MAP = Atmosphere->GetPressure() * 47.88; // psf to Pa
CylinderHeadTemp_degK = 0.0;
Displacement = 360;
- MaxHP = 200;
+ MaxHP = 0;
Cycles = 2;
IdleRPM = 600;
Magnetos = 0;
buf << Name << "_PwrAvail[" << EngineNumber << "]" << delimeter
<< Name << "_HP[" << EngineNumber << "]" << delimeter
+ << Name << "_equiv_ratio[" << EngineNumber << "]" << delimeter
+ << Name << "_MAP[" << EngineNumber << "]" << delimeter
<< Thruster->GetThrusterLabels(EngineNumber, delimeter);
return buf.str();
std::ostringstream buf;
buf << PowerAvailable << delimeter << HP << delimeter
+ << equivalence_ratio << delimeter << MAP << delimeter
<< Thruster->GetThrusterValues(EngineNumber, delimeter);
return buf.str();