Recent content by s4177112

thank you very much. it is exactly what i needed.

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?