#Title:An124
#Author:SP4, Ratty
#Version:Beta v0.1 Engines Lotarev D18T Turbofan (51,590 lbs)
#MODIF MAV-JP / STORE LIMITER / TO BE USED WITH ASSOCIATED WCD
#
# SIMULATION INPUT PANEL
#
# INPUT MASS AND GEOMETRIC PROPERTIES:
        385800  # Empty Weight (lbs)
          6760  # Reference Area
        165100  # Internal Fuel
#
#
# ANGLE OF ATTACK AND SIDESLIP LIMITS
            20  # AOA Max
            -5  # AOA Min
             5  # Beta Max
            -5  # Beta Min
           2.3  # Max G
            60  # Max Roll
           220  # Min Vcas
           450  # Max Vcas
           250  # Corner Vcas
             6  # Theta Max
             3  # Num Gear
# Gear X, Y, Z, Rng
          32.2             0            15           100
         114.9           -42            15           100
         114.9            42            15           100
#
# Physical data
          95.5  # CG Loc
           175  # Length
         240.6  # Span
          12.5  # Fus Radius
          68.2  # Tail Ht
#
# End of Airframe data
#
#
#
#     BASIC AERODYNAMIC COEFFICIENTS
#
#
#     MACH BREAKPOINTS
#
5   # Num MACH
             0           0.4           0.6           0.8
          0.86
#
#     ALPHA BREAKPOINTS
#
12   # Num Alpha
           -20           -10            -5             0
             5            10            15            20            25
            30            35            40
#
#     LIFT COEFFICIENT  CL
#
             1  # Table Multiplier
#
# Mach 0.00
       -0.7056       -0.4844       -0.0991         0.155          0.62         1.005
        1.3604        1.6349        1.8161        2.0743        2.1527        2.1416
#
# Mach 0.40
       -0.7093       -0.4873       -0.1012         0.155          0.62         1.004
         1.361         1.633        1.8114         2.069         2.152         2.143
#
# Mach 0.60
       -0.7093       -0.4873       -0.1012        0.0155         0.652        1.0324
        1.3891        1.6611        1.8395        2.0974        2.1808        2.1701
#
# Mach 0.80
        -0.704        -0.479       -0.0896         0.175        0.7619        1.1353
        1.4996        1.7619        1.9286         2.185         2.288         2.284
#
# Mach 0.86
        -0.679        -0.454       -0.0646           0.2        0.8228        1.1962
        1.5605        1.8228         1.989        2.2464          2.34          2.34
#
#     DRAG COEFFICIENT  CD
#
           0.7  # Table Multiplier
#
# Mach 0.00
        0.1981        0.1482        0.0358        0.0157        0.0332        0.0806
        0.1816        0.4582        0.5752        0.8598         1.106        1.3599
#
# Mach 0.40
        0.1873        0.1474        0.0575        0.0147        0.0324        0.0654
        0.1462        0.2885        0.4611        0.6887        0.8857        1.0888
#
# Mach 0.60
        0.1883        0.1484        0.0585        0.0157        0.0341        0.0699
        0.1507         0.293        0.4656        0.6932        0.8902        1.0934
#
# Mach 0.80
        0.1974        0.1576        0.0634        0.0163        0.0354        0.0739
        0.1534        0.2977        0.4688        0.6981        0.8877        1.0992
#
# Mach 0.86
        0.2021        0.1623        0.0681         0.021        0.0358        0.0743
        0.1538        0.2981        0.4692        0.6985        0.8881         1.099
#
#     SIDE FORCE DERIVATIVE CY-BETA
#
             1  # Table Multiplier
#
# Mach 0.00
        -0.011       -0.0109       -0.0166       -0.0182       -0.0192       -0.0187
       -0.0163       -0.0176       -0.0164       -0.0158       -0.0141        -0.009
#
# Mach 0.40
        -0.011          0.37       -0.0166       -0.0182       -0.0192       -0.0187
       -0.0163       -0.0176       -0.0164       -0.0158       -0.0141        -0.009
#
# Mach 0.60
        -0.011       -0.0109          0.57       -0.0182       -0.0192       -0.0187
       -0.0163       -0.0176       -0.0164       -0.0158       -0.0141        -0.009
#
# Mach 0.80
       -0.0115       -0.0112       -0.0172          0.69       -0.0196       -0.0196
       -0.0168       -0.0178       -0.0167       -0.0161       -0.0148        -0.013
#
# Mach 0.86
        -0.012       -0.0118        -0.018       -0.0195         -0.74         -0.02
       -0.0174       -0.0182       -0.0171       -0.0168       -0.0155       -0.0142
# End of Aero Data
#
#
# PROPULSION DATA
#
             4  # Thrust multiplier
             1  # Fuel Flow Multiplier
#
# MACH BREAKPOINTS
#
10   # Number of Mach Breaks
             0           0.1           0.2           0.3           0.4           0.5
           0.6           0.7           0.8           0.9
#
#     ALTITUDE BREAKPOINTS
#
7   # Number of Alt Break Points
             0          5000         10000         20000         30000         36000
         45000
#
#    THRST1 - THRUST AT IDLE (THROTL = 0.00)
#
# Alt 0
             0             0             0             0             0             0             0             0             0             0
#
# Alt 5000
             0             0             0             0             0             0             0             0             0             0
#
# Alt 10000
             0             0             0             0             0             0             0             0             0             0
#
# Alt 20000
             0             0             0             0             0             0             0             0             0             0
#
# Alt 30000
             0             0             0             0             0             0             0             0             0             0
#
# Alt 36000
             0             0             0             0             0             0             0             0             0             0
#
# Alt 45000
             0             0             0             0             0             0             0             0             0             0
#
#    THRST2 - THRUST AT MIL POWER (THROTL = 1.00)
#
# Alt 0
       50042.3       44753.3       40684.8       37023.2       34073.5       31530.7       29496.5       28174.2       27157.1       25834.8
#
# Alt 5000
       41701.9       37633.4       34582.1       32751.3       31530.7       29293.1       27462.3       26445.1       25224.6       24105.7
#
# Alt 10000
       34582.1       31123.9       28479.3       26953.7       25733.1         25428         25428       24410.9       23393.8       22376.6
#
# Alt 20000
       23393.8       21359.5       19325.3       18308.2         17291       17087.6         17291       17494.5       18104.7       18511.6
#
# Alt 30000
       15256.8         13426       12408.9         12002       11391.7       11188.3       11188.3       11391.7         12002       12205.4
#
# Alt 36000
       11595.2       10679.8       9560.92       9154.07       8747.23        8543.8        8543.8       8747.23       8950.65        9357.5
#
# Alt 45000
       3000.11       3000.99       3000.71       3000.29       3000.58       3000.87       3000.87       3000.29       3000.71       3000.43
#
#    THRST3 - THRUST AT FULL AB (THROTL = 1.05)
#
# Alt 0
       50042.3       44753.3       40684.8       37023.2       34073.5       31530.7       29496.5       28174.2       27157.1       25834.8
#
# Alt 5000
       41701.9       37633.4       34582.1       32751.3       31530.7       29293.1       27462.3       26445.1       25224.6       24105.7
#
# Alt 10000
       34582.1       31123.9       28479.3       26953.7       25733.1         25428         25428       24410.9       23393.8       22376.6
#
# Alt 20000
       23393.8       21359.5       19325.3       18308.2         17291       17087.6         17291       17494.5       18104.7       18511.6
#
# Alt 30000
       15256.8         13426       12408.9         12002       11391.7       11188.3       11188.3       11391.7         12002       12205.4
#
# Alt 36000
       11595.2       10679.8       9560.92       9154.07       8747.23        8543.8        8543.8       8747.23       8950.65        9357.5
#
# Alt 45000
       3000.11       3000.99       3000.71       3000.29       3000.58       3000.87       3000.87       3000.29       3000.71       3000.43
#
#    ROLL DATA
#
#
#    ALPHA BREAKPOINTS
5   # Num ALPHA
           -10             0            10            20            30
#
#     DYNAMIC PRESSURE BREAKPOINTS
#
7   # Num QBAR
             0           100           200           300           400           500
           600
#
#     RCMDMX - PEAK ROLL RATE
#
             1  # Table Multiplier
#
# ALPHA -10
             0            30            30            30            30            30            30
#
# ALPHA 0
             0            30            60            60            60            60            60
#
# ALPHA 10
             0            30            30            30            30            30            30
#
# ALPHA 20
             0            10            20            20            20            20            20
#
# ALPHA 30
             0            10            10            10            10            10            10
#
# End Of Roll Data
#
#
# LIMITERS
#
17   # Number of limiters
# Type Key Values
#
# Neg G Limiter
0 0            250            -3           100             0
# Pos G Limiter (Cat I)
3 1             15             9          20.4           7.3            25             1
# Roll Rate Limiter
0 2             15             1            29             0
# Yaw Alpha Limiter
0 3             14             1            26             0
# Yaw Roll Rate Limiter
0 4             20             1           360             0
# Cat III Command Type
0 5            100             7           420            15
# Cat III AOA Limiter
1 6             17
# Cat III Roll Rate Limiter
2 7            0.6
# Cat III Yaw Alpha Limiter
0 8              3             1            15             0
# Cat III Yaw Roll Rate Limiter
0 9             20             1           180             0
# Pitch and Yaw Control Damper
3 10              0           0.3            15          0.85            50             1
# Roll Control Damper
3 11              0           0.6            15          0.85            50             2
# Command Type
1 12             15
# Low Speed Omega
3 13           0.01           0.1            40           0.8            60             1
# Stores Drag
0 14            0.9       0.0001             1       0.000283
# Cat III Max Gs
1 16              1
# AOA Limiter
1 17             20
#
# End Of Limiters
#
#
#  ADDITIONAL DATA
#
normSpoolRate 2
abSpoolRate 2
jfsSpoolUpRate 15
jfsSpoolUpLimit 0.25
lightupSpoolRate 10
flameoutSpoolRate 35
jfsRechargeTime 60
jfsMinRechargeRpm 0.12
jfsSpinTime 240
mainGenRpm 0.63
stbyGenRpm 0.6
epuBurnTime 600
DeepStallEngineStall 0
engineDamageStopThreshold 15
engineDamageNoRestartThreshold 3
engineDamageHitThreshold 50
rollMomentum 1.3
pitchMomentum 1.3
yawMomentum 1.3
pitchElasticity 1
gearPitchFactor 0
rollGearGain 1
yawGearGain 1
pitchGearGain 1
sinkRate 15
tefMaxAngle 50
hasFlapperons 0
hasTef 1
CLtefFactor 0.06
CDtefFactor 0.06
tefNStages 2
tefTakeoff 50
tefRate 5
lefRate 5
hasLef 2
lefGround -2
lefMaxAngle 20
lefMaxMach 0.4
lefNStages 1
CDlefFactor 0
CDSPDBFactor 0.08
CDLDGFactor 0.03
flapGearRelative 1
maxFlapVcas 220
flapVcasRange 40
area2Span 0.0355
rudderMaxAngle 20
aileronMaxAngle 20
elevonMaxAngle 20
airbrakeMaxAngle 60
hasSwingWing 0
isComplex 0
landingAOA 12.5
dragChuteCd 0
dragChuteMaxSpeed 170
rollCouple 0
elevatorRoll 1
canopyMaxAngle 20
canopyRate 5
fuelFlowFactorNormal 0.36
fuelFlowFactorAb 0.36
minFuelFlow 2360
fuelFwdRes 0
fuelAftRes 0
fuelFwd1 0
fuelAft1 0
fuelWingAl 0
fuelWingFr 0
fuelFwdResRate 0
fuelAftResRate 0
fuelFwd1Rate 0
fuelAft1Rate 0
fuelWingAlRate 0
fuelWingFrRate 0
fuelClineRate 0
fuelWingExtRate 0
fuelMinFwd 400
fuelMinAft 250
nChaff 30
nFlare 60
gunLocation 2 -2 0
nEngines 4
engine1Location -0.2 -61 1.4
engine2Location 13.4 -34.7 0
engine3Location 13.4 34.7 0
engine4Location -0.2 61 1.4
engineSmokes 0
wingTipLocation 0 0 0
refuelLocation 0 0 0
hardpoint1Grp 0
hardpoint2Grp 0
hardpoint3Grp 0
hardpoint4Grp 0
hardpoint5Grp 0
hardpoint6Grp 0
hardpoint7Grp 0
hardpoint8Grp 0
hardpoint9Grp 0
hardpoint10Grp 0
hardpoint11Grp 0
hardpoint12Grp 0
hardpoint13Grp 0
hardpoint14Grp 0
hardpoint15Grp 0
hardpoint16Grp 0
sndExt 231
sndWind 33
sndAbInt 40
sndAbExt 231
sndEject 5
sndSpdBrakeStart 141
sndSpdBrakeLoop 140
sndSpdBrakeEnd 139
sndSpdBrakeWind 142
sndOverSpeed1 191
sndOverSpeed2 192
sndGunStart 25
sndGunLoop 26
sndGunEnd 27
sndBBPullup 68
sndBBBingo 66
sndBBWarning 63
sndBBCaution 64
sndBBChaffFlareLow 184
sndBBFlare 138
sndBBChaffFlare 183
sndBBChaffFlareOut 185
sndBBAltitude 65
sndBBLock 67
sndTouchDown 42
sndWheelBrakes 132
sndDragChute 218
sndLowSpeed 167
sndFlapStart 145
sndFlapLoop 144
sndFlapEnd 143
sndHookStart 195
sndHookLoop 194
sndHookEnd 193
sndGearCloseStart 147
sndGearCloseEnd 146
sndGearOpenStart 149
sndGearOpenEnd 150
sndGearLoop 148
rollLimitForAiInWP 30
flap2Nozzle 0
refuelSpeed 255
refuelAltitude 20000
decelDistance 1000
followRate 20
desiredClosureFactor 0.35
IL78Factor 0
longLeg 60
shortLeg 25
refuelRate 50
AIBoomDistance 50
BingoReturnDistance 50
jokerFactor 19.1
bingoFactor 19.1
fumesFactor 105.1
maxRippleCount 0
largePark 1
Has_TFR 0
PID_K 0.6
PID_KI 0
PID_KD 0.3
TFR_LimitMX 0
TFR_Corner 350
TFR_Gain 0.015
EVA_Gain 5
TFR_MaxRoll 20
TFR_SoftG 2
TFR_MedG 4
TFR_HardG 6
TFR_Clearance 20
SlowPercent 0
TFR_lookAhead 2000
EVA1_SoftFactor 0.6
EVA2_SoftFactor 0.4
EVA1_MedFactor 0.8
EVA2_MedFactor 0.6
EVA1_HardFactor 1.2
EVA2_HardFactor 0.9
TFR_GammaCorrMult 0.5
LantirnCameraX 10
LantirnCameraY 2
LantirnCameraZ 5
MinTGTMAR 0
MaxMARIdedStart 0
AddMARIded5k 0
AddMARIded18k 0
AddMARIded28k 0
AddMARIdedSpike 0
PilotEyePos 73.4 -3.4 -11.5
// Camera TopGun by Revientor
// left wing looking towards cockpit
TopGunCamera1 7 -36.0 -124.7 -5.2 0.0 35.0 0.0 60.0
// right of cockpit looking toward pilots
TopGunCamera2 7 120.0 -124.7 -5.2 0.0 120.0 0.0 60.0
// before air intake looking backwards to gear..
TopGunCamera3 7 96.5 -0.0 9.0 -2.0 -180.0 0.0 60.0
// placed near the gun (created by Revient0R), looking backward..
//TopGunCamera4
TopGunCamera4 7 200.0 0.0 -49.0 -13.0 180.0 0.0 47.0
#
# End of Additional
#

END OF DATA