version = 1.1;
name = "Peregrine hybrid propulsion";
info = "Hybrid engine for Peregrine Sounding Rocket";
generalOptions : 
{
  multiphase = true;
  ions = true;
  flowSeparation = true;
};
combustionChamberConditions : 
{
  pressure : 
  {
    value = 700.0;
    unit = "psi";
  };
};
nozzleFlow : 
{
  calculateNozzleFlow = true;
  nozzleInletConditions : 
  {
    contractionAreaRatio = 7.25;
  };
  nozzleExitConditions : 
  {
    areaRatio = 8.4;
  };
};
propellant : 
{
  components : 
  {
    ratio : 
    {
      value = 4.0654;
      unit = "O/F";
    };
    oxidizer = ( 
      {
        name = "N2O(L),184.67K";
        massFraction = 1.0;
        p : 
        {
          value = 0.0;
          unit = "MPa";
        };
      } );
    fuel = ( 
      {
        name = "C32H66(a)";
        massFraction = 1.0;
        p : 
        {
          value = 0.0;
          unit = "MPa";
        };
      } );
  };
};
engineSize : 
{
  thrust : 
  {
    value = 14034.0;
    unit = "lbf";
  };
  ambientConditions : 
  {
    value = 1.0;
    unit = "atm";
  };
  chambersNo = 1;
};