My main requirements:
- Calculate propeller thrust with big range of the altitudes (0 - 200 km) or to have air pressure input parameter, which I can type. For example pressure for 152 km is $4.98\times10^{-7} kPa$ as mentioned here.
- Calculate required power.
- Calculation can be done for static case, like helicopter which is staying on the ground or moving up very slowly like 1 m/s.
I found this one which is good enough for me, but I am not sure if it is doing good calculations for high altitude (50-100km) and I can trust it. Below is the screenshot from it. I would be more confident, if I would be able to type air pressure, but not altitude.
P.S. I do not want to dispute if it make sense or no to use propeller at high altitudes. I just want to know if there is software which can do this calculation. I will do calculation and based on the calculation will decide if it make sense or not. Please do not put comments about propeller inefficiency at high altitude.
