[fltsim.0] title=MAI MIR2 CG HAF sim=MIR2000_AI model= texture=HAF visual_damage=1 atc_id=2EK atc_airline=AIR FORCE atc_flight_number=2EK atc_heavy=0 editable=0 ui_manufacturer=Dassault ui_type=Mirage 2000C ui_variation=Hellenic Air Force description=Mirage 2000 C modélisé sous Gmax Laborie Roland, rollus13@club-internet.fr atc_parking_codes=MIR2,M001 atc_parking_types=MIL_COMBAT [general] performance=specifications \ncountries of origin france \nbuilder team : dassault aviation, snecma, thomson-csf \nfirst flight : march, 1978 [mirage 2000c]\nfebruary, 1991 [mirage 2000d] \nin-service in the french air force : summer 1983 [mirage 2000c]\nrole interceptor [mirage 2000c] \n\nlength 50 ft, 3 in (14.36 m) \nspan 29 ft, 5 in (9.13 m) \nheight 5.30 meters \nempty weight 7,600 kg \nmaximum weight 16,500 kg \nmaximal armament weight : 5,900 kg \npower plant \/ thrust : snecma m 53 p2 jet engine \/ height 5.30 meters empty weight 7,600 kg maximum weight 16,500 kg maximal armament weight : 5,900 kg power plant / thrust : snecma m 53 p2 jet engine / 9.7 t with afterburner maximum speed mach 1,2 [low altitude] mach 2,2 [high altitude] rate of climb 17,000 m/min ceiling above 50,000 ft / 16,500 m combat radius 800 nm (1,475 km) w/ 4 250-kg bombs 1,000 nm (1,850 km) w/ 2 1,700-liter drop tanks 1,800 nm (3,335 km) max fuel w/ 2 1,700-liter + 1 1,300-liter drop tanks in-flight refueling yes fuel capacity : 3,950 l internal / 8,000 l maximal / in-flight refuelling [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=17535.000000 empty_weight_roll_moi=15000.000000 empty_weight_pitch_moi=100000.000000 empty_weight_yaw_moi=100000.000000 empty_weight_coupled_moi=5000.000000 max_gross_weight=26302.500000 [fuel] leftmain=0.000000,0.000000,0.000000,460.000000,0.000000 leftaux=0.000000,-11.916667,0.000000,200.000000,0.000000 rightmain=0.000000,0.000000,0.000000,460.000000,0.000000 rightaux=0.000000,11.916667,0.000000,200.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=448.0 wing_span=29.91 wing_root_chord=14.916667 wing_dihedral=1.999512 wing_incidence=-0.494385 wing_twist=-0.999756 oswald_efficiency_factor=1.510044 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=81.000000 htail_span=22.000000 htail_pos_lon=-41.666667 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=55.000000 vtail_span=8.455767 vtail_sweep=0.000000 vtail_pos_lon=-41.666667 vtail_pos_vert=5.833333 elevator_area=20.250000 aileron_area=17.920000 rudder_area=9.350000 elevator_up_limit=27.501974 elevator_down_limit=11.459156 aileron_up_limit=40.107046 aileron_down_limit=40.107046 rudder_limit=23.491270 elevator_trim_limit=19.480565 spoiler_limit=59.988681 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [contact_points] //0 class //1 longitudinal position (feet) //2 lateral position (feet) //3 vertical position (feet) //4 impact damage threshold (feet per minute) //5 brake map (0=none, 1=left, 2=right) //6 wheel radius (feet) //7 steer angle (degrees) //8 static compression (feet) (0 if rigid) //9 max/static compression ratio //10 damping ratio (0=undamped, 1=critically damped) //11 extension time (seconds) //12 retraction time (seconds) //13 sound type 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.0=1.000000, 9.666667, 0.000000, -5.416667, 1574.803150, 0.000000, 0.682870, 30.000000, 0.205730, 2.500000, 0.781503, 5.000000, 5.000000, 0.000000, 0.000000, 0.000000 point.1=1.000000, -8.416667, -5.500000, -5.166667, 1574.803150, 1.000000, 0.682870, 0.000000, 0.205771, 2.500000, 0.781504, 5.000000, 5.000000, 2.000000, 0.000000, 0.000000 point.2=1.000000, -8.416667, 5.500000, -5.166667, 1574.803150, 2.000000, 0.682870, 0.000000, 0.205771, 2.500000, 0.781504, 5.000000, 5.000000, 3.000000, 0.000000, 0.000000 point.3=2.000000, -16.916667,-13.916667,-1.666667, 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, -16.916667, 13.916667,-1.666667, 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, -23.583333, 0.000000, -3.666667, 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, 28.666667, 0.000000, -3.666667, 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=0.791016 static_cg_height=5.167943 gear_system_type=0 [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=13.330818,0.000000 flaps-position.2=26.661636,0.000000 flaps-position.3=39.992454,0.000000 [generalenginedata] engine_type=1 engine.0=0.000000,0.000000,0.833333 fuel_flow_scalar=1.000000 min_throttle_limit=-0.25 [turbineenginedata] fuel_flow_gain=0.002170 inlet_area=24.528480 rated_n2_rpm=29920.000000 static_thrust=20440.400000 afterburner_available=0 reverser_available=1 [reference speeds] flaps_up_stall_speed=140.0 full_flaps_stall_speed=112.0 cruise_speed=680.9 max_indicated_speed=1460.9 max_mach=2.20 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [views] eyepoint=16.801489,0.000000,2.896366 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1800.0 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.00 pitch_takeoff_ga=8.00 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain=0.00 [direction_indicators] direction_indicator.0=3,0 [smokesystem] smoke.0=0.0, -17.0, 0.0, fx_smoke_rfn [lights] //types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -14.75, -13.00, -0.90, fx_navred , light.1 = 3, -14.60, 13.35, -0.90, fx_navgre , light.2 = 3, -24.50, 0.20, 9.80, fx_navwhi , light.3 = 2, -14.75, -13.00, -0.90, fx_strobe , light.4 = 2, -14.60, 13.35, -0.90, fx_strobe , light.5 = 1, -24.50, 0.20, 9.80, fx_beacon , light.6 = 2, -3.15, 0.25, 3.80, fx_strobe , light.7 = 4, -3.15, 0.25, 3.80, fx_vclight, light.8=9, -20.20, 0.00, 1.10, fx_mirage_burn_one light.9=9, -20.20, 0.00, 1.10, fx_mirage_burn_two light.10=9, -27.30, 0.00, 1.10, fx_mirage_torch_flam light.11=9, -26.00, 0.00, 1.10, fx_mirage_glitter light.12 = 3, 13.00, 0.25, 1.50, fx_navred , [effects] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [brakes] toe_brakes_scale=1.000031 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [electrical] max_battery_voltage = 12.0 generator_alternator_voltage = 13.8 max_generator_alternator_amps = 40.0 ;bustype, maxampload, minvoltage bustypes:0=mainbus,1=avionicsbus,2=batterybus,3=hotbatterybus,4-7=generator/alternatorbus(1-4) avionics_bus = 0, 5 , 9.5 avionics = 1, 5 , 9.5 additional_system = 0, 2 , 9.5 marker_beacon = 1, 2 , 9.0 fuel_pump = 0, 5 , 9.0 [jet_engine] thrust_scalar = 1.0 [forcefeedback] stick_shaker_magnitude=5000 ; 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