RPAEngineData.cfg

version = 1.2;
name = "EngineDataGatherer";
info = "Settings used for gathering engine data";
generalOptions : 
{
  multiphase = true;
  ions = true;
  flowSeparation = true;
};
combustionChamberConditions : 
{
  pressure : 
  {
    value = 2.0;
    unit = "MPa";
  };
};
nozzleFlow : 
{
  calculateNozzleFlow = true;
  nozzleExitConditions : 
  {
    areaRatio = 1.3;
    supersonic = true;
  };
  nozzleStations = ( );
};
propellant : 
{
  components : 
  {
    ratio : 
    {
      value = 2.1;
      unit = "O/F";
    };
    oxidizer = ( 
      {
        name = "O2(L)";
        massFraction = 1.0;
        p : 
        {
          value = 0.0;
          unit = "MPa";
        };
      } );
    fuel = ( 
      {
        name = "RP-1";
        massFraction = 1.0;
        p : 
        {
          value = 0.0;
          unit = "MPa";
        };
      } );
  };
};
engineSize : 
{
  chambersNo = 1;
};
propelantFeedSystem : 
{
  estimateDryMass = false;
};