//********************************************************************
//                     Dassault/Dornier AlphaJet                    
//                         version fs9-11b                           
//                           2004 fev 01                            	
//********************************************************************


[fltsim.0]
title=Alpha Jet-E r
sim=alphajet
model=
panel=
sound=
texture=
checklists=
kb_checklists=alphajet_check
kb_reference=alphajet_ref
atc_id=F-TERP
atc_id_color=
ui_manufacturer=Dassault/Dornier
ui_type=Alpha Jet-E
ui_variation=Patrouille de FRANCE 
description=Modele par lco26\nlco26@wanadoo.fr\nTableau de bord par Jean-Pierre Langer\nfichier air version FS9-11 \nJean-Pierre Bourgeois "BeeGee"\bourgeoisjpierre@free.fr\nBenoit M. Dube\ndube_benoit_m@yahoo.fr  \nSonny\nhttp:\/\/sonny3.free.fr\/\n2004  fev. 01\n\n
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=1

[fltsim.1]
title=Alpha Jet-E 1r
sim=alphajet
model=
panel=
sound=
texture=2
checklists=
kb_checklists=alphajet_check
kb_reference=alphajet_ref
atc_id=F-TERP
atc_id_color=
ui_manufacturer=Dassault/Dornier
ui_type=Alpha Jet-E
ui_variation=Patrouille de FRANCE 
description=Modele par lco26\nlco26@wanadoo.fr\nTableau de bord par Jean-Pierre Langer\nfichier air version FS9-11 \nJean-Pierre Bourgeois "BeeGee"\bourgeoisjpierre@free.fr\nBenoit M. Dube\ndube_benoit_m@yahoo.fr  \nSonny\nhttp:\/\/sonny3.free.fr\/\n2004  fev. 01\n\n
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=1


[fltsim.2]
title=Alpha Jet-E 3r
sim=alphajet
model=
panel=
sound=
texture=3
checklists=
kb_checklists=alphajet_check
kb_reference=alphajet_ref
atc_id=F-TERP
atc_id_color=
ui_manufacturer=Dassault/Dornier
ui_type=Alpha Jet-E
ui_variation=Patrouille de FRANCE 
description=Modele par lco26\nlco26@wanadoo.fr\nTableau de bord par Jean-Pierre Langer\nfichier air version FS9-11 \nJean-Pierre Bourgeois "BeeGee"\bourgeoisjpierre@free.fr\nBenoit M. Dube\ndube_benoit_m@yahoo.fr  \nSonny\nhttp:\/\/sonny3.free.fr\/\n2004  fev. 01\n\n
atc_heavy=0
atc_airline=
atc_flight_number=
visual_damage=1
[General]
performance=Avion d'entrainement avancé \nEnvergure....... 9.14 m  ( 30 ft )  \nLongueur........ 12.3 m ( 40 ft, 3 in )  \nHauteur......... 4.19 m ( 13 ft 09 in ) \nMasse a vide.... 3,515 kg ( 7,374 lb )\nMasse max decol. 8,000 kg ( 17,637 lb )  \nMoteurs......... 2 * SNECMA\/Turbomeca Larzac 04-C6 turbofans\nPoussée......... 26.48 kN ( 5,952 lb ) total  \nVitesse max..... 1,160 km\/h \/ 0.8 Mach  \nCarburant....... 1520 kg \nCharge.......... 2200kg \n\nRayon d'action.. 2,600 km \/ 1330nm (reservoirs externes)  \nPlafond......... 13700 m \/ 50.000 feet  \nDistance decol.. 400 m  \nDistance atter.. 520 m  \n\nEquipage........ 2 pilotes\n
atc_type=
atc_model=
Category=airplane



[SMOKESYSTEM]
smoke.0=-10.00, -0.70, 0.0, fx_smoke_r
//smoke.0=-100.00, -11.00, -2.00, alphajet_r
//smoke.1=-100.00, -11.00, -2.00, alphajet_w
//smoke.2=-100.00, -11.00, -2.00, alphajet_b



[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=-1.00000,0.000000,0.000000

max_number_of_stations=50
station_load.0=185.0,10.000000,0.000000,0.000000
station_load.1=0.000,5.000000,0.000000,0.000000

empty_weight=7374.000000                              // (livres) masse à vide

empty_weight_roll_MOI=14000.000000                    // moment d'inertie roulis
empty_weight_pitch_MOI=40000.000000                   // moment d'inertie tangage
empty_weight_yaw_MOI=72000.000000                     // moment d'inertie lacet
empty_weight_coupled_MOI=0.000000                     // moment d'inertie couplé

max_gross_weight= 17637

[fuel]
//--------Av./Arr.--gau./droit----vert.------Capacite-------Non util--
//         pieds       pieds      pieds       gallons       gallons

Center1   =-1.000000,  0.000000,   0.00000,   330.00000,    0.000000
LeftMain  =-1.000000,  -5.000000,  0.000000,  41.00000,    0.000000
RightMain=-1.000000,  5.000000,  0.000000,   41.00000,    0.000000
//Left_tip=-1.000000,  -9.5, 0.00,81.80,0.00
//Right_tip=-1.000000,  9.5, 0.00,81.80,0.00
fuel_type=2.000000            // type carburant : 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=2


[flight_tuning]
cruise_lift_scalar     = 1.0
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness  = 1.0
rudder_effectiveness   = 1.0
pitch_stability        = 1.0
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0

[airplane_geometry]
                                       // Ailes
                                       // -----
wing_area=200.000000                   // (pieds carrés) surface ailaire
wing_span=30.000000                    // (pieds) envergure
wing_root_chord=10.400000               // (pieds) corde à l'emplanture
wing_dihedral=0.000000                 // (degrés) dièdre
wing_incidence=0.000000                // (degrés) incidence à l'emplanture
wing_twist=-1.499634                   // (degrés) vrillage
oswald_efficiency_factor=0.900      // mesure de l'efficacité de la portance de l'aile  2.417461 
wing_winglets_flag=0                   // ailerettes disponibles? 0=non, 1=oui
wing_sweep=26.000000                   // (degrés) flèche
wing_pos_apex_lon=4.30            // (pieds)  0.019170
wing_pos_apex_vert=0.000000            // (piedsw)
                                       // stablisateur
                                       // -------------
htail_area=55.000000                   // (pieds carrés) surface stabilisateur
htail_span=14.500000                   // (pieds) envergure stabilisateur
htail_pos_lon=-20.333333               // (pieds) position longi. stabilisateur
htail_pos_vert=0.000000                // (pieds) position vet. stabilisateur
htail_incidence=0.000000               // (degrés) incidence stabilisateur
htail_sweep=26.000000                  // (degrés) flèche
                                       // Dérive
                                       // ------
vtail_area=100.000000                  // (pieds carrés) surface dérive
vtail_span=11.401754                   // (pieds) hauteur dérive
vtail_sweep=26.000000                  // (pieds) flèche dérive
vtail_pos_lon=-16.333333               // (pieds) position longi. dérive
vtail_pos_vert=8.166667                // (pieds) position vert. dérive
                                       // surfaces des gouvernes
                                       // ----------------------  
elevator_area=7.500000                 // (pieds carrés) gouverneprofondeur
aileron_area=6.880000                  // (pieds carrés) ailerons
rudder_area=3.400000                   // (pieds carrés) gouverne direction
elevator_up_limit=28.647890            // (degrés) limite sup. profondeur
elevator_down_limit=28.647890          // (degrés) limite inf. profondeur
aileron_up_limit=17.761692             // (degrés) limite sup. aileron
aileron_down_limit=17.761692           // (degrés) limite inf. aileron
rudder_limit=22.918312                 // (degrés) limite gouv. direction
elevator_trim_limit=19.480565          // (degrés) limite compensateur profondeur
spoiler_limit=59.988681                // (degrés) limite aérofreins
spoilerons_available=0                 // aileron aérofrein disponible? 0=non, 1=oui
aileron_to_spoileron_gain=0.000000     // gain aileon - aérofrein
min_ailerons_for_spoilerons=0.000000   // (degrés) 
min_flaps_for_spoilerons=0.000000      // position min. volets pour action aileron aérofrein
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=14.957265
positive_g_limit_flaps_down=4.914530
negative_g_limit_flaps_up=-12.820513
negative_g_limit_flaps_down=-4.059829

[contact_points]
//0  Classe
//1  Position longitudinale       (pieds)
//2  Position latérale            (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               (degrés)
//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 rentrée train          (secondes)
//13 Sound Type

// Train  0    1      2        3        4       5         6      7          8         9        10         11       12        13        14        15
point.0=1, 12.15, 0.000,-5.50, 2600,  0, 0.354715, 30, 0.250000, 4.00, 0.577863, 3.5,  4.5,  0,0.000000,0.000000 // roulette av avec palonnier.
//point.0=1, 12.15, 0.000,-5.50, 2600,  0, 0.354715, 180, 0.250000, 4.00, 0.577863, 3.5,  4.5,  0,0.000000,0.000000 // roulette av libre.
point.1=1, -2.50,-4.1,-5.10,     2600,  1, 0.574715,  0, 0.390256, 2.50, 0.577863, 4.5,  5.5,  2,0.000000,0.000000
point.2=1, -2.50, 4.1,-5.10,     2600,  2, 0.574715,  0, 0.390256, 2.50, 0.577863, 5.0,   6.0, 3,0.000000,0.000000

// 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

static_pitch=2.1            
static_cg_height=5.2
gear_system_type=0

[Flaps.0]
type=1                                  // 1=bord de fuite, 2=bord d'attaque
span-outboard=0.500000                  // 0.0, ..., 1.0
extending-time=5.000000                 // (secondes)
system_type=0
flaps-position.0=0.000000,0.000000      // (degrés)
flaps-position.1=19.999092,0.000000     // (degrés)
flaps-position.2=39.998184,0.000000     // (degrés)
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar=1.0                         // scalaire portance
drag_scalar=1.0                         // scalaire trainée
pitch_scalar=1.0                        // scalaire effet tangage

[GeneralEngineData]
engine_type=1                           // 0=Piston, 1=Jet, 2=Aucun, 3=Helo-Turbine, 4=Fusée, 5=Turboprop
Engine.0=-6.666667,-0.833333,0.00  // (pieds) position moteur 1 longitudinale, latérale, verticale par rapport au point ref. 
Engine.1=-6.666667,0.833333,0.00    // (pieds) position moteur 2 longitudinale, latérale, verticale par rapport au point ref.
fuel_flow_scalar=0.69600              // scalaire pour efficacité débit carburant
min_throttle_limit=0.000000

[TurbineEngineData]
fuel_flow_gain=0.025000                 // Gain débit carburant
inlet_area=2.000000                     // (pieds carrés) surface entrée air
rated_N2_rpm=29920.000000               // (tours/minute) valeur nominale vit. rotation 2-ème étage 29920 compresseur
static_thrust=2975.000000               // (livres) poussée nominale statique max au niveau de la mer
afterburner_available=0                 // réchauffe disponible? 0=non, 1=oui
reverser_available=0                    // inverseur poussée disponible? 0=non, 1=oui

[jet_engine]
thrust_scalar = 1.0

[Reference Speeds]
flaps_up_stall_speed=116.000000          // (noeuds) vitesse vraie      
full_flaps_stall_speed=92.800000         // (noeuds) vitesse vraie
cruise_speed=420                // (noeuds) vitesse vraie
max_indicated_speed=550.000000
max_mach=0.950000

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

[Views]
eyepoint= 9.900000,0.000000,0.480000     

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit,  5=landing
light.0=3,  -3.60, -14.80, -0.4, fx_navred ,
light.1=3,  -3.60,  14.80, -0.4, fx_navgre ,
light.2=3, -19.10,   0.00, 1.30, fx_navwhi ,
light.3=4,  10.00,   0.00, 1.20, fx_vclighth,
light.4=2,  -3.50, -14.75,-0.39, fx_strobe ,
light.5=2,  -3.50,  14.75,-0.39, fx_strobe ,
light.6=2, -10.90,   0.00,-1.10, fx_beaconb ,
light.7=1,  -9.80,   0.00, 2.50, fx_beaconh ,
light.8=5,  18.69,   0.00,-2.25, fx_landing,


[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

   
[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
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0

[direction_indicators]
// 1  type: 0=Aucun, 1=Gyro Vide, 2=Gyro electrique, 3=electro-mag asservi compas, 4=asservi à 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


[electrical]
max_battery_voltage=24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=60.0

[brakes]
toe_brakes_scale=2.0
parking_brake=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000

[exits] 
number_of_exits = 2
exit_rate.0 = 0.4
exit_rate.1=0.4

[stall_warning]
type=1
stick_shaker=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0
