#Title:E2C
#Author:SP2 beta1
#Version:T56-A-427 engine, AN24 wing
#MODIF MAV-JP / STORE LIMITER / TO BE USED WITH ASSOCIATED WCD
#
# SIMULATION INPUT PANEL
#
# INPUT MASS AND GEOMETRIC PROPERTIES:
         40484  # Empty Weight (lbs)
          2000  # Reference Area
         12400  # Internal Fuel
#
#
# ANGLE OF ATTACK AND SIDESLIP LIMITS
            20  # AOA Max
            -5  # AOA Min
             5  # Beta Max
            -5  # Beta Min
             3  # Max G
            60  # Max Roll
           145  # Min Vcas
           385  # Max Vcas
           250  # Corner Vcas
             8  # Theta Max
             3  # Num Gear
# Gear X, Y, Z, Rng
           5.6             0           5.8           100
            24         -21.7           5.8           100
            24          21.7           5.8           100
#
# Physical data
          23.5  # CG Loc
          47.2  # Length
          80.7  # Span
           2.8  # Fus Radius
          18.4  # 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
#
       0.66666  # 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
#
             2  # 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
#
10   # Number of Alt Break Points
             0          5000         10000         15000         20000         25000
         30000         35000         40000         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 15000
             0             0             0             0             0             0             0             0             0             0
#
# Alt 20000
             0             0             0             0             0             0             0             0             0             0
#
# Alt 25000
             0             0             0             0             0             0             0             0             0             0
#
# Alt 30000
             0             0             0             0             0             0             0             0             0             0
#
# Alt 35000
             0             0             0             0             0             0             0             0             0             0
#
# Alt 40000
             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
         18700         18700         11111          7164          5707          4979          4311          4129          3643          3521
#
# Alt 5000
         15361         15361          8500          6132          5100          4554          4129          3764          3582          3461
#
# Alt 10000
         12689         12689          6861          4979          4250          3764          3704          3582          3218          3036
#
# Alt 15000
         10321         10321          5586          4189          3521          3157          3036          2975          2975          2914
#
# Alt 20000
          8439          8439          4432          3279          2975          2671          2550          2429          2429          2489
#
# Alt 25000
          6739          6739          3704          2732          2307          2125          2064          1943          1943          1943
#
# Alt 30000
          5404          5404          3036          2125          1761          1700          1639          1579          1579          1579
#
# Alt 35000
          4068          4068          2368          1518          1214          1275          1214          1214          1214          1214
#
# Alt 40000
          2732          2732          1700           911           668           850           789           850           850           850
#
# Alt 45000
          1396          1396          1032           304           121           425           364           486           486           486
#
#    THRST3 - THRUST AT FULL AB (THROTL = 1.05)
#
# Alt 0
         18700         18700         11111          7164          5707          4979          4311          4129          3643          3521
#
# Alt 5000
         15361         15361          8500          6132          5100          4554          4129          3764          3582          3461
#
# Alt 10000
         12689         12689          6861          4979          4250          3764          3704          3582          3218          3036
#
# Alt 15000
         10321         10321          5586          4189          3521          3157          3036          2975          2975          2914
#
# Alt 20000
          8439          8439          4432          3279          2975          2671          2550          2429          2429          2489
#
# Alt 25000
          6739          6739          3704          2732          2307          2125          2064          1943          1943          1943
#
# Alt 30000
          5404          5404          3036          2125          1761          1700          1639          1579          1579          1579
#
# Alt 35000
          4068          4068          2368          1518          1214          1275          1214          1214          1214          1214
#
# Alt 40000
          2732          2732          1700           911           668           850           789           850           850           850
#
# Alt 45000
          1396          1396          1032           304           121           425           364           486           486           486
#
#    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             1
# 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 38
rollMomentum 1.3
pitchMomentum 1.3
yawMomentum 1.3
pitchElasticity 1
gearPitchFactor 0
rollGearGain 1
yawGearGain 1
pitchGearGain 1
sinkRate 25
tefMaxAngle 50
hasFlapperons 0
hasTef 1
CLtefFactor 0.1
CDtefFactor 0.1
tefNStages 5
tefTakeoff 30
tefRate 5
lefRate 5
hasLef 1
lefGround 20
lefMaxAngle 20
lefMaxMach 0.4
lefNStages 1
CDlefFactor 0.004
CDSPDBFactor 0.08
CDLDGFactor 0.03
flapGearRelative 1
maxFlapVcas 150
flapVcasRange 20
area2Span 0.0403
rudderMaxAngle 20
aileronMaxAngle 20
elevonMaxAngle 20
airbrakeMaxAngle 60
hasSwingWing 0
isComplex 0
landingAOA 12.5
dragChuteCd 0
dragChuteMaxSpeed 170
rollCouple -0.05
elevatorRoll 1
canopyMaxAngle 20
canopyRate 5
fuelFlowFactorNormal 0.501
fuelFlowFactorAb 0.501
minFuelFlow 1200
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 2
engine1Location -6.5 -11 -2
engine2Location -6.5 11 -2
engine3Location 0 0 0
engine4Location 0 0 0
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 242
sndWind 33
sndAbInt 40
sndAbExt 242
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 200
refuelAltitude 17000
decelDistance 2500
followRate 20
desiredClosureFactor 0.35
IL78Factor 0
longLeg 60
shortLeg 25
refuelRate 50
AIBoomDistance 50
BingoReturnDistance 50
jokerFactor 9.2
bingoFactor 9.2
fumesFactor 71.6
maxRippleCount 0
largePark 0
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 16.1 -1.5 -2.7
animEngineRPMMult 1000
// Camera TopGun by Revientor
// left wing looking towards cockpit
TopGunCamera1 7 -3.0 -43.7 -8.4 0.0 60.0 0.0 60.0
// right of cockpit looking toward pilots
TopGunCamera2 7 27.0 -43.7 -8.4 0.0 120.0 0.0 60.0
// before air intake looking backwards to gear..
TopGunCamera3 7 23.0 0.0 4.4 -2.0 -180.0 0.0 60.0
// placed near the gun (created by Revient0R), looking backward..
//TopGunCamera4
TopGunCamera4 7 70.0 -0.0 -11.5 -13.0 180.0 0.0 47.0
#
# End of Additional
#

END OF DATA