//+------------------------------------------------------------------+ //| Dassault/Dornier AlphaJet | //| version b3 bis | //| 2002 0ct. 16 | //+------------------------------------------------------------------+ [fltsim.0] title=Alpha Jet-E 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\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= atc_flight_number= [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= [SMOKESYSTEM] smoke.0=-100.00, -20.00, -2.00, fx_smoke_r [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,-5.366667, 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=9.356666,0.000000,1.300000 [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 [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