protected string GetThrustInfo()
{
string output = "";
if (engineSolver == null || !(engineSolver is SolverRF))
{
CreateEngine();
}
rfSolver.SetPropellantStatus(true, true);
// get stats
double pressure = 101.325d, temperature = 288.15d, density = 1.225d;
if (Planetarium.fetch != null)
{
CelestialBody home = Planetarium.fetch.Home;
if (home != null)
{
pressure = home.GetPressure(0d);
temperature = home.GetTemperature(0d);
density = home.GetDensity(pressure, temperature);
}
}
ambientTherm = new EngineThermodynamics();
ambientTherm.FromAmbientConditions(pressure, temperature, density);
inletTherm = new EngineThermodynamics();
inletTherm.CopyFrom(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
double spaceHeight = 131000d;
pressure = 0d;
density = 0d;
if (Planetarium.fetch != null)
{
CelestialBody home = Planetarium.fetch.Home;
if (home != null)
{
temperature = home.GetTemperature(home.atmosphereDepth + 1d);
spaceHeight = home.atmosphereDepth + 1000d;
}
}
else
{
temperature = PhysicsGlobals.SpaceTemperature;
}
ambientTherm.FromAmbientConditions(pressure, temperature, density);
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);
}
protected new string GetThrustInfo()
{
string output = "";
if (engineSolver == null || !(engineSolver is SolverRF))
CreateEngine();
(engineSolver as SolverRF).SetEngineStatus(true, true, true);
// get stats
double pressure = 101.325d, temperature = 288.15d, density = 1.225d;
if (Planetarium.fetch != null)
{
CelestialBody home = Planetarium.fetch.Home;
if (home != null)
{
pressure = home.GetPressure(0d);
temperature = home.GetTemperature(0d);
density = home.GetDensity(pressure, temperature);
}
}
ambientTherm = new EngineThermodynamics();
ambientTherm.FromAmbientConditions(pressure, temperature, density);
inletTherm = new EngineThermodynamics();
inletTherm.CopyFrom(ambientTherm);
currentThrottle = 1f;
lastPropellantFraction = 1d;
bool oldE = EngineIgnited;
EngineIgnited = true;
(engineSolver as SolverRF).UpdateThrustRatio(1d);
UpdateFlightCondition(ambientTherm, 0d, Vector3d.zero, 0d, true);
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
double spaceHeight = 131000d;
pressure = 0d;
density = 0d;
if (Planetarium.fetch != null)
{
CelestialBody home = Planetarium.fetch.Home;
if (home != null)
{
temperature = home.GetTemperature(home.atmosphereDepth + 1d);
spaceHeight = home.atmosphereDepth + 1000d;
}
}
else
temperature = PhysicsGlobals.SpaceTemperature;
ambientTherm.FromAmbientConditions(pressure, temperature, density);
UpdateFlightCondition(ambientTherm, spaceHeight, Vector3d.zero, 0d, true);
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;
return output;
}