protected void GetThrustData(out double thrustVac, out double thrustASL)
{
rfSolver.SetPropellantStatus(true, true);
bool oldE = EngineIgnited;
bool oldIg = ignited;
float oldThrottle = currentThrottle;
double oldLastPropellantFraction = lastPropellantFraction;
currentThrottle = 1f;
lastPropellantFraction = 1d;
EngineIgnited = true;
ignited = true;
ambientTherm = EngineThermodynamics.StandardConditions(true);
inletTherm = ambientTherm;
rfSolver.UpdateThrustRatio(1d);
rfSolver.SetPropellantStatus(true, true);
UpdateSolver(EngineThermodynamics.StandardConditions(true), 0d, Vector3d.zero, 0d, true, true, false);
thrustASL = engineSolver.GetThrust() * 0.001d;
double spaceHeight = Planetarium.fetch?.Home?.atmosphereDepth + 1000d ?? 141000d;
UpdateSolver(EngineThermodynamics.VacuumConditions(true), spaceHeight, Vector3d.zero, 0d, true, true, false);
thrustVac = engineSolver.GetThrust() * 0.001d;
EngineIgnited = oldE;
ignited = oldIg;
currentThrottle = oldThrottle;
lastPropellantFraction = oldLastPropellantFraction;
}
protected string GetThrustInfo()
{
string output = string.Empty;
if (engineSolver == null || !(engineSolver is SolverRF))
{
CreateEngine();
}
rfSolver.SetPropellantStatus(true, true);
ambientTherm = EngineThermodynamics.StandardConditions(true);
inletTherm = ambientTherm;
currentThrottle = 1f;
lastPropellantFraction = 1d;
bool oldE = EngineIgnited;
EngineIgnited = true;
bool oldIg = ignited;
ignited = true;
rfSolver.UpdateThrustRatio(1d);
rfSolver.SetPropellantStatus(true, true);
UpdateSolver(ambientTherm, 0d, Vector3d.zero, 0d, true, true, false);
double thrustASL = (engineSolver.GetThrust() * 0.001d);
var weight = part.mass * (Planetarium.fetch?.Home?.GeeASL * 9.80665 ?? 9.80665);
if (atmChangeFlow) // If it's a jet
{
if (throttleLocked || minThrottle == 1f)
{
output += String.Format("<b> Static Thrust: </b>{0} (TWR {1}), {2}\n", Utilities.FormatThrust(thrustASL), (thrustASL / weight).ToString("0.0##"), (throttleLocked ? "throttle locked" : "unthrottleable"));
}
else
{
output += String.Format("{0}% min throttle\n", (minThrottle * 100f).ToString("N0"));
output += String.Format("<b>Max. Static Thrust: </b>{0} (TWR {1})\n", Utilities.FormatThrust(thrustASL), (thrustASL / weight).ToString("0.0##"));
output += String.Format("<b>Min. Static Thrust: </b>{0} (TWR {1})\n", Utilities.FormatThrust(thrustASL * minThrottle), (thrustASL * minThrottle / weight).ToString("0.0##"));
}
if (useVelCurve) // if thrust changes with mach
{
float vMin, vMax, tMin, tMax;
velCurve.FindMinMaxValue(out vMin, out vMax, out tMin, out tMax); // get the max mult, and thus report maximum thrust possible.
output += String.Format("<b>Max. Thrust: </b>{0} at Mach {1} (TWR {2})\n", Utilities.FormatThrust(thrustASL * vMax), tMax.ToString("0.#"), (thrustASL * vMax / weight).ToString("0.0##"));
}
}
else
{
// get stats again
ambientTherm = EngineThermodynamics.VacuumConditions(true);
double spaceHeight = Planetarium.fetch?.Home?.atmosphereDepth + 1000d ?? 141000d;
UpdateSolver(ambientTherm, spaceHeight, Vector3d.zero, 0d, true, true, false);
double thrustVac = (engineSolver.GetThrust() * 0.001d);
if (throttleLocked || minThrottle == 1f)
{
var suffix = throttleLocked ? "throttle locked" : "unthrottleable";
if (thrustASL != thrustVac)
{
output += String.Format("<b>Thrust (Vac): </b>{0} (TWR {1}), {2}\n", Utilities.FormatThrust(thrustVac), (thrustVac / weight).ToString("0.0##"), suffix);
output += String.Format("<b>Thrust (ASL): </b>{0} (TWR {1}), {2}\n", Utilities.FormatThrust(thrustASL), (thrustASL / weight).ToString("0.0##"), suffix);
}
else
{
output += String.Format("<b>Thrust: </b>{0} (TWR {1}), {2}\n", Utilities.FormatThrust(thrustVac), (thrustVac / weight).ToString("0.0##"), suffix);
}
}
else
{
output += String.Format("{0}% min throttle\n", (minThrottle * 100f).ToString("N0"));
if (thrustASL != thrustVac)
{
output += String.Format("<b>Max. Thrust (Vac): </b>{0} (TWR {1})\n", Utilities.FormatThrust(thrustVac), (thrustVac / weight).ToString("0.0##"));
output += String.Format("<b>Max. Thrust (ASL): </b>{0} (TWR {1})\n", Utilities.FormatThrust(thrustASL), (thrustASL / weight).ToString("0.0##"));
output += String.Format("<b>Min. Thrust (Vac): </b>{0} (TWR {1})\n", Utilities.FormatThrust(thrustVac * minThrottle), (thrustVac * minThrottle / weight).ToString("0.0##"));
output += String.Format("<b>Min. Thrust (ASL): </b>{0} (TWR {1})\n", Utilities.FormatThrust(thrustASL * minThrottle), (thrustASL * minThrottle / weight).ToString("0.0##"));
}
else
{
output += String.Format("<b>Max. Thrust: </b>{0} (TWR {1})\n", Utilities.FormatThrust(thrustVac), (thrustVac / weight).ToString("0.0##"));
output += String.Format("<b>Min. Thrust: </b>{0} (TWR {1})\n", Utilities.FormatThrust(thrustVac * minThrottle), (thrustVac * minThrottle / weight).ToString("0.0##"));
}
}
}
EngineIgnited = oldE;
ignited = oldIg;
return(output);
}
protected string GetThrustInfo()
{
string output = string.Empty;
if (engineSolver == null || !(engineSolver is SolverRF))
{
CreateEngine();
}
rfSolver.SetPropellantStatus(true, true);
ambientTherm = EngineThermodynamics.StandardConditions(true);
inletTherm = ambientTherm;
currentThrottle = 1f;
lastPropellantFraction = 1d;
bool oldE = EngineIgnited;
EngineIgnited = true;
bool oldIg = ignited;
ignited = true;
rfSolver.UpdateThrustRatio(1d);
rfSolver.SetPropellantStatus(true, true);
UpdateSolver(ambientTherm, 0d, Vector3d.zero, 0d, true, true, false);
double thrustASL = (engineSolver.GetThrust() * 0.001d);
if (atmChangeFlow) // If it's a jet
{
output += "<b>Static Thrust: </b>" + (thrustASL).ToString("0.0##") + " kN" + ThrottleString();
if (useVelCurve) // if thrust changes with mach
{
float vMin, vMax, tMin, tMax;
velCurve.FindMinMaxValue(out vMin, out vMax, out tMin, out tMax); // get the max mult, and thus report maximum thrust possible.
output += "\n<b>Max. Thrust: </b>" + (thrustASL * vMax).ToString("0.0##") + " kN Mach " + tMax.ToString("0.#");
}
}
else
{
// get stats again
ambientTherm = EngineThermodynamics.VacuumConditions(true);
double spaceHeight = Planetarium.fetch?.Home?.atmosphereDepth + 1000d ?? 141000d;
UpdateSolver(ambientTherm, spaceHeight, Vector3d.zero, 0d, true, true, false);
double thrustVac = (engineSolver.GetThrust() * 0.001d);
if (thrustASL != thrustVac)
{
output += (throttleLocked ? "<b>" : "<b>Max. ") + "Thrust (Vac.): </b>" + (thrustVac).ToString("0.0##") + " kN" + ThrottleString()
+ "\n" + (throttleLocked ? "<b>" : "<b>Max. ") + "Thrust (ASL): </b>" + (thrustASL).ToString("0.0##") + " kN";
}
else
{
output += (throttleLocked ? "<b>" : "<b>Max. ") + "Thrust: </b>" + (thrustVac).ToString("0.0##") + " kN" + ThrottleString();
}
}
output += "\n";
EngineIgnited = oldE;
ignited = oldIg;
return(output);
}