#Title:IL76A
#Author:SP2 Beta1
#Version:Engines, FF, 767wing
#MODIF MAV-JP / STORE LIMITER / TO BE USED WITH ASSOCIATED WCD
#
# SIMULATION INPUT PANEL
#
# INPUT MASS AND GEOMETRIC PROPERTIES:
        165347  # Empty Weight (lbs)
          3229  # Reference Area
        134258  # 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
           210  # Min Vcas
           650  # Max Vcas
           450  # Corner Vcas
             6  # Theta Max
             3  # Num Gear
# Gear X, Y, Z, Rng
            25             0            11           100
          80.5          -8.6            11           100
          80.5           8.6            11           100
#
# Physical data
          73.6  # CG Loc
           120  # Length
           185  # Span
             7  # Fus Radius
            20  # 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
#
             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
         50000
#
#    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 50000
             0             0             0             0             0             0             0             0             0             0
#
#    THRST2 - THRUST AT MIL POWER (THROTL = 1.00)
#
# Alt 0
       25666.2       22953.5       20866.8       18988.8         17476       16171.8       15128.5       14450.3       13928.6       13250.4
#
# Alt 5000
       21388.5       19301.8       17736.8       16797.8       16171.8       15024.1       14085.1       13563.4       12937.4       12363.6
#
# Alt 10000
       17736.8       15963.1       14606.8       13824.3       13198.3       13041.8       13041.8       12520.1       11998.4       11476.8
#
# Alt 20000
       11998.4       10955.1       9911.74       9390.07        8868.4       8764.07        8868.4       8972.74          8500          8000
#
# Alt 30000
       7825.06       6886.05       6364.38       6155.71       5842.71       5738.38       5738.38       5842.71          5400          5000
#
# Alt 36000
       5947.05       5477.54       4903.71       4695.04       4486.37       4382.03       4382.03       4486.37          4000          3500
#
# Alt 50000
             0             0             0             0             0             0             0             0             0             0
#
#    THRST3 - THRUST AT FULL AB (THROTL = 1.05)
#
# Alt 0
       25666.2       22953.5       20866.8       18988.8         17476       16171.8       15128.5       14450.3       13928.6       13250.4
#
# Alt 5000
       21388.5       19301.8       17736.8       16797.8       16171.8       15024.1       14085.1       13563.4       12937.4       12363.6
#
# Alt 10000
       17736.8       15963.1       14606.8       13824.3       13198.3       13041.8       13041.8       12520.1       11998.4       11476.8
#
# Alt 20000
       11998.4       10955.1       9911.74       9390.07        8868.4       8764.07        8868.4       8972.74          8500          8000
#
# Alt 30000
       7825.06       6886.05       6364.38       6155.71       5842.71       5738.38       5738.38       5842.71          5400          5000
#
# Alt 36000
       5947.05       5477.54       4903.71       4695.04       4486.37       4382.03       4382.03       4486.37          4000          3500
#
# Alt 50000
             0             0             0             0             0             0             0             0             0             0
#
#    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 33
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 0.2
CDtefFactor 1.1
tefNStages 2
tefTakeoff 30
tefRate 5
lefRate 5
hasLef 1
lefGround 15
lefMaxAngle 15
lefMaxMach 0.4
lefNStages 1
CDlefFactor 0.004
CDSPDBFactor 0.08
CDLDGFactor 0.03
flapGearRelative 0
maxFlapVcas 210
flapVcasRange 20
area2Span 0.0572
rudderMaxAngle 20
aileronMaxAngle 20
elevonMaxAngle 20
airbrakeMaxAngle 60
hasSwingWing 0
isComplex 0
landingAOA 8.5
dragChuteCd 0
dragChuteMaxSpeed 170
rollCouple -0.05
elevatorRoll 1
canopyMaxAngle 20
canopyRate 5
fuelFlowFactorNormal 0.716
fuelFlowFactorAb 0.716
minFuelFlow 5040
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 6 -32 0
engine2Location 13 -20 0
engine3Location 13 20 0
engine4Location 6 32 0
engineSmokes 2
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 280
refuelAltitude 20000
decelDistance 1000
followRate 20
desiredClosureFactor 0.35
IL78Factor 0
longLeg 60
shortLeg 25
refuelRate 50
AIBoomDistance 50
BingoReturnDistance 50
jokerFactor 21.4
bingoFactor 21.4
fumesFactor 122.5
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 47.4 -3.8 -3.7
// Camera TopGun by Revientor
// left wing looking towards cockpit
TopGunCamera1 7 -23.0 -80.2 -5.4 0.0 50.0 0.0 60.0
// right of cockpit looking toward pilots
TopGunCamera2 7 84.0 -80.2 -5.4 0.0 120.0 0.0 60.0
// before air intake looking backwards to gear..
TopGunCamera3 7 60.3 0.0 12.0 -2.0 -180.0 0.0 60.0
// placed near the gun (created by Revient0R), looking backward..
//TopGunCamera4
TopGunCamera4 7 135.0 -0.0 -38.8 -13.0 180.0 0.0 47.0
#
# End of Additional
#

END OF DATA