thanks for your help.
i'll give you a bit more background to the problem.
i am actually trying to calculate the surface pressure of a vehicle that has been shot up in a rocket and detaches. it reaches a height of 300km and begins its descent. i have already modeled its velocity with python...
hi I'm new here and i need some help regarding atmospheric pressures.
i have a way of calculating it up until about 50 km above sea level.
is there a way to accurately model the pressure at an altitude up to 300km?