Hello,

I've been having an issue with modelling the C* of a propellant with a large amount of condensed flow, when I input the numbers from the combustion simulator (AFCESIC) I find that the C* is lower by about 10. In static testing, the C* was found to be closer to the AFCESIC numbers, so I've started just futzing with the combustion temperature number to make the C* match.

It would be nice to be able to input C* instead of the variables required to derive it, as the basic equations for C* seem to exclude things that more advanced sims don't