Me 262c 2b
Model | Me-262c-2b |
Value_silv | 790000 |
Reqexp_resp | 320000 |
Unitclass | Fighter |
Train | |
Basic_silv | 230000 |
Expert_silv | 790000 |
Ace_gold | 1800 |
Ace_exp | 770000 |
Repair | |
Timehrsarcade | 126.18 |
Timehrshistorical | 216.144 |
Timehrssimulation | 447.946 |
Timehrsnocrewarcade | 588.36 |
Timehrsnocrewhistorical | 768.287 |
Timehrsnocrewsimulation | 1231.89 |
Costarcade_silv | 4550 |
Costhistorical_silv | 9260 |
Costsimulation_silv | 38840 |
Rewards | |
Battletimeawardarcade | 1300 |
Battletimeawardhistorical | 3900 |
Battletimeawardsimulation | 4700 |
Avgawardarcade | 5674 |
Avgawardhistorical | 7279 |
Avgawardsimulation | 16378 |
Rewardmularcade | 1.1446 |
Rewardmulhistorical | 2.68732 |
Rewardmulsimulation | 5.22742 |
Rewardmulvisualarcade | 2.1 |
Rewardmulvisualhistorical | 3.5 |
Rewardmulvisualsimulation | 5.1 |
Battletimearcade | 65.5907 |
Battletimehistorical | 69.0537 |
Battletimesimulation | 149.193 |
Expmul | 2 |
Groundkillmul | 1 |
Rank | 5 |
Economicrankarcade | 21 |
Economicrankhistorical | 0 |
Economicranksimulation | 21 |
Economicranktankarcade | 21 |
Economicranktankhistorical | 21 |
Economicranktanksimulation | 21 |
Premrewardmulvisualarcade | 0 |
Premrewardmulvisualhistorical | 0 |
Premrewardmulvisualsimulation | 0 |
Misc | |
Gunnerscount | 0 |
Needbuytoopennextintier1 | 1 |
Needbuytoopennextintier2 | 1 |
Needbuytoopennextintier3 | 1 |
Needbuytoopennextintier4 | 1 |
Groundkillmul | 1 |
Sparecost_gold | 70 |
Data | |
Aileronangles | [14, 14] |
Aileroneffectivespeed | 500.004 |
Aileronpowerloss | 2.7 |
Aileronsens | 0.2 |
Allowstrongcontrolsrestrictions | True |
Alphaaileronmin | 0.1 |
Alphaelevatormin | 0.1 |
Alpharuddermin | 0.1 |
Arcadehelperssensitivity | 1 |
Arcadelimitwepmultiplier | 1.8 |
Cockpitdoorspeed | 0.1 |
Crew | 1 |
Criticalspeed | 50 |
Elevatorangles | [28, 20] |
Elevatorpowerloss | 2.6 |
Elevatorsens | 0.26 |
Elevatorseffectivespeed | 620.006 |
Finheight | 1.77482 |
Gearactuatorspeed | 0.2 |
Keelangle | 0 |
Length | 10.58 |
Maxspeedataltitude | 845 |
Maxspeedflaps | 450 |
Maxspeednearground | 864.972 |
Minspeedflaps | 139.2 |
Minimalspeed | 220 |
Momentofinertia | [11227.6, 18674.4, 13528.4] |
Rudderangles | [28, 28] |
Ruddereffectivespeed | 600.005 |
Rudderpowerloss | 2 |
Ruddersens | 0.17 |
Stabangle | 0 |
Stabwidth | 3.59166 |
Vslats | [160, 220] |
Vne | 1050 |
Vnemach | 0.95 |
Wingactuatorspeed | 0.1 |
Wingangle | -0.5 |
Wingspan | 12.5 |
Dvflapsin | [150, 280, 0.15, 0.25] |
Dvflapsout | [150, 280, 0.15, 0.02] |
Fightaibehaviour | Fighter |
Model | Me_262c_2b |
Paratrooper | German |
Type | Fighter |
Booster0 | |
Position | [-0.8, -0.3, 2.25] |
Proppos | [-0.8, -0.3, 2.25] |
Vector | [1, 0, 0] |
Afterburner | |
Iscontrollable | False |
Nitroconsumption | 0 |
Type | 0 |
Compressor | |
Ata0 | 1 |
Ata1 | 2 |
Afterburnercompressionfactor | 1 |
Altitude0 | 6000 |
Compressorpressureatrpm0 | 0.3 |
Compressorturbocompmult | 0.9 |
Compressorturboextmult | 0.1 |
Iscontrollable | False |
Multiplier0 | 0.8 |
Numsteps | 1 |
Rpm0 | 1600 |
Rpm1 | 3480 |
Speedmanifoldmultiplier | 0.8 |
Type | 3 |
Controls | |
Hasmagnetocontrol | False |
Hasradiatorcontrol | False |
Hasthrottlecontrol | True |
Main | |
Advancedjetengine | False |
Afterburnerboost | 1 |
Carbueretortype | 0 |
Consumptionomegamax | 1.05 |
Consumptionomegamincoeff | 1039.18 |
Cylinders | 12 |
Engineacceleration | 0.15 |
Engineinertiamoment | 1 |
Extinguishernum | 0 |
Fuelconsumptiononfullthr | 5 |
Fuelconsumptiononhalfthr | 2 |
Fuelconsumptiononidle | 0 |
Fuelconsumptiononwep | 5 |
Fuelsystemnum | 1 |
Horsepowers | 1200 |
Isautonomous | False |
Iswatercooled | False |
Mass | 165.5 |
Maxcarburetorthrmult | 1.1 |
Optimalspeed | 324 |
Rpmamplitude0 | [3480, 0] |
Rpmamplitude1 | [0, 2] |
Rpmmax | 1600 |
Rpmmaxallowed | 5040 |
Rpmmin | 100 |
Rpmnom | 1600 |
Throttleboost | 1 |
Thrust | 12200 |
Thrustomegamincoeff | 2.40201e-11 |
Turbinetimeconstant | 3.4 |
Type | Rocket |
Userealreductor | True |
Thrustmax | |
Altitude_0 | 0 |
Altitude_1 | 5000 |
Altitude_2 | 10000 |
Altitude_3 | 15000 |
Thrustmax0 | 2700 |
Thrustmaxcoeff_0_0 | 1 |
Thrustmaxcoeff_0_1 | 0.944444 |
Thrustmaxcoeff_0_2 | 0.907407 |
Thrustmaxcoeff_0_3 | 0.874074 |
Thrustmaxcoeff_0_4 | 0.877778 |
Thrustmaxcoeff_0_5 | 0.914815 |
Thrustmaxcoeff_0_6 | 0.974074 |
Thrustmaxcoeff_1_0 | 0.644444 |
Thrustmaxcoeff_1_1 | 0.644444 |
Thrustmaxcoeff_1_2 | 0.607407 |
Thrustmaxcoeff_1_3 | 0.592593 |
Thrustmaxcoeff_1_4 | 0.6 |
Thrustmaxcoeff_1_5 | 0.637037 |
Thrustmaxcoeff_1_6 | 0.703704 |
Thrustmaxcoeff_2_0 | 0.388889 |
Thrustmaxcoeff_2_1 | 0.388889 |
Thrustmaxcoeff_2_2 | 0.374074 |
Thrustmaxcoeff_2_3 | 0.37037 |
Thrustmaxcoeff_2_4 | 0.388889 |
Thrustmaxcoeff_2_5 | 0.414815 |
Thrustmaxcoeff_2_6 | 0.444444 |
Thrustmaxcoeff_3_0 | 0.162963 |
Thrustmaxcoeff_3_1 | 0.162963 |
Thrustmaxcoeff_3_2 | 0.166667 |
Thrustmaxcoeff_3_3 | 0.174074 |
Thrustmaxcoeff_3_4 | 0.185185 |
Thrustmaxcoeff_3_5 | 0.211111 |
Thrustmaxcoeff_3_6 | 0.237037 |
Velocity_0 | 0 |
Velocity_1 | 200 |
Velocity_2 | 400 |
Velocity_3 | 600 |
Velocity_4 | 800 |
Velocity_5 | 1000 |
Velocity_6 | 1200 |
Mixer | |
Altitudepressuretop0 | 0.118161 |
Iscontrollable | False |
Type | 0 |
Propellor | |
Advancedpropradius | 21.825 |
Allowautoprop | False |
Diameter | 43.65 |
Direction | 1 |
Governorafterburnerparam | 0 |
Governormaxparam | 3480 |
Governorminparam | 280 |
Governorspeed | 1 |
Governortype | 0 |
Hasfeatheringcontrol | False |
Inertiamomentcoeff | 1 |
Iscontrollable | False |
Mass | 150 |
Numblades | 2 |
Phialpha0 | 11 |
Phifeather | 1.54 |
Phimax | 1 |
Phimin | 0 |
Propphi0 | 0 |
Propphi1 | 0 |
Propphi2 | 0 |
Propphi3 | 0 |
Propwidth0 | 0 |
Propwidth1 | 0 |
Propwidth2 | 0 |
Propwidth3 | 0 |
Reductor | 1 |
Useadvancedprop | False |
Useautopropinertia | False |
Polar | |
Aftercritdeclinecoeff | 0.0222222 |
Aftercritmaxdistanceangle | 36 |
Aftercritparabangle | 3 |
Cdmin | 0.012 |
Cl0 | 0.4 |
Claftercrit | 1.09 |
Clcrithigh | 1.4 |
Clcritlow | -0.9 |
Alphacrithigh | 17 |
Alphacritlow | -17 |
Lineclcoeff | 0.075 |
Temperature | |
Effectiveradspeed | 250 |
Ineffectiveradmult | 0.8 |
Oilmaxtemp | 96 |
Oilmintemp | 0 |
Oiloutmaxrpmtemp | 80 |
Overheattime | 600 |
Radiatortype | 2 |
Tempchangespeed | 0.01 |
Underheattime | 999 |
Watermaxrpmtemp | 680 |
Watermaxtemp | 650 |
Watermintemp | 0 |
Booster1 | |
Position | [-0.8, -0.3, -2.25] |
Proppos | [-0.8, -0.3, -2.25] |
Vector | [1, 0, 0] |
Afterburner | |
Iscontrollable | False |
Nitroconsumption | 0 |
Type | 0 |
Compressor | |
Ata0 | 1 |
Ata1 | 2 |
Afterburnercompressionfactor | 1 |
Altitude0 | 6000 |
Compressorpressureatrpm0 | 0.3 |
Compressorturbocompmult | 0.9 |
Compressorturboextmult | 0.1 |
Iscontrollable | False |
Multiplier0 | 0.8 |
Numsteps | 1 |
Rpm0 | 1600 |
Rpm1 | 3480 |
Speedmanifoldmultiplier | 0.8 |
Type | 3 |
Controls | |
Hasmagnetocontrol | False |
Hasradiatorcontrol | False |
Hasthrottlecontrol | True |
Main | |
Advancedjetengine | False |
Afterburnerboost | 1 |
Carbueretortype | 0 |
Consumptionomegamax | 1.05 |
Consumptionomegamincoeff | 1039.18 |
Cylinders | 12 |
Engineacceleration | 0.15 |
Engineinertiamoment | 1 |
Extinguishernum | 0 |
Fuelconsumptiononfullthr | 5 |
Fuelconsumptiononhalfthr | 2 |
Fuelconsumptiononidle | 0 |
Fuelconsumptiononwep | 5 |
Fuelsystemnum | 1 |
Horsepowers | 1200 |
Isautonomous | False |
Iswatercooled | False |
Mass | 165.5 |
Maxcarburetorthrmult | 1.1 |
Optimalspeed | 324 |
Rpmamplitude0 | [3480, 0] |
Rpmamplitude1 | [0, 2] |
Rpmmax | 1600 |
Rpmmaxallowed | 5040 |
Rpmmin | 100 |
Rpmnom | 1600 |
Throttleboost | 1 |
Thrust | 12200 |
Thrustomegamincoeff | 2.40201e-11 |
Turbinetimeconstant | 3.4 |
Type | Rocket |
Userealreductor | True |
Thrustmax | |
Altitude_0 | 0 |
Altitude_1 | 5000 |
Altitude_2 | 10000 |
Altitude_3 | 15000 |
Thrustmax0 | 2700 |
Thrustmaxcoeff_0_0 | 1 |
Thrustmaxcoeff_0_1 | 0.944444 |
Thrustmaxcoeff_0_2 | 0.907407 |
Thrustmaxcoeff_0_3 | 0.874074 |
Thrustmaxcoeff_0_4 | 0.877778 |
Thrustmaxcoeff_0_5 | 0.914815 |
Thrustmaxcoeff_0_6 | 0.974074 |
Thrustmaxcoeff_1_0 | 0.644444 |
Thrustmaxcoeff_1_1 | 0.644444 |
Thrustmaxcoeff_1_2 | 0.607407 |
Thrustmaxcoeff_1_3 | 0.592593 |
Thrustmaxcoeff_1_4 | 0.6 |
Thrustmaxcoeff_1_5 | 0.637037 |
Thrustmaxcoeff_1_6 | 0.703704 |
Thrustmaxcoeff_2_0 | 0.388889 |
Thrustmaxcoeff_2_1 | 0.388889 |
Thrustmaxcoeff_2_2 | 0.374074 |
Thrustmaxcoeff_2_3 | 0.37037 |
Thrustmaxcoeff_2_4 | 0.388889 |
Thrustmaxcoeff_2_5 | 0.414815 |
Thrustmaxcoeff_2_6 | 0.444444 |
Thrustmaxcoeff_3_0 | 0.162963 |
Thrustmaxcoeff_3_1 | 0.162963 |
Thrustmaxcoeff_3_2 | 0.166667 |
Thrustmaxcoeff_3_3 | 0.174074 |
Thrustmaxcoeff_3_4 | 0.185185 |
Thrustmaxcoeff_3_5 | 0.211111 |
Thrustmaxcoeff_3_6 | 0.237037 |
Velocity_0 | 0 |
Velocity_1 | 200 |
Velocity_2 | 400 |
Velocity_3 | 600 |
Velocity_4 | 800 |
Velocity_5 | 1000 |
Velocity_6 | 1200 |
Mixer | |
Altitudepressuretop0 | 0.118161 |
Iscontrollable | False |
Type | 0 |
Propellor | |
Advancedpropradius | 21.825 |
Allowautoprop | False |
Diameter | 43.65 |
Direction | 1 |
Governorafterburnerparam | 0 |
Governormaxparam | 3480 |
Governorminparam | 280 |
Governorspeed | 1 |
Governortype | 0 |
Hasfeatheringcontrol | False |
Inertiamomentcoeff | 1 |
Iscontrollable | False |
Mass | 150 |
Numblades | 2 |
Phialpha0 | 11 |
Phifeather | 1.54 |
Phimax | 1 |
Phimin | 0 |
Propphi0 | 0 |
Propphi1 | 0 |
Propphi2 | 0 |
Propphi3 | 0 |
Propwidth0 | 0 |
Propwidth1 | 0 |
Propwidth2 | 0 |
Propwidth3 | 0 |
Reductor | 1 |
Useadvancedprop | False |
Useautopropinertia | False |
Polar | |
Aftercritdeclinecoeff | 0.0222222 |
Aftercritmaxdistanceangle | 36 |
Aftercritparabangle | 3 |
Cdmin | 0.012 |
Cl0 | 0.4 |
Claftercrit | 1.09 |
Clcrithigh | 1.4 |
Clcritlow | -0.9 |
Alphacrithigh | 17 |
Alphacritlow | -17 |
Lineclcoeff | 0.075 |
Temperature | |
Effectiveradspeed | 250 |
Ineffectiveradmult | 0.8 |
Oilmaxtemp | 96 |
Oilmintemp | 0 |
Oiloutmaxrpmtemp | 80 |
Overheattime | 300 |
Radiatortype | 2 |
Tempchangespeed | 0.01 |
Underheattime | 999 |
Watermaxrpmtemp | 680 |
Watermaxtemp | 650 |
Watermintemp | 0 |
Engine0 | |
Direction | [0, 0] |
Position | [-0.5, -0.7, 2.25] |
Proppos | [-0.5, -0.7, 2.25] |
Afterburner | |
Iscontrollable | False |
Nitroconsumption | 0 |
Type | 0 |
Compressor | |
Ata0 | 1 |
Ata1 | 2 |
Afterburnermanifoldpressure | 2 |
Altitude0 | 6000 |
Altitudeconstrpm0 | 18300 |
Ceiling0 | 6100 |
Compressorpressureatrpm0 | 0.3 |
Compressorturbocompmult | 0.9 |
Compressorturboextmult | 0.1 |
Externalpressurelimit | True |
Iscontrollable | False |
Numsteps | 1 |
Power0 | 960 |
Poweratceiling0 | 200 |
Powerconstrpm0 | 1200 |
Powerconstrpmcurvature0 | 0.5 |
Rpm0 | 1600 |
Rpm1 | 9800 |
Speedmanifoldmultiplier | 0.8 |
Type | 3 |
Controls | |
Hasmagnetocontrol | False |
Hasradiatorcontrol | False |
Hasthrottlecontrol | True |
Main | |
Advancedjetengine | True |
Afterburnerboost | 1 |
Carbueretortype | 0 |
Consumptionomegamax | 1.15 |
Consumptionomegamincoeff | 1039.18 |
Cylinders | 12 |
Engineacceleration | 0.15 |
Engineinertiamoment | 1 |
Extinguishernum | 0 |
Fuelconsumptiononfullthr | 1.15 |
Fuelconsumptiononhalfthr | 0.5 |
Fuelconsumptiononidle | 0.175 |
Fuelconsumptiononwep | 1.25 |
Fuelsystemnum | 0 |
Isautonomous | False |
Iswatercooled | False |
Mass | 900 |
Maxcarburetorthrmult | 1.1 |
Optimalspeed | 324 |
Power | 1200 |
Rpmamplitude0 | [9500, 0] |
Rpmamplitude1 | [3000, 2] |
Rpmmax | 9800 |
Rpmmaxallowed | 11000 |
Rpmmin | 1600 |
Rpmnom | 9000 |
Throttleboost | 1.08 |
Thrust | 8000 |
Thrustomegamincoeff | 2.40202e-11 |
Turbinetimeconstant | 3.4 |
Type | Jet |
Userealreductor | True |
Thrustmax | |
Altitude_0 | 0 |
Altitude_1 | 3047 |
Altitude_2 | 6095 |
Altitude_3 | 9143 |
Altitude_4 | 12000 |
Thrustmax0 | 910 |
Thrustmaxcoeff_0_0 | 1 |
Thrustmaxcoeff_0_1 | 0.89 |
Thrustmaxcoeff_0_2 | 0.85 |
Thrustmaxcoeff_0_3 | 0.83 |
Thrustmaxcoeff_0_4 | 0.85 |
Thrustmaxcoeff_0_5 | 0.88 |
Thrustmaxcoeff_0_6 | 0.98 |
Thrustmaxcoeff_1_0 | 0.8 |
Thrustmaxcoeff_1_1 | 0.72 |
Thrustmaxcoeff_1_2 | 0.69 |
Thrustmaxcoeff_1_3 | 0.68 |
Thrustmaxcoeff_1_4 | 0.7 |
Thrustmaxcoeff_1_5 | 0.73 |
Thrustmaxcoeff_1_6 | 0.78 |
Thrustmaxcoeff_2_0 | 0.595 |
Thrustmaxcoeff_2_1 | 0.565 |
Thrustmaxcoeff_2_2 | 0.545 |
Thrustmaxcoeff_2_3 | 0.54 |
Thrustmaxcoeff_2_4 | 0.555 |
Thrustmaxcoeff_2_5 | 0.585 |
Thrustmaxcoeff_2_6 | 0.625 |
Thrustmaxcoeff_3_0 | 0.489 |
Thrustmaxcoeff_3_1 | 0.459 |
Thrustmaxcoeff_3_2 | 0.44 |
Thrustmaxcoeff_3_3 | 0.44 |
Thrustmaxcoeff_3_4 | 0.454 |
Thrustmaxcoeff_3_5 | 0.465 |
Thrustmaxcoeff_3_6 | 0.478 |
Thrustmaxcoeff_4_0 | 0.372 |
Thrustmaxcoeff_4_1 | 0.366 |
Thrustmaxcoeff_4_2 | 0.353 |
Thrustmaxcoeff_4_3 | 0.343 |
Thrustmaxcoeff_4_4 | 0.349 |
Thrustmaxcoeff_4_5 | 0.367 |
Thrustmaxcoeff_4_6 | 0.385 |
Velocity_0 | 0 |
Velocity_1 | 200 |
Velocity_2 | 400 |
Velocity_3 | 600 |
Velocity_4 | 800 |
Velocity_5 | 1000 |
Velocity_6 | 1200 |
Mixer | |
Altitudepressuretop0 | 0.118161 |
Iscontrollable | False |
Type | 0 |
Propellor | |
Advancedpropradius | 21.825 |
Allowautoprop | False |
Diameter | 43.65 |
Direction | 1 |
Governorafterburnerparam | 9800 |
Governormaxparam | 9499 |
Governorminparam | 1800 |
Governorspeed | 1 |
Governortype | 0 |
Hasfeatheringcontrol | False |
Inertiamomentcoeff | 1 |
Iscontrollable | False |
Mass | 150 |
Numblades | 2 |
Phialpha0 | 11 |
Phifeather | 1.54 |
Phimax | 1 |
Phimin | 0 |
Propphi0 | 0 |
Propphi1 | 0 |
Propphi2 | 0 |
Propphi3 | 0 |
Propwidth0 | 0 |
Propwidth1 | 0 |
Propwidth2 | 0 |
Propwidth3 | 0 |
Reductor | 1 |
Useadvancedprop | False |
Useautopropinertia | False |
Polar | |
Aftercritdeclinecoeff | 0.0222222 |
Aftercritmaxdistanceangle | 36 |
Aftercritparabangle | 3 |
Cdmin | 0.012 |
Cl0 | 0.4 |
Claftercrit | 1.09 |
Clcrithigh | 1.4 |
Clcritlow | -0.87 |
Machcrit1 | 0.6 |
Machcrit2 | 0.65 |
Machcrit3 | 0.3 |
Machcrit4 | 0.3 |
Machcrit5 | 0.6 |
Machfactor | 2 |
Machmax1 | 1 |
Machmax2 | 0.97 |
Machmax3 | 1 |
Machmax4 | 1 |
Machmax5 | 1.5 |
Multlimit1 | 1 |
Multlimit2 | 1 |
Multlimit3 | 0.25 |
Multlimit4 | 0.25 |
Multlimit5 | 5 |
Multlinecoeff1 | -5.2 |
Multlinecoeff2 | -3.7 |
Multlinecoeff3 | -0.44 |
Multlinecoeff4 | -0.2 |
Multlinecoeff5 | 1.1 |
Multmachmax1 | 7 |
Multmachmax2 | 6.7 |
Multmachmax3 | 0.32 |
Multmachmax4 | 0.4 |
Multmachmax5 | 2 |
Alphacrithigh | 17 |
Alphacritlow | -17 |
Lineclcoeff | 0.075 |
Temperature | |
Effectiveradspeed | 250 |
Ineffectiveradmult | 0.8 |
Oilmaxtemp | 96 |
Oilmintemp | 0 |
Oiloutmaxrpmtemp | 85 |
Overheattime | 300 |
Radiatortype | 2 |
Tempchangespeed | 0.02 |
Underheattime | 999 |
Watermaxrpmtemp | 660 |
Watermaxtemp | 650 |
Watermintemp | 0 |
Gear | |
Centerwheelradius | 0.303 |
Floats | False |
Frontalspringscoeff | 351977 |
Frontalspringsheight | 0.6 |
Haswheels | True |
Height | 1.82 |
Leftwheelradius | 0.385 |
Pitch | 0 |
Retractabletailstrut | False |
Rightwheelradius | 0.385 |
Sinkfactor | 500 |
Tailspringscoeff | 351977 |
Tailspringsheight | 0.6 |
Waterfriction | 1 |
Mass | |
Advancedmass | False |
Centerofgravity | [-0.15, 0, 0] |
Emptymass | 4995 |
Flapsdestructionindspeed | 320.4 |
Geardestructionindspeed | 450 |
Maxfuelmass0 | 1070 |
Maxfuelmass1 | 1500 |
Maxnitro | 0 |
Oilmass | 25 |
Separatefueltanks | True |
Takeoff | 7800 |
Wingcritoverload | [-149812, 309812] |
Parts | |
Tank1_capacity | 1070 |
Tank1_system | 0 |
Tank2_capacity | 1500 |
Tank2_system | 1 |
Passport | |
Climbspeedias | True |
Climbspeednum | 0 |
Mass | 0 |
Turntimeflaps | 0 |
Alt | {} |
Ias | {} |
Climbspeed | {} |
Selfsealingtanks | |
Tank1_dm | True |
Tank2_dm | True |
Tank3_dm | True |
Tank4_dm | True |
Tank5_dm | True |
Tank6_dm | True |
Tank7_dm | True |
Tank8_dm | True |
Shop | |
Airfieldlen | 628.433 |
Climbalt | 6000 |
Climbspeed | 20 |
Climbtime | 408 |
Maxaltitude | 14900 |
Maxspeed | 240.27 |
Maxspeedalt | 6000 |
Turntime | 30.2541 |
Arcadeoverride | |
Maxspeedmultiplier | 1.15 |
Wepoverspeed | 1.1 |
Balancedata | |
Accspd | 4.03451 |
Climbspeed | 20 |
Maxspeed | 240.27 |
Turntime | 28.1492 |
Commonweapons | |
Weapon | |
Blk | Cannonmk108 |
Bullets | 80 |
Counterindex | 1 |
Spread | 1.2 |
Traceoffset | 1 |
Trigger | Cannon |
Weapon2 | |
Blk | Cannonmk108 |
Bullets | 100 |
Counterindex | 2 |
Spread | 1.2 |
Traceoffset | 1 |
Trigger | Cannon |
Weapon3 | |
Blk | Cannonmk108 |
Bullets | 100 |
Spread | 1.2 |
Trigger | Cannon |
Weapon4 | |
Blk | Cannonmk108 |
Bullets | 80 |
Spread | 1.2 |
Trigger | Cannon |
Fireparams | |
Engineextinguishfirespeed | [193, 277] |
Engineextinguishfirespeedchance | [0.01, 0.1] |
Firedamagepowerrel | 0.05 |
Nonextinguishfiretime | 5 |
Overheat_arcade | |
Enginecooldowntime | 18 |
Engineoverheatcooldowntime | 14 |
Engineoverheattime | 25 |
Enginetempafteroverheat | 0.15 |
Guncooldowntime | 2.5 |
Gunoverheatcooldowntime | 3 |
Gunoverheattime | 8 |
Guntempafteroverheat | 0.15 |
Overheat_hardcore | |
Enginecooldowntime | 20 |
Engineoverheatcooldowntime | 60 |
Engineoverheattime | 40 |
Enginetempafteroverheat | 0.3 |
Guncooldowntime | 2.5 |
Gunoverheatcooldowntime | 3 |
Gunoverheattime | 4 |
Guntempafteroverheat | 0.2 |
Overheat_realistic | |
Enginecooldowntime | 20 |
Engineoverheatcooldowntime | 60 |
Engineoverheattime | 40 |
Enginetempafteroverheat | 0.3 |
Guncooldowntime | 2.5 |
Gunoverheatcooldowntime | 3 |
Gunoverheattime | 4 |
Guntempafteroverheat | 0.2 |
Tags | |
All | True |
Axis | True |
Axis_achievement | True |
Berlin | True |
Can_be_played_with_cockpit_view_only | True |
Country_germany | True |
Eastern_front | True |
Hangar | True |
Jet_engine | True |
Training | True |
Type_fighter | True |
Type_jet_fighter | True |
Western_front | True |
Year1944 | True |
Year1945 | True |
Years_active | |
Year1944 | |
Berlin | 0.6 |
Year1945 | |
Berlin | 0.9 |