v1.0 must do the following as a Matlab script:

• Accept a nozzle profile and predict M, P, and T over the profile for quasi-1D flow
• Determine whether the flow contains normal shocks and the location of such shocks
• Plot these parameters versus the x-axis, including the shock cases.
• Output critical and exit parameters for M, P, T, mdot
• Predict and output thrust and specific impulse
• Match known validation cases

v1.0 may not, but future versions should:

• Work on multiple platforms
• Have a GUI
• Handle cases other than non-reacting, homogeneous gas propellants without heat addition
• Predict performance 2D by the method of characteristics
• Take performance losses due to geometry or assumptions into account