;****************************************************************************** ;* Le Dewoitine 520, chasseur français de la 2ème guerre mondiale * ;* Version 4 * ;* Pour Flight Simulator 2002 * ;* Modèle et textures par Jean-Marie MERMAZ * ;* jmmermaz@wanadoo.fr - http://perso.wanadoo.fr/jm.mermaz/aviation.htm * ;****************************************************************************** [fltsim.0] title=Dewoitine 520 "Groupe Doret" sim=Dewoitine520 model=CHAUVIERE panel= sound= texture= kb_checklists= kb_reference= editable=0 atc_id=001 atc_airline= atc_flight_number=xxx atc_heavy=0 ui_manufacturer=Dewoitine ui_type=D 520 ui_variation=Groupe Doret visual_damage=1 description=Dewoitine 520 du Groupe Doret, octobre 1944 à Toulouse (Couleurs Françaises et bandes d'invasion sur camouflage Allemand). [fltsim.1] title=Dewoitine 520 "Loup Garou" sim=Dewoitine520 model=RATIER panel= sound= texture=lg kb_checklists= kb_reference= editable=0 atc_id=73 atc_airline= atc_flight_number=73 atc_heavy=0 ui_manufacturer=Dewoitine ui_type=D 520 ui_variation=Loup Garou visual_damage=1 description=Dewoitine 520 N°73 « Loup Garou », 2ème escadrille du GC I/3. Avril 1940 à Cannes. [fltsim.2] title=Dewoitine 520 "GC II/7 juin 40" sim=Dewoitine520 model=RATIER panel= sound= texture=GCII7a kb_checklists= kb_reference= editable=0 atc_id=73 atc_airline= atc_flight_number=248 atc_heavy=0 ui_manufacturer=Dewoitine ui_type=D 520 ui_variation=GC II/7 juin 40 visual_damage=1 description=Dewoitine 520 N°248 du GC II/7 fin 1940. [fltsim.3] title=Dewoitine 520 "GC II/7 Vichy" sim=Dewoitine520 model=RATIER panel= sound= texture=GCII7b kb_checklists= kb_reference= editable=0 atc_id=73 atc_airline= atc_flight_number=248 atc_heavy=0 ui_manufacturer=Dewoitine ui_type=D 520 ui_variation=GC II/7 Vichy visual_damage=1 description=Dewoitine 520 N°248 du GC II/7 fin 1940 aux couleurs de Vichy en 1941. [fltsim.4] title=Dewoitine 520 "Corps franc Pommiès" sim=Dewoitine520 model=CHAUVIERE panel= sound= texture=cfp kb_checklists= kb_reference= editable=0 atc_id=73 atc_airline= atc_flight_number=xxx atc_heavy=0 ui_manufacturer=Dewoitine ui_type=D 520 ui_variation=cfp visual_damage=1 description=Dewoitine 520 du « Corps Franc Pommiès » (Couleurs Françaises et bandes d'invasion sur camouflage Allemand). [General] atc_model= editable=1 performance=Longueur : 8.76 m\nEnvergure : 10.20 m\nHauteur posé au sol : 2.57 m\nPoids max au décollage : 2790 Kg\nPuissance : 935 Cv\nVi. max à 6750m : 535 Km\/H\nVi. de croisière à 4000m : 400 Km:h\nVi. en piqué : 800 Km\/h\nVi. d'atterrissage : 130 Km\/h\nDistance franchissable : 1530 Km\nRayon d'action normal : 998 Km\nVitesse d'ascension : 720 m\/mn\nPlafond pratique : 10250 m\nMoteur en V Hispano-Suiza 12Y-45 de 935CV.\nhélice tripale métallique de 3,00 m de diamètre (Ratier, type 1606M,à commande de pas électrique, du n° 1 à 350), ou 1 Chauvière, type 3981, à commande pneumatique à partir du n° 351) un canon Hispano HS 404 de 20 mm avec 60 obus et 4 mitrailleuses MAC 1934-M39 de 7.5 dans chaque aile avec 675 cartouches.\nDesigner : Jean-Marie MERMAZ\n atc_type= [WEIGHT_AND_BALANCE] empty_weight = 2090.000 reference_datum_position = 0.500, 0.000, 0.000 empty_weight_CG_position = 0.100, 0.000, 0.000 max_number_of_stations = 50 station_load.0 = 170.000, -4.000, 0.000, 3.000 ;Moments of Inertia empty_weight_pitch_MOI = 2686.000 empty_weight_roll_MOI = 1628.000 empty_weight_yaw_MOI = 3426.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 2750.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar =1.000 parasite_drag_scalar =1.000 induced_drag_scalar =1.000 elevator_effectiveness =1.201 aileron_effectiveness =1.301 rudder_effectiveness =1.000 pitch_stability =1.801 roll_stability =1.201 yaw_stability =1.201 elevator_trim_effectiveness =1.500 aileron_trim_effectiveness =1.000 rudder_trim_effectiveness =1.000 [piston_engine] power_scalar =1.000 cylinder_displacement= 125.857 compression_ratio= 6.500 number_of_cylinders= 12 max_rated_rpm= 2800.000 max_rated_hp= 935.000 fuel_metering_type= 0 cooling_type= 0 normalized_starter_torque= 0.035 turbocharged= 1 max_design_mp= 39.000 min_design_mp= 1.000 critical_altitude= 14400.000 emergency_boost_type= 0 emergency_boost_mp_offset= 0.000 emergency_boost_gain_offset= 0.000 fuel_air_auto_mixture= 0 auto_ignition= 0 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [propeller] thrust_scalar =1.000 propeller_type= 0 propeller_diameter= 9.500 propeller_blades= 3 propeller_moi= 22.500 beta_max= 45.000 beta_min= 25.000 min_gov_rpm= 1400.000 prop_tc= 0.010 gear_reduction_ratio= 1.710 fixed_pitch_beta= 0.000 low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 0 prop_feathering_available= 0 prop_auto_feathering_available= 0 min_rpm_for_feather= 0.000 beta_feather= 0.000 power_absorbed_cf= 0.000 defeathering_accumulators_available= 0 prop_reverse_available= 0 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second [electrical] max_battery_voltage = 24.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps = 60.0 [contact_points] point.0= 1.000, -17.500, 0.000, -1.68, 3200.000, 0.000, 0.500, 60.000, 0.200, 2.500, 0.800, 7.500, 5.000, 0.000, 0.000, 0.000 point.1= 1.000, 1.000, -4.400, -5.82, 2200.000, 1.000, 1.050, 0.000, 0.500, 2.500, 0.830, 2.500, 4.000, 2.000, 0.000, 0.000 point.2= 1.000, 1.000, 4.400, -5.82, 2200.000, 2.000, 1.050, 0.000, 0.500, 2.500, 0.830, 2.500, 8.250, 3.000, 0.000, 0.000 point.3= 2.000, 0.000, -20.000, -0.500, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, 0.000, 20.000, -1.250, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -20.250, 0.000, 1.000, 2400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 2.410, 0.000, -2.080, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= 12.475 static_cg_height= 5.200 [SMOKESYSTEM] smoke.0=0.00, -0.70, 1.40, fx_smoke_w [Views] eyepoint=-5.5,0,2.6 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -0.2, -16.7, -0.1, fx_navred light.1=3, -0.2, 16.7, -0.1, fx_navgre light.2=3, -16.3, -0.3, 5, fx_navwhi light.3=3, -16.3, 0.2, 5, fx_navwhi light.5=4,-3.6, 0, 2.9, fx_vclight light.5=4,-3.6, 0, 3, fx_vclight [fuel] Center1= .6, 0.000, 0.000, 104.000, 0.000 LeftMain= 0, 0, 0, 0, 0.000 RightMain= 0, 0, 0, 0, 0.000 External1= -0, 0, 0, 0, 0.000 fuel_type=1.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area= 171.900 wing_span= 39.417 wing_root_chord= 5.000 wing_dihedral= 3.500 wing_incidence= 1.000 wing_twist= 0.000 oswald_efficiency_factor= 0.697 wing_winglets_flag= 0 wing_sweep= 5.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 29.810 htail_span= 11.970 htail_pos_lon= 18.800 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 15.000 vtail_area= 8.070 vtail_span= 3.280 vtail_sweep= 45.000 vtail_pos_lon= 18.800 vtail_pos_vert= 0.583 elevator_area= 10.549 aileron_area= 20.000 rudder_area= 10.760 elevator_up_limit= 22.000 elevator_down_limit= 22.000 aileron_up_limit= 25.000 aileron_down_limit= 25.000 rudder_limit= 25.000 elevator_trim_limit= 19.996 spoiler_limit= 0.000 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [GeneralEngineData] engine_type= 0 Engine.0= 5.000, 0.000, 0.000 fuel_flow_scalar= 1.000 [Reference Speeds] flaps_up_stall_speed= 110.000 full_flaps_stall_speed= 80.000 cruise_speed= 245.912 [keyboard_response] elevator=350.000000,500.000000 aileron=450.000000,1000.000000 rudder=200.000000,1000.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=1,0 [Flaps.0] type= 1 span-outboard= 0.125 extending-time= 5.000 system_type= 0 damaging-speed= 172.000 blowout-speed= 260.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 14.000, 0.000 flaps-position.2= 28.000, 0.000 flaps-position.3= 42.000, 0.000 flaps-position.4= 55.000, 0.000
