[fltsim.0]
title=Continental Virtual Airlines Concorde
sim=Concorde
model=
panel=
sound=
texture=CVA
kb_checklists=Concorde_check
kb_reference=Concorde_ref
atc_type=
atc_id_enable=1
atc_id=N700MS
editable=0
atc_flight_number=
atc_airline=
atc_model=
atc_parking_types=
atc_parking_codes=
ui_manufacturer=Aerospatiale / BAC
ui_type=Concorde
ui_variation=Continental Airlines
description=Continental Virtual Concorde. Painted by David Hays
performance=Weight: 196170 lbs Max 412000 lbs \nPower: 31350 lbs thrust \n2.5g Corner speed: 235 mph \nMax speed @ SL: 450mph \nMax speed: 1513 mph @ 51000 ft \nClimb rate: 3200 ft\/min @ 736 mph
visual_damage=0
[WEIGHT_AND_BALANCE]
empty_weight = 172930.0 // (pounds)
reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -50.333, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
station_load.0 = 1760, 1.00, 0.0, 0.0 //Weight Crew (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 3342, -29.00, 0.0, 0.0 //Weight Galleys(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 300, 8.00, 0.0, 0.0 //Weight Baggage 1 (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 500, -4.00, 0.0, 0.0 //Weight Baggage 2 (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 2562, -82.00, 0.0, 0.0 //Weight Baggage 3 (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = 3040, 18.00, 0.0, 0.0 //Weight Psgr Sect OA (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = 3040, 2.00, 0.0, 0.0 //Weight Psgr Sect OB (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = 4370, -28.00, 0.0, 0.0 //Weight Psgr Sect OC (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = 6080, -53.00, 0.0, 0.0 //Weight Psgr Sect OD (lbs), longitudinal, lateral, vertical positions from datum (feet)
empty_weight_roll_MOI=695703.000000
empty_weight_pitch_MOI=9295118.000000
empty_weight_yaw_MOI=4906663.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=296886.000000
[ground_reaction]
main_gear_static_compression = 1.5 // (feet), The distance the main gear strut is compressed when at rest on the ground
center_gear_static_compression = 1.5 // (feet), The distance the center gear strut is compressed when at rest on the ground
main_gear_damping_ratio = 0.95 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped
center_gear_damping_ratio = 0.95 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
fuel_transfer_pump = 0, 10, 17.0
[forcefeedback]
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=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=00500 ; 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
[General]
performance=Max Speed\tM 2.04\nCruise Speed\tMach 2\nMaximum Range\t3,371 nm\nService Ceiling\t60,000 ft\nMax Takeoff Weight\t408,000 lb\nSeating\t\t128\nMax Payload\t29,000 lb\n
[fuel]
Center1=-21.000000,0.000000,0.000000,7680.000000,0.000000
Center2=-98.500000,0.000000,0.000000,3500.000000,0.000000
LeftMain=-54.200000,-14.600000,-4.500000,10170.000000,0.000000
RightMain=-54.200000,14.600000,-4.500000,10170.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=4262.000000
wing_span=83.833333
wing_root_chord=66.166667
wing_dihedral=0.000000
wing_incidence=0.247192
wing_twist=0.000000
oswald_efficiency_factor=0.903612
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=0.000000
htail_span=0.000000
htail_pos_lon=0.000000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=249.000000
vtail_span=17.991665
vtail_sweep=0.000000
vtail_pos_lon=-35.833333
vtail_pos_vert=5.833333
elevator_area=70.500000
aileron_area=26.800000
rudder_area=56.200000
elevator_up_limit=29.793805
elevator_down_limit=29.793805
aileron_up_limit=29.793805
aileron_down_limit=29.793805
rudder_limit=30.000070
elevator_trim_limit=19.996227
spoiler_limit=0.000000
spoilerons_available=1
aileron_to_spoileron_gain=3.000000
min_ailerons_for_spoilerons=9.969466
min_flaps_for_spoilerons=0.000000
[contact_points]
point.0=1.000000,5.666667,0.000000,-14.000000,1181.102362,0.000000,3.336104,34.080000,1.500000,2.500000,0.950000,5.000000,5.000000,0.000000,0.000000,0.000000
point.1=1.000000,-54.000000,-13.000000,-15.500000,1574.803150,1.000000,3.336104,0.000000,1.500000,2.500000,0.950000,7.900000,7.900000,2.000000,0.000000,0.000000
point.2=1.000000,-54.000000,13.000000,-15.500000,1574.803150,2.000000,3.336104,0.000000,1.500000,2.500000,0.950000,8.100000,8.100000,3.000000,0.000000,0.000000
point.3=2.000000,-14.166667,-47.333333,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-14.166667,47.333333,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-116.666667,0.000000,0.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,42.666667,0.000000,-3.750000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=0.280151
static_cg_height=12.720257
gear_system_type=0
[brakes]
toe_brakes_scale=0.762963
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[Flaps.0]
type=0
span-outboard=0.500000
extending-time=0.000000
system_type=0
[GeneralEngineData]
engine_type=1
Engine.0=-38.000000,-19.250000,-1.000000
Engine.1=-38.000000,-15.250000,-1.000000
Engine.2=-38.000000,15.250000,-1.000000
Engine.3=-38.000000,19.250000,-1.000000
fuel_flow_scalar=1.000000
min_throttle_limit=-0.250000
[TurbineEngineData]
fuel_flow_gain=0.002000
inlet_area=16.000000
rated_N2_rpm=29920.000000
static_thrust=30500.000000
afterburner_available=1
reverser_available=0.000000
[Reference Speeds]
flaps_up_stall_speed=142.000000
full_flaps_stall_speed=113.600000
cruise_speed=250.000000
max_indicated_speed=1000.000000
max_mach=2.040039
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[Views]
eyepoint=59.388328,-1.307210,4.267655
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[direction_indicators]
direction_indicator.0=3,0
