particles per unit volume.
200km is the approximate boundary between Earth's atmosphere and outer space. The atmospheric density at this altitude is very low, making it an important point of reference for understanding the behavior of Earth's atmosphere.