[fltsim.0]
title=Mirage 2000c
sim=Mirage 2000c
model=
panel=
sound=
texture=
visual_damage=1
kb_checklists=
kb_reference=
atc_id=2EK
atc_type=Dassault
atc_model=Dassault
atc_airline=French Air Force
atc_flight_number=2EK
atc_heavy=0
editable=0
ui_manufacturer=Dassault
ui_type=Mirage 2000C
ui_variation=
description=Mirage 2000 C modélisé sous Gmax Laborie Roland, rollus13@club-internet.fr
[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