//+------------------------------------------------------------------+
//| Dassault/Dornier AlphaJet |
//| version b3 bis |
//| 2002 0ct. 16 |
//+------------------------------------------------------------------+
[fltsim.0]
title=Alpha Jet-E ,Ecole de chasse, Tours
sim=alphajet
model=
panel=
sound=
texture=
checklists=
kb_checklists=alphajet_check
kb_reference=alphajet_ref
atc_id=
atc_id_color=
ui_manufacturer=Dassault/Dornier
ui_type=Alpha Jet-E
ui_variation=E.A.C
description=Modele par lco26\nlco26@wanadoo.fr\nhttp:\/\/perso.wanadoo.fr/lco\nfichier air version b3 bis \nBenoit M. Dube\ndube_benoit_m@yahoo.fr\net Sonny\nhttp:\/\/sonny3.free.fr\/\n2002 oct. 16\n\n
atc_heavy=0
atc_airline=Air force
atc_flight_number=314LL
[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=
[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=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
[fuel]
//--------Av./Arr.--gau./droit----vert.------Capacite-------Non util--
// pieds pieds pieds gallons gallons
LeftMain=0.000000, -5.000000, 0.000000, 254.000000, 0.000000
RightMain=0.000000, 5.000000, 0.000000, 254.000000, 0.000000
fuel_type=2.000000 // type carburant : 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
[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=9.000000 // (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=2.417461 // mesure de l'efficacité de la portance de l'aile
wing_winglets_flag=0 // ailerettes disponibles? 0=non, 1=oui
wing_sweep=26.000000 // (degrés) flèche
wing_pos_apex_lon=0.019170 // (pieds)
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
[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 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
static_pitch=0.000000
static_cg_height=3.003744
[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,-1.083333 // (pieds) position moteur 1 longitudinale, latérale, verticale par rapport au point ref.
Engine.1=0.000000,0.833333,-1.083333 // (pieds) position moteur 2 longitudinale, latérale, verticale par rapport au point ref.
fuel_flow_scalar=1.000000 // scalaire pour efficacité débit carburant
[TurbineEngineData]
fuel_flow_gain=0.025000 // Gaim 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 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=425.904679 // (noeuds) vitesse vraie
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[Views]
eyepoint=9.356666,0.000000,2.300000
[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
[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
[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
