109 K-4 and 190 D-9 have the same engine thrust?

In "...\CoreMods\WWII Units\Bf-109K-4.lua":

engine = {
           Nmg     = 20.5, -- RPM at idle
           MinRUD  = 0, -- Min state of the throttle
           MaxRUD  = 1, -- Max state of the throttle
           MaksRUD = 1, -- Military power state of the throttle
           ForsRUD = 1, -- Afterburner state of the throttle
           typeng  = 2, --PISTON ENGINE
		--[[
			E_TURBOJET = 0
			E_TURBOJET_AB = 1
			E_PISTON = 2
			E_TURBOPROP = 3
			E_TURBOFAN				= 4
			E_TURBOSHAFT = 5
		--]]
		
           hMaxEng = 12.5, -- Max altitude for safe engine operation in km
           dcx_eng = 0.015, -- Engine drag coeficient
           cemax   = 0.37, -- not used for fuel calulation , only for AI routines to check flight time ( fuel calculation algorithm is built in )
           cefor   = 0.37, -- not used for fuel calulation , only for AI routines to check flight time ( fuel calculation algorithm is built in )
           dpdh_m  = 1800, -- altitude coefficient for max thrust
           dpdh_f  = 1800, -- altitude coefficient for AB thrust

           k_adiab_1           = 0.037923,
           k_adiab_2			= 0.0562,
           MAX_Manifold_P_1	= 180000,		
           MAX_Manifold_P_2	= 180000,		
           MAX_Manifold_P_3	= 180000,		
           k_after_cool		= 0.0,
           Displ				= 35,
           k_Eps				= 6.5,
           Stroke				= 0.165,
           V_pist_0			= 13,
           Nu_0				= 1.2,
           Nu_1				= 0.9,
           Nu_2				= 0.001,
           N_indic_0			= 1052480,
           N_fr_0				= 0.04,
           N_fr_1				= 0.001,
		Init_Mom			= 220,
		D_prop				= 3.5,
		MOI_prop			= 45,
		k_gearbox			= 2.4,
		P_oil				= 495438,
		k_boost				= 3,
		k_cfug				= 0.003,
		k_oil				= 0.00004,
		k_piston			= 3000,
		k_reg				= 0.003,
		k_vel				= 0.017,
		table_data = 
		{
		--   M			Pmax
			{0.0,		16620.0},
			{0.1,		15600.0},
			{0.2,		14340.0},
			{0.3,		13320.0},
			{0.4,		12230.0},
			{0.5,		11300.0},
			{0.6,		10600.0},
			{0.7,		10050.0},
			{0.8,		 9820.0},
			{0.9,		 5902.0},
			{1.9,		 3469.0}
		}
		-- M - Mach number
		-- Pmax - Engine thrust at military power
		-- Pfor - Engine thrust at AFB
	}, -- end of engine

And in "...\CoreMods\WWII Units\FW-190D9.lua"

engine = 
	{
		Nmg	=	20.5, -- RPM at idle
		MinRUD	=	0, -- Min state of the throttle
		MaxRUD	=	1, -- Max state of the throttle
		MaksRUD	=	1, -- Military power state of the throttle
		ForsRUD	=	1, -- Afterburner state of the throttle
		typeng	=	2,--PISTON ENGINE
		--[[
			E_TURBOJET = 0
			E_TURBOJET_AB = 1
			E_PISTON = 2
			E_TURBOPROP = 3
			E_TURBOFAN				= 4
			E_TURBOSHAFT = 5
		--]]
		
		hMaxEng	=	12.5, -- Max altitude for safe engine operation in km
		dcx_eng	=	0.015, -- Engine drag coeficient
		cemax	=	0.37, -- not used for fuel calulation , only for AI routines to check flight time ( fuel calculation algorithm is built in )
		cefor	=	0.37, -- not used for fuel calulation , only for AI routines to check flight time ( fuel calculation algorithm is built in )
		dpdh_m	=	1800, --  altitude coefficient for max thrust
		dpdh_f	=	1800,  --  altitude coefficient for AB thrust
		
		k_adiab_1			= 0.037923,
		k_adiab_2			= 0.0562,
		MAX_Manifold_P_1	= 155774,		
		MAX_Manifold_P_2	= 206570,		
		MAX_Manifold_P_3	= 226648,		
		k_after_cool		= 0.0,
		Displ				= 35,
		k_Eps				= 6.5,
		Stroke				= 0.165,
		V_pist_0			= 13,
		Nu_0				= 1.2,
		Nu_1				= 0.9,
		Nu_2				= 0.001,
		N_indic_0			= 1052480,
		N_fr_0				= 0.04,
		N_fr_1				= 0.001,
		Init_Mom			= 220,
		D_prop				= 3.5,
		MOI_prop			= 45,
		k_gearbox			= 2.4,
		P_oil				= 495438,
		k_boost				= 3,
		k_cfug				= 0.003,
		k_oil				= 0.00004,
		k_piston			= 3000,
		k_reg				= 0.003,
		k_vel				= 0.017,
		table_data = 
		{
		--   M			Pmax
			{0.0,		16620.0},
			{0.1,		15600.0},
			{0.2,		14340.0},
			{0.3,		13320.0},
			{0.4,		12230.0},
			{0.5,		11300.0},
			{0.6,		10600.0},
			{0.7,		10050.0},
			{0.8,		 9820.0},
			{0.9,		 5902.0},
			{1.9,		 3469.0}
		}
		-- M - Mach number
		-- Pmax - Engine thrust at military power
		-- Pfor - Engine thrust at AFB
	}, -- end of engine

The only difference are"MAX_Manifold_P_1", "MAX_Manifold_P_2" and "MAX_Manifold_P_3".

Is this real?

+1

附议（Second it）..

Suspicios. Could be a placeholder though.