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Modeling gurus:
The simulators apply launch site conditions (temp, pressure, latitude, sometimes humidity) to the US Standard Atmosphere model. I am trying to duplicate that, for the troposphere only. I've Googled the hell out of this, and the best I can figure to do is:
1. Compute the standard atmosphere as a function of altitude, using standard sea level T0 = 288.15 K and P0 = 101325 Pa. I am using the hydrostatic equations here:
https://en.wikipedia.org/wiki/Density_of_air
2. Then, simply apply the difference between the launch site T,P and T0, P0 to the results as a constant offset. Use the corrected T,P vs. altitude to then compute density, speed of sound, etc.
With this method, I can duplicate this calculator with the temperature deviation:
https://www.digitaldutch.com/atmoscalc/index.htm
I assume the same would apply to pressure deviation, but I can't find any calculators that do that.
Am I on the right track?
The simulators apply launch site conditions (temp, pressure, latitude, sometimes humidity) to the US Standard Atmosphere model. I am trying to duplicate that, for the troposphere only. I've Googled the hell out of this, and the best I can figure to do is:
1. Compute the standard atmosphere as a function of altitude, using standard sea level T0 = 288.15 K and P0 = 101325 Pa. I am using the hydrostatic equations here:
https://en.wikipedia.org/wiki/Density_of_air
2. Then, simply apply the difference between the launch site T,P and T0, P0 to the results as a constant offset. Use the corrected T,P vs. altitude to then compute density, speed of sound, etc.
With this method, I can duplicate this calculator with the temperature deviation:
https://www.digitaldutch.com/atmoscalc/index.htm
I assume the same would apply to pressure deviation, but I can't find any calculators that do that.
Am I on the right track?