Flameout = false;
}
- return Thruster->Calculate(Cf*maxPC*PctPower*propEff);
+ return Thrust = Thruster->Calculate(Cf*maxPC*PctPower*propEff);
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-string FGRocket::GetEngineLabels(void)
+string FGRocket::GetEngineLabels(string delimeter)
{
std::ostringstream buf;
- buf << Name << "_ChamberPress[" << EngineNumber << "], "
- << Thruster->GetThrusterLabels(EngineNumber);
+ buf << Name << "_ChamberPress[" << EngineNumber << "]" << delimeter
+ << Thruster->GetThrusterLabels(EngineNumber, delimeter);
return buf.str();
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-string FGRocket::GetEngineValues(void)
+string FGRocket::GetEngineValues(string delimeter)
{
std::ostringstream buf;
- buf << PC << ", " << Thruster->GetThrusterValues(EngineNumber);
+ buf << PC << delimeter << Thruster->GetThrusterValues(EngineNumber, delimeter);
return buf.str();
}