Hello there,
I plan to program some simple software to optimize the start/orbiting of rockets in some optimal way. At the moment it works somehow, but I have some questions:
1) How can I accurately calculate the drag? Can I just use the formula of http://wiki.kerbalspaceprogram.com/wiki/Atmosphere#Drag with an appropriate constant or does the drag also depend on the Mach number (as in reality).
2) Does the specific impulse ISP for a specific rocket engine depend only on the (static) pressure?
3) Which functions of the API can be used to determine the current thrust/drag?
Thanks for your help.
Best wishes
Marcus