public void RetrofitEngine()
{
if (isupgraded || myScience < upgradeCost) { return; } // || !hasScience || myScience < upgradeCost) { return; }
isupgraded = true;
var curEngine = this.part.Modules["ModuleEngines"] as ModuleEngines;
if (curEngine != null) {
ModuleEngines.Propellant prop = new ModuleEngines.Propellant();
//prop.id = PartResourceLibrary.Instance.GetDefinition("VacuumPlasma").id;
//ConfigNode prop_node = new ConfigNode();
//PartResourceLibrary.Instance.GetDefinition("VacuumPlasma").Save(prop_node);
//PartResource part_resource = part.Resources.list[0];
//part_resource.info = PartResourceLibrary.Instance.GetDefinition("VacuumPlasma");
//part_resource.maxAmount = 10;
//part_resource.amount = 10;
ConfigNode node = new ConfigNode("RESOURCE");
node.AddValue("name", "VacuumPlasma");
node.AddValue("maxAmount", 10);
node.AddValue("amount", 10);
part.AddResource(node);
propellants = ElectricEngineController.getPropellants(isupgraded);
fuel_mode = 0;
//curEngine.propellants[1].id = PartResourceLibrary.Instance.GetDefinition("VacuumPlasma").id;
//curEngine.propellants[1].name = PartResourceLibrary.Instance.GetDefinition("VacuumPlasma").name;
engineType = upgradedName;
part.RequestResource("Science", upgradeCost);
evaluateMaxThrust();
}
}
public void evaluateMaxThrust()
{
List<Part> vessel_parts = vessel.parts;
total_power_output = 0;
var curEngine = this.part.Modules["ModuleEngines"] as ModuleEngines;
ConfigNode chosenpropellant = propellants[fuel_mode];
ConfigNode[] assprops = chosenpropellant.GetNodes("PROPELLANT");
List<ModuleEngines.Propellant> list_of_propellants = new List<ModuleEngines.Propellant>();
//bool propellant_is_upgrade = false;
for (int i = 0; i < assprops.Length; ++i) {
fuelmode = chosenpropellant.GetValue("guiName");
ispMultiplier = float.Parse(chosenpropellant.GetValue("ispMultiplier"));
//propellant_is_upgrade = bool.Parse(chosenpropellant.GetValue("isUpgraded"));
ModuleEngines.Propellant curprop = new ModuleEngines.Propellant();
curprop.Load(assprops[i]);
if (curprop.drawStackGauge) {
curprop.drawStackGauge = false;
fuel_gauge.SetMessage(curprop.name);
fuel_gauge.SetMsgBgColor(XKCDColors.DarkLime);
fuel_gauge.SetMsgTextColor(XKCDColors.ElectricLime);
fuel_gauge.SetProgressBarColor(XKCDColors.Yellow);
fuel_gauge.SetProgressBarBgColor(XKCDColors.DarkLime);
fuel_gauge.SetValue(0f);
}
list_of_propellants.Add(curprop);
}
total_power_output = getStableResourceSupply(FNResourceManager.FNRESOURCE_MEGAJOULES);
final_thrust_store = thrust_efficiency*2000.0f*total_power_output / (initial_isp * ispMultiplier * 9.81f);
//float thrust_ratio = total_power_output / reference_power;
//final_thrust_store = initial_thrust * thrust_ratio / ispMultiplier;
FloatCurve newISP = new FloatCurve ();
newISP.Add (0, initial_isp * ispMultiplier);
curEngine.atmosphereCurve = newISP;
if (PartResourceLibrary.Instance.GetDefinition(list_of_propellants[0].name) != null) {
curEngine.propellants.Clear();
curEngine.propellants = list_of_propellants;
curEngine.SetupPropellant();
}
List<PartResource> partresources = new List<PartResource>();
part.GetConnectedResources(curEngine.propellants[0].id, partresources);
//if(!isupgraded) {
if (partresources.Count == 0 && fuel_mode != 0) {
TogglePropellant();
}
//}else{
// if(!propellant_is_upgrade) {
//TogglePropellant();
// }
//}
}
public void setupPropellants()
{
ModuleEngines curEngine = (ModuleEngines)this.part.Modules["ModuleEngines"];
ConfigNode chosenpropellant = propellants[fuel_mode];
ConfigNode[] assprops = chosenpropellant.GetNodes("PROPELLANT");
List<ModuleEngines.Propellant> list_of_propellants = new List<ModuleEngines.Propellant>();
//VStackIcon stackicon = new VStackIcon(part);
bool currentpropellant_is_jet = false;
bool currentpropellant_is_electric = false;
//part.stackIcon.RemoveInfo(fuel_gauge);
//part.stackIcon.ClearInfoBoxes();
//part.stackIcon.DisplayInfo().
for (int i = 0; i < assprops.Length; ++i) {
fuelmode = chosenpropellant.GetValue("guiName");
ispMultiplier = float.Parse(chosenpropellant.GetValue("ispMultiplier"));
isLFO = bool.Parse(chosenpropellant.GetValue("isLFO"));
if(chosenpropellant.HasValue("isJet")) {
currentpropellant_is_jet = bool.Parse(chosenpropellant.GetValue("isJet"));
}
ModuleEngines.Propellant curprop = new ModuleEngines.Propellant();
curprop.Load(assprops[i]);
if (curprop.drawStackGauge) {
curprop.drawStackGauge = false;
if (currentpropellant_is_jet) {
print("Atmosphere");
fuel_gauge.SetMessage("Atmosphere");
}else {
fuel_gauge.SetMessage(curprop.name);
}
fuel_gauge.SetMsgBgColor(XKCDColors.DarkLime);
fuel_gauge.SetMsgTextColor(XKCDColors.ElectricLime);
fuel_gauge.SetProgressBarColor(XKCDColors.Yellow);
fuel_gauge.SetProgressBarBgColor(XKCDColors.DarkLime);
fuel_gauge.SetValue(0f);
}
list_of_propellants.Add(curprop);
}
Part[] childParts = this.part.FindChildParts<Part>(true);
PartModuleList childModules;
for (int i = 0; i < childParts.Length; ++i) {
childModules = childParts.ElementAt(i).Modules;
for (int j = 0; j < childModules.Count; ++j) {
PartModule thisModule = childModules.GetModule(j);
var thisModule2 = thisModule as FNReactor;
if (thisModule2 != null) {
FNReactor fnr = (FNReactor)thisModule;
FloatCurve newISP = new FloatCurve();
FloatCurve vCurve = new FloatCurve ();
if (!currentpropellant_is_jet) {
maxISP = (float)Math.Sqrt((double)fnr.getReactorTemp()) * 17*ispMultiplier;
minISP = maxISP * 0.4f;
newISP.Add(0, maxISP, 0, 0);
newISP.Add(1, minISP, 0, 0);
curEngine.useVelocityCurve = false;
curEngine.useEngineResponseTime = false;
}else {
if (thisModule2.getIsNuclear()) {
maxISP = 150;
newISP.Add(0, 100);
newISP.Add(0.3f, 150);
newISP.Add(1, 75);
vCurve.Add(0, 1);
vCurve.Add(400, 0.8f);
vCurve.Add(950, 0.9f);
vCurve.Add (1471, 0);
} else {
maxISP = 2500;
newISP.Add(0, 1200);
newISP.Add(0.3f, 2500);
newISP.Add(1, 800);
vCurve.Add(0, 1);
vCurve.Add(400, 0.8f);
vCurve.Add(1000, 0.9f);
vCurve.Add (2000, 0.5f);
}
curEngine.useVelocityCurve = true;
curEngine.useEngineResponseTime = true;
}
//ModuleEngines curEngine = (ModuleEngines)this.part.Modules["ModuleEngines"];
curEngine.atmosphereCurve = newISP;
curEngine.velocityCurve = vCurve;
assThermalPower = fnr.getReactorThermalPower();
engineMaxThrust = 2000 * assThermalPower / maxISP / 9.81f;
float heat_exchanger_thrust_divisor = 1;
if (radius > fnr.getRadius ()) {
heat_exchanger_thrust_divisor = fnr.getRadius () * fnr.getRadius () / radius / radius;
}else{
heat_exchanger_thrust_divisor = radius * radius / fnr.getRadius () / fnr.getRadius ();
}
engineMaxThrust = engineMaxThrust * heat_exchanger_thrust_divisor;
if (isLFO) {
engineMaxThrust = engineMaxThrust*1.5f;
}
curEngine.maxThrust = engineMaxThrust;
}
}
}
Part parent = this.part.parent;
if (parent != null) {
childModules = parent.Modules;
for (int j = 0; j < childModules.Count; ++j) {
PartModule thisModule = childModules.GetModule(j);
var thisModule2 = thisModule as FNReactor;
if (thisModule2 != null) {
FNReactor fnr = (FNReactor)thisModule;
FloatCurve newISP = new FloatCurve();
FloatCurve vCurve = new FloatCurve ();
if (!currentpropellant_is_jet) {
maxISP = (float)Math.Sqrt((double)fnr.getReactorTemp()) * 17 * ispMultiplier;
minISP = maxISP * 0.4f;
newISP.Add(0, maxISP, 0, 0);
newISP.Add(1, minISP, 0, 0);
curEngine.useVelocityCurve = false;
curEngine.useEngineResponseTime = false;
}
else {
if (thisModule2.getIsNuclear()) {
maxISP = 150;
newISP.Add(0, 100);
newISP.Add(0.3f, 150);
newISP.Add(1, 75);
vCurve.Add(0, 1);
vCurve.Add(400, 0.8f);
vCurve.Add(950, 0.9f);
vCurve.Add (1471, 0);
} else {
maxISP = 2500;
newISP.Add(0, 1200);
newISP.Add(0.3f, 2500);
newISP.Add(1, 800);
vCurve.Add(0, 1);
vCurve.Add(400, 0.8f);
vCurve.Add(1000, 0.9f);
vCurve.Add (2000, 0.5f);
}
curEngine.useVelocityCurve = true;
curEngine.useEngineResponseTime = true;
}
//ModuleEngines curEngine = (ModuleEngines)this.part.Modules["ModuleEngines"];
curEngine.atmosphereCurve = newISP;
curEngine.velocityCurve = vCurve;
assThermalPower = fnr.getReactorThermalPower();
engineMaxThrust = 2000 * assThermalPower / maxISP / 9.81f;
float heat_exchanger_thrust_divisor = 1;
if (radius > fnr.getRadius ()) {
heat_exchanger_thrust_divisor = fnr.getRadius () * fnr.getRadius () / radius / radius;
}else{
heat_exchanger_thrust_divisor = radius * radius / fnr.getRadius () / fnr.getRadius ();
}
if (fnr.getRadius () == 0 || radius == 0) {
heat_exchanger_thrust_divisor = 1;
}
engineMaxThrust = engineMaxThrust * heat_exchanger_thrust_divisor;
if (isLFO) {
engineMaxThrust = engineMaxThrust * 1.5f;
}
curEngine.maxThrust = engineMaxThrust;
}
}
}
if (PartResourceLibrary.Instance.GetDefinition(list_of_propellants[0].name) != null) {
curEngine.propellants.Clear();
curEngine.propellants = list_of_propellants;
curEngine.SetupPropellant();
}
//List<PartResource> partresources = new List<PartResource>();
//part.GetConnectedResources(curEngine.propellants[0].id, partresources);
bool next_propellant = false;
List<ModuleEngines.Propellant> curEngine_propellants_list = new List<ModuleEngines.Propellant>();
curEngine_propellants_list = curEngine.propellants;
foreach(ModuleEngines.Propellant curEngine_propellant in curEngine_propellants_list) {
List<PartResource> partresources = new List<PartResource>();
part.GetConnectedResources(curEngine_propellant.id, partresources);
if(partresources.Count == 0) {
next_propellant = true;
}
}
if (next_propellant && fuel_mode != 1) {
TogglePropellant();
}
/*else {
if ((!isJet && currentpropellant_is_jet) || (isJet && !currentpropellant_is_jet)) {
TogglePropellant();
}
}*/
}