J57-420 and J79-IAI

Because I wanted to

GameData/RealismOverhaul/Engine_Configs/Jet_Engine_Configs/J57_Config.cfg

@@ -151,13 +151,37 @@
 //	Exhaust Mixer: false
 //	Adjustable Nozzle: true
 //	=================================================================================
+//	J57-P-420
+//	1967, F-8H/J, RF-8G
+//
+//	Dry Mass: 2195 kg
+//	Thrust (Dry): 55.2 kN
+//	Thrust (Wet): 87.2 kN
+//	SFC (Dry): 0.87 lb/lbf-hr
+//	Area: 0.24 m^2	//Compressor Area
+//	BPR: 0.0		//Bypass Ratio
+//	CPR: 13.0		//Compressor Pressure Ratio
+//	FPR: 0.0		//Fan Ratio
+//	Mdes: 0.9 M		//Mach Design Point
+//	Tdes: 250 K		//Temp Design Point
+//	eta_n: 0.7		//Efficiency at afterburner rear / nozzle entrance
+//	FHV: 35000000 J	//Fuel heat of burning
+//	TIT: 1330 K		//Combustion peak temp
+//	TAB: 2556* K		//Afterburner peak temp
+//	maxT3: 825 K	//Turbine max temperature
+//	Exhaust Mixer: false
+//	Adjustable Nozzle: true
+//	=================================================================================
 
 //	Sources:
 
 //	https://www.jet-engine.net/miltfspec.htm
 //	https://en.wikipedia.org/wiki/Pratt_%26_Whitney_J57
 //	https://www.thisdayinaviation.com/tag/pratt-whitney-jt3c-6/
 //	https://aircorpslibrary.com/jt3c-4-and-jt3c-6/
+//	https://www.marvellouswings.com/Aircraft/Fighter/F-8/F-8.html
+//	https://www.aerosociety.com/media/8037/an-examination-of-the-f-8-crusader-through-archival-sources.pdf
+//	https://www.tapatalk.com/groups/warships1discussionboards/if-no-phantom-upgrade-what-to-operate-from-audacio-t31193.html
 
 //	Used by:
 
@@ -519,7 +543,7 @@
 		CONFIG
 		{
 			name = J57-P-20A
-			description = Ultimate afterburning J57, as used on the F-8E/J. Temperature Mach limit at 15 km: 2.5.
+			description = Afterburning J57, as used on the F-8E/J. Temperature Mach limit at 15 km: 2.5.
 			massMult = 1.00
 
 			Area = 0.24	//Compressor Area
@@ -547,6 +571,44 @@
 			drySFC = 0.77
 			throttleResponseMultiplier = 0.3	//60s double-spool, 0.3
 
+			PROPELLANT
+			{
+				name = Kerosene
+				ratio = 1.0
+				DrawGauge = True
+			}
+		}
+		CONFIG
+		{
+			name = J57-P-420
+			description = Ultimate afterburning J57, remanufactured J57-P-20 as used on upgraded F-8H/J. Temperature Mach limit at 15 km: 2.58.
+			massMult = 1.0186
+
+			Area = 0.24	//Compressor Area
+			BPR = 0		//Bypass Ratio
+			CPR = 13.0		//Compressor Pressure Ratio
+			FPR = 0		//Fan Ratio
+			Mdes = 0.9		//Mach Design Point
+			Tdes = 250		//Temp Design Point
+			eta_c = 0.95	//Efficiency at burner inlet
+			eta_t = 0.98	//Efficiency at burner exit
+			eta_n = 0.7	//Efficiency at afterburner rear / nozzle entrance
+			FHV = 35000000	//Fuel heat of burning (joules?)
+			TIT = 1330		//Combustion peak temp
+			TAB = 2556		//Afterburner temp?
+			maxT3 = 850	//Turbine max temperature
+			exhaustMixer = False
+			adjustableNozzle = True
+			thrustUpperLimit = 170
+
+			// Engine fitting params
+			defaultTPR = 0.85
+			dryThrust = 55.2
+			wetThrust = 87.2
+			maxThrust = 87.2	//Just to let MEC know thrust
+			drySFC = 0.87
+			throttleResponseMultiplier = 0.3	//60s double-spool, 0.3
+
 			PROPELLANT
 			{
 				name = Kerosene

GameData/RealismOverhaul/Engine_Configs/Jet_Engine_Configs/J79_Config.cfg

@@ -198,7 +198,7 @@
 //
 //	Dry Mass: 1745 kg
 //	Thrust (Dry): 53.60 kN
-//	Thrust (Wet): 82.29 kN
+//	Thrust (Wet): 83.29 kN
 //	SFC (Dry): 0.834 lb/lbf-hr
 //	Area: 0.29 m^2	//Compressor Area
 //	BPR: 0.0		//Bypass Ratio
@@ -214,11 +214,33 @@
 //	Exhaust Mixer: false
 //	Adjustable Nozzle: true
 //	=================================================================================
+//	J79-IAI-J1E
+//	1982, Kfir C.7
+//
+//	Dry Mass: 1740? kg
+//	Thrust (Dry): 49.4 kN
+//	Thrust (Wet): 83.4 kN
+//	SFC (Dry): 0.843? lb/lbf-hr
+//	Area: 0.29 m^2	//Compressor Area
+//	BPR: 0.0		//Bypass Ratio
+//	CPR: 12.2		//Compressor Pressure Ratio
+//	FPR: 0.0		//Fan Ratio
+//	Mdes: 0.9 M		//Mach Design Point
+//	Tdes: 250 K		//Temp Design Point
+//	eta_n: 0.7		//Efficiency at afterburner rear / nozzle entrance
+//	FHV: 28000000 J	//Fuel heat of burning
+//	TIT: 1261? K		//Combustion peak temp
+//	TAB: 2767* K		//Afterburner peak temp
+//	maxT3: 850 K	//Turbine max temperature
+//	Exhaust Mixer: false
+//	Adjustable Nozzle: true
+//	=================================================================================
 
 //	Sources:
 
 //	http://www.leteckemotory.cz/motory/j79/
 //	https://www.jet-engine.net/miltfspec.htm
+//	http://paulcegelski.com/j79.html
 
 //	Used by:
 
@@ -641,11 +663,50 @@
 			// Engine fitting params
 			defaultTPR = 0.85
 			dryThrust = 53.60
-			wetThrust = 82.29
-			maxThrust = 82.29	//Just to let MEC know thrust
+			wetThrust = 83.29
+			maxThrust = 83.29	//Just to let MEC know thrust
 			drySFC = 0.834
 			throttleResponseMultiplier = 0.60
 
+			PROPELLANT
+			{
+				name = Kerosene
+				ratio = 1.0
+				DrawGauge = True
+			}
+		}
+		CONFIG
+		{
+			name = J79-IAI-J1E
+			description = License-built J79, created by IAI for the Kfir C.7. Temperature Mach limit at 15 km: 2.75.
+			specLevel = operational
+			massMult = 1.1538
+
+			Area = 0.29		//Compressor Area
+			BPR = 0.0		//Bypass Ratio
+			CPR = 12.2		//Compressor Pressure Ratio
+			FPR = 0.0		//Fan Ratio
+			Mdes = 0.9		//Mach Design Point
+			Tdes = 250		//Temp Design Point
+			eta_c = 0.95	//Efficiency at burner inlet
+			eta_t = 0.98	//Efficiency at burner exit
+			eta_n = 0.7		//Efficiency at afterburner rear / nozzle entrance
+			FHV = 28000000	//Fuel heat of burning (joules?)
+			TIT = 1261		//Combustion peak temp
+			TAB = 2767		//Afterburner temp?
+			maxT3 = 850		//Turbine max temperature
+			exhaustMixer = False
+			adjustableNozzle = True
+			thrustUpperLimit = 160
+
+			// Engine fitting params
+			defaultTPR = 0.85
+			dryThrust = 49.4
+			wetThrust = 83.4
+			maxThrust = 83.4	//Just to let MEC know thrust
+			drySFC = 0.843
+			throttleResponseMultiplier = 0.60
+
 			PROPELLANT
 			{
 				name = Kerosene