public override void CreateEngine()
{
engineSolver = new SolverRF();
if (!useAtmCurve)
{
atmCurve = null;
}
if (!useVelCurve)
{
velCurve = null;
}
if (!useThrustCurve)
{
thrustCurve = null;
}
// FIXME quick temp hax
if (useAtmCurve)
{
if (maxEngineTemp == 0)
{
maxEngineTemp = 2000d;
}
if (chamberNominalTemp == 0)
{
chamberNominalTemp = 950d;
}
}
else
{
if (maxEngineTemp == 0)
{
maxEngineTemp = 3600d;
}
if (chamberNominalTemp == 0)
{
chamberNominalTemp = 3500d;
}
}
(engineSolver as SolverRF).InitializeOverallEngineData(
minFuelFlow,
maxFuelFlow,
atmosphereCurve,
atmCurve,
velCurve,
throttleResponseRate,
chamberNominalTemp,
machLimit,
machHeatMult);
}
public override void CreateEngine()
{
rfSolver = new SolverRF();
if(!useAtmCurve)
atmCurve = null;
if(!useVelCurve)
velCurve = null;
if (!useThrustCurve)
thrustCurve = null;
// FIXME quick temp hax
if (useAtmCurve)
{
if (maxEngineTemp == 0d)
maxEngineTemp = 2000d;
if (chamberNominalTemp == 0d)
chamberNominalTemp = 950d;
}
else
{
if (maxEngineTemp == 0d)
maxEngineTemp = 3600d;
if (chamberNominalTemp == 0d)
chamberNominalTemp = 3400d;
if (tempGaugeMin == 0.8d)
tempGaugeMin = 0.95d;
}
double thrustVariation = varyThrust * RFSettings.Instance.varyThrust;
chamberNominalTemp *= (1d - thrustVariation);
rfSolver.InitializeOverallEngineData(
minFuelFlow,
maxFuelFlow,
atmosphereCurve,
atmCurve,
velCurve,
throttleResponseRate,
chamberNominalTemp,
machLimit,
machHeatMult,
flowMultMin,
flowMultCap,
flowMultCapSharpness,
multFlow,
thrustVariation,
(float)part.name.GetHashCode());
rfSolver.SetScale(scale);
engineSolver = rfSolver;
}
public override void CreateEngine()
{
rfSolver = new SolverRF();
if (!useAtmCurve)
{
atmCurve = null;
}
if (!useVelCurve)
{
velCurve = null;
}
// FIXME quick temp hax
if (useAtmCurve)
{
if (maxEngineTemp == 0d)
{
maxEngineTemp = 2000d;
}
if (chamberNominalTemp == 0d)
{
chamberNominalTemp = 950d;
}
}
else
{
if (maxEngineTemp == 0d)
{
maxEngineTemp = 3600d;
}
if (chamberNominalTemp == 0d)
{
chamberNominalTemp = 3400d;
}
if (tempGaugeMin == 0.8d)
{
tempGaugeMin = 0.95d;
}
}
double thrustVariation = varyThrust * RFSettings.Instance.varyThrust;
chamberNominalTemp *= (1d - thrustVariation);
rfSolver.InitializeOverallEngineData(
minFuelFlow,
maxFuelFlow,
atmosphereCurve,
useAtmCurve ? atmCurve : null,
useVelCurve ? velCurve : null,
useAtmCurveIsp ? atmCurveIsp : null,
useVelCurveIsp ? velCurveIsp : null,
disableUnderwater,
throttleResponseRate,
chamberNominalTemp,
machLimit,
machHeatMult,
flowMultMin,
flowMultCap,
flowMultCapSharpness,
thrustVariation,
(float)part.name.GetHashCode());
rfSolver.SetScale(scale);
engineSolver = rfSolver;
}
protected bool started = false; // Track start state, don't handle MEC notification before first start.
#endregion
#region Overrides
public override void CreateEngine()
{
rfSolver = new SolverRF();
if (!useAtmCurve)
{
atmCurve = null;
}
if (!useVelCurve)
{
velCurve = null;
}
// FIXME quick temp hax
if (useAtmCurve)
{
if (maxEngineTemp == 0d)
{
maxEngineTemp = 2000d;
}
if (chamberNominalTemp == 0d)
{
chamberNominalTemp = 950d;
}
}
else
{
if (maxEngineTemp == 0d)
{
maxEngineTemp = 3600d;
}
if (chamberNominalTemp == 0d)
{
chamberNominalTemp = 3400d;
}
if (tempGaugeMin == 0.8d)
{
tempGaugeMin = 0.95d;
}
}
double totalVariation = (1d + localVaryFlow) * (1d + localVaryIsp) - 1d;
chamberNominalTemp *= (1d - totalVariation);
rfSolver.InitializeOverallEngineData(
minFuelFlow,
maxFuelFlow,
atmosphereCurve,
useAtmCurve ? atmCurve : null,
useVelCurve ? velCurve : null,
useAtmCurveIsp ? atmCurveIsp : null,
useVelCurveIsp ? velCurveIsp : null,
disableUnderwater,
throttleResponseRate,
chamberNominalTemp,
machLimit,
machHeatMult,
flowMultMin,
flowMultCap,
flowMultCapSharpness,
localVaryFlow,
localVaryIsp,
localVaryMixture,
isSolid,
partSeed);
rfSolver.SetScale(scale);
engineSolver = rfSolver;
}
