[fltsim.0]
title=Alpha Jet-E Belgian Air Aerobatics
sim=Alphaero
model=
panel=
sound=
texture=
checklists=
kb_checklists=alphajet_check
kb_reference=alphajet_ref
atc_id=AT26 
atc_id_color=
atc_heavy=0
atc_airline=Air Force
atc_flight_number=2446
ui_manufacturer=Dassault/Dornier
ui_type=Alpha Jet-E
ui_variation=BAF Aerobatics 

description=Modele par lco26\[email protected]\nhttp:\/\/perso.wanadoo.fr/lco\nfichier air version b3 bis \nBenoit M. Dube\[email protected]\net Sonny\nhttp:\/\/sonny3.free.fr\/\n2002  oct. 16\n\n

[General]
performance=Max speed Mach 1.35\nMinimum landing speed 100 Knts \nDesigned for aerobatics \nMax alt 45.000 feet\nFlight Dynamics By: Alejandro Villa


[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[SMOKESYSTEM]

smoke.0=-1.00, -5.00, 3.750, fx_smoke_rx
smoke.1=-1.00, -5.00, -3.750, fx_smoke_rx
smoke.2=-1.00, -5.00, 0.000, fx_smoke_red
smoke.3=-0.30, -3.70, 14.10, fx_WingVortex
smoke.4=-0.30, -3.70, -14.10, fx_WingVortex 


[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1


[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=15000.000000
empty_weight_roll_MOI=135000.000000
empty_weight_pitch_MOI=262662.000000
empty_weight_yaw_MOI=373480.000000
empty_weight_coupled_MOI=1300.000000

[fuel]
Center1=0.000000,0.000000,0.000000,200.000000,0.000000
LeftMain=0.000000,0.000000,0.000000,100.000000,0.000000
RightMain=0.000000,0.000000,0.000000,100.000000,0.000000
LeftAux=0.000000,0.00000,0.000000,50.000000,0.000000
RightAux=0.000000,0.00000,0.000000,50.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1



[airplane_geometry]
wing_area=608.000000
wing_span=46.666667
wing_root_chord=13.000000
wing_dihedral=-0.049438
wing_incidence=-0.494385
wing_twist=-0.999756
oswald_efficiency_factor=1.000000
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=80.000000
htail_span=20.000000
htail_pos_lon=-14.166667
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=140.000000
vtail_span=13.490738
vtail_sweep=0.000000
vtail_pos_lon=-14.333333
vtail_pos_vert=5.833333
elevator_area=16.250000
aileron_area=11.920000
rudder_area=12.750000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=99.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000


[contact_points]
//0  Classe
//1  Position longitudinale       (pieds)
//2  Position latйrale            (pieds)
//3  Position verticale           (pieds)
//4  Seuil dommage impac          (pieds/minute)
//5  Freins                       (0=aucun, 1=Gauche, 2=Droit)
//6  Rayon roues                  (pieds)
//7  angle braquage               (degrйs)
//8  Compression statiqu          (pieds) (0 si rigide)
//9  Ratio compression statique/max
//10 Ratio amortissement          (0=non amortie, 1=amortissement critique)
//11 Temps de sortie train        (secondes)
//12 Temps rentrйe train          (secondes)
//13 Sound Type

// Train               1         2        3           4          5         6         7          8         9        10         11       12        13        14        15
point.0=1.000000, 12.500000, 0.000000,-5.306667, 2776.282603, 0.000000, 0.574715, 39.000000, 0.507873, 2.500000, 1.317230, 5.000000, 5.000000, 0.000000,0.000000,0.000000 // roulette av.
point.1=1.000000, -3.500000,-5.083333,-5.263333, 2776.282603, 1.000000, 0.574715,  0.000000, 0.390256, 2.500000, 0.577863, 5.000000, 5.000000, 2.000000,0.000000,0.000000
point.2=1.000000, -3.500000, 5.083333,-5.263333, 2776.282603, 2.000000, 0.574715,  0.000000, 0.390256, 2.500000, 0.577863, 5.000000, 5.000000, 3.000000,0.000000,0.000000
// points de contact    1         2        3          4          5         6          7         8         9         10        11        12        13       14        15
point.3=2.000000,   0.000000,-15.583333,0.666667,1574.803150,0.000000,0.000000,   0.000000,  0.000000, 0.000000,0.000000,  0.000000, 0.000000, 5.000000,0.000000,0.000000
point.4=2.000000,   0.000000, 15.583333,0.666667,1574.803150,0.000000,0.000000,   0.000000,  0.000000, 0.000000,0.000000,  0.000000, 0.000000, 6.000000,0.000000,0.000000
point.5=2.000000, -15.666667, 0.000000,-0.166667,1574.803150,0.000000,0.000000,   0.000000,  0.000000, 0.000000,0.000000,  0.000000, 0.000000, 9.000000,0.000000,0.000000
point.6=2.000000,   8.000000, 0.000000,-0.166667,1574.803150,0.000000,0.000000,   0.000000,  0.000000, 0.000000,0.000000,  0.000000, 0.000000, 4.000000,0.000000,0.000000
point.7=4.000, -7.000, -4.250, -2.400, 1068.000, 0.000, 0.512, 20.000, 0.800, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.0
point.8=4.000, -7.000, 4.250, -2.400, 1068.000, 0.000, 0.512, 20.000, 0.800, 2.500, 0.700, 0.000, 0.000,1.000, 0.000, 0.0
point.9=4.000, 5.350, -4.250, -2.450, 1068.000, 1.000, 0.512, 0.000, 0.800, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.0
point.10=4.000, 5.350, 4.250, -2.450, 1068.000, 2.000, 0.512, 0.000, 0.800, 2.500, 0.700, 0.000,0.000, 3.000, 0.000, 0.0
static_pitch=0.000000               
static_cg_height=3.003744



[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=6.665409,0.000000
flaps-position.2=13.330818,0.000000
flaps-position.3=19.996227,0.000000
flaps-position.4=26.661636,0.000000
flaps-position.5=33.327045,0.000000
flaps-position.6=39.992454,0.000000


[GeneralEngineData]
engine_type=1
Engine.0=-19.583333,0.000000,-0.083333
Engine.1= 00.000000,0.000000,0.000000
fuel_flow_scalar=0.010000

[TurbineEngineData]
fuel_flow_gain=1.500---------------1.002
inlet_area=44.486640
rated_N2_rpm=32920.000000
static_thrust=32072.200000
afterburner_available=1
reverser_available=1

//[TurbineEngineData]
//fuel_flow_gain=0.002170
//inlet_area=44.486640
//rated_N2_rpm=29920.000000
//static_thrust=34072.200000
//afterburner_available=1
//reverser_available=1

[jet_engine]
thrust_scalar = 1.0

[Reference Speeds]
flaps_up_stall_speed=70.000000
full_flaps_stall_speed=56.000000
cruise_speed=812.160408

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=9.356666,0.000000,1.300000

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit,  5=landing
light.0=3,   -3.70, -14.10, -0.30, fx_navred
light.1=3,   -3.70,  14.10, -0.30, fx_navgre
light.2=3,  -18.70,   0.00,  1.00, fx_navwhi
light.3=4,   10.00,   0.00,  0.00, fx_vclight
light.4=4,    6.00,   0.00,  0.00, fx_vclight
light.5=2,   -3.70, -14.10, -0.30, fx_strobeh
light.6=2,   -3.70,  14.10, -0.30, fx_strobeh
light.7=2,  -10.90,   0.00, -1.10, fx_beaconb 
light.8=1,   -9.80,   0.00,  2.20, fx_beaconh
light.9=5,  4.0,   4.00,  -3.00, Newll,
light.10=5,  4.0,   -4.00,  -3.00, Newll,
light.11=5,  -15.00,   1.00,  1.50, Newll,
light.12=5,  -15.00,   -1.00,  1.50, Newll,
light.13=5,  0.00,   3.00,  3.50, Newll,
light.14=5,  0.00,   -3.00,  3.50, Newll,

////////////jet flame effects
light.15=3,  -10.00,  -1.80,  -1.52, fx_flankerflame
light.16=3, -10.00,   1.80,  -1.52, fx_flankerflame
//////////afterburner effects
light.17=2, -13.30,  -1.80,  -1.52, fx_flankerburner
light.18=2, -13.30,   1.80,  -1.52, fx_flankerburner

   
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
use_no_default_bank=1


[direction_indicators]
// 1  type: 0=Aucun, 1=Gyro Vide, 2=Gyro electrique, 3=electro-mag asservi compas, 4=asservi а un autre
// 2  no. type indicateur asservie dans le cas type 4
direction_indicator.0=3,0


[forcefeedback]
stick_shaker_magnitude=1000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
gear_bump_nose_magnitude=3000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=2700           ; 0 - 10000
gear_bump_left_direction=9000           ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=27000         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=1300            ; 0 - 10000
ground_bumps_angle1=08900               ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200             ; 0 - 10000
ground_bumps_angle2=09100               ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000                  ; 0 - 10000
crash_direction1=01000                  ; 0 - 35999 degrees
crash_magnitude2=10000                  ; 0 - 10000
crash_direction2=9000                   ; 0 - 35999 degrees
crash_period2=75000                     ; in microseconds
crash_duration2=2500000                 ; in microseconds