[fltsim.0]
title=Antonov AN225-100 Antonov Air Cargo
sim=an225
model=
panel=
sound=
texture=
checklists=
description=An-225-100\nCurrent designation for the An-225 after being modernized with updated communications gear, navigation equipment, a collision avoidance system, and noise reduction features for use as a heavy commercial transport. 2 converted, 1 in operation, 1 pending full construction.\nCallsign ADB116F\nCorrected Flight Dynamics & Data by:\nDouglas E. Trapp\nFS Flight Dynamics Engineer\nKC6ZOF@Yahoo.com\nJune 2009\nModel and Textures by:\nTom Ruth & Alex Kvitta\nAugust 2003\nSound by:\nMike Hambly & Riuji Ozawa\n
ui_manufacturer=Antonov
ui_type=AN225
ui_variation=Antonov Air Cargo
kb_checklists=AN-225_check
kb_reference=AN-225_ref
atc_heavy=1
atc_id=UR82060
atc_airline=ANTONOV DESIGN BUREAU
atc_flight_number=116F //Real World Callsign
atc_parking_types=CARGO, RAMP
atc_parking_codes=ADB
[General]
performance=Engines: 6-Lotarev D-18T turbofans, 51,590 lbf each \nLength: 275.6 ft\nHeight: 59.3 ft\nWingspan: 290 ft 2 in\nWing Area: 9,743.7 ft²\nEmpty Weight: 385,805 lb/175,000 kg\nMTOW: 1,322,760 lb/600,000 kg\nFuel Capacity: 98,712.0 US gal (661,370 lbs/300,000 kg)\nPayload (this model): 275,594 lb/125,009 kg (125 tons)\nMax Payload: 440,920 lb/200,000 kg (200 tons)\nTakeoff Run (max): 11,483 ft (3,500 m)\nService Ceiling: 42,651 ft/13,000 m\nMax Climb Rate: 3,000 f/m @ 350 KIAS/mach .78\nCruise Speed:\nmach .74-.82 below FL350\nmach .82-.90 above FL350\nMax mach: .925\nRange:\n7,400 nm @ FL410E, mach .88\n7,200 nm @ FL420W, mach .88\nCrew: 6\n
atc_type=ANTONOV
atc_model=AN225
Category=airplane
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[WEIGHT_AND_BALANCE]
max_gross_weight =1322760
empty_weight =385805
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
//Long Range Payload Weight = 275,594 lb/125,009 kg
station_load.0 =170.0, 127.5, -4.0, 8.5,//Pilot
station_load.1 =170.0, 127.5, 4.0, 8.5,//Co-Pilot
station_load.2 =680.0, 110.0, 0.0, 9.5,//Crew X 4
station_load.3 =90.0, 90.0, 0.0, -4.5,//Luggage
station_load.4 =90.0, 85.0, 0.0, -4.5,//Luggage
station_load.5 =136597.0, 38.75, 0.0, -6.0,//Cargo Fore
station_load.6 =137797.0, -38.75, 0.0, -6.0,//Cargo Aft
;Moments of Inertia
empty_weight_roll_MOI = 13352310
empty_weight_pitch_MOI = 24223159
empty_weight_yaw_MOI = 39531785
empty_weight_coupled_MOI = 0
[fuel]
//98,712 US Gal = 661,370.4 lb/300,000 kg
LeftMain =0.0, -28.0, 4.0, 32904.0, 0.0
RightMain =0.0, 28.0, 4.0, 32904.0, 0.0
LeftAux =0.0, -36.5, 3.0, 16452.0, 0.0
RightAux =0.0, 36.5, 3.0, 16452.0, 0.0
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area =9743.7 //Square feet
wing_span =290.166667 //Feet
wing_root_chord = 48.8 //Feet
wing_dihedral = -7.0 //Degrees
wing_incidence = 2.0 //Degrees
wing_twist = -1.0 //Degrees
oswald_efficiency_factor= 0.58 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 37.5 //Degrees, wing leading edge
wing_pos_apex_lon = 1 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 10 //Feet, vertical distance from reference point, positive going up
htail_area =3597.023136 //Square feet
htail_span =107.119083 //Feet
htail_dihedral = 7.0 //Degrees
htail_pos_lon = -121.4 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 10.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 37.5 //Degrees, horizontal tail leading edge
vtail_area =2491.611291 //Square feet
vtail_span = 37.1 //Feet, tip to body
vtail_sweep = 45.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -120.5 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 26.1 //Feet, vertical distance from reference point, positive going up
elevator_area = 527 //Square feet
aileron_area = 325 //Square feet
rudder_area = 330 //Square feet
elevator_up_limit = 25 //Degrees
elevator_down_limit = 15 //Degrees
aileron_up_limit = 25 //Degrees
aileron_down_limit = 15 //Degrees
rudder_limit = 25.5 //Degrees
elevator_trim_limit = 20 //Degrees
spoiler_limit = 40 //Degrees
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 3 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 10 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000
[Reference Speeds]
flaps_up_stall_speed = 130.0 //Knots True (KTAS)
full_flaps_stall_speed = 102.0 //Knots True (KTAS)
cruise_speed =437.0 //Knots True (KTAS)
max_mach =0.925
max_indicated_speed = 530.0 //Red line (KIAS)
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 25 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 0 // degrees
flaps-position.2 = 10 // degrees
flaps-position.3 = 20 // degrees
flaps-position.4 = 30 // degrees
flaps-position.5 = 45 // degrees
flaps-position.6 = 60 // degrees
damaging-speed = 310 // KIAS
blowout-speed = 350 // KIAS
lift_scalar = 0.7
drag_scalar = 0.9
pitch_scalar= 0.9
system_type = 1 //Hydraulic
[flaps.1]
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.3 // 0.0 .. 1.0
extending-time = 8 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 1.0 // degrees
damaging-speed = 310 // KIAS
blowout-speed = 350 // KIAS
lift_scalar = 0.3
drag_scalar = 0.1
pitch_scalar= 0.1
system_type = 1 //Hydraulic
[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
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -22.304, -58.384, -4.592 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -10.168, -32.144, -3.28 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 = -10.168, 32.144, -3.28 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.3 = -22.304, 58.384, -4.592 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit = -0.25; //Minimum percent throttle. Generally negative for turbine reverser
[SMOKESYSTEM]
smoke.0=-34.44,-84.624,-5.904, fx_contrail_l
smoke.1=-34.44,84.624,-5.904, fx_contrail_l
[TurbineEngineData]
//Lotarev D-18T turbofans
fuel_flow_gain = 0.003 //Gain on fuel flow
inlet_area =37.675 //Square Feet, engine nacelle inlet area
bypass_ratio =6.45
rated_N2_rpm =44880 //RPM, second stage compressor rated value
static_thrust =77385 //Lbs, max rated static thrust at Sea Level
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?
[jet_engine]
thrust_scalar = 1.0
[autopilot]
autopilot_available = 1
flight_director_available = 1
default_vertical_speed =1500.0
autothrottle_available = 1
autothrottle_arming_required = 1
autothrottle_max_rpm =92
autothrottle_takeoff_ga = 1
pitch_takeoff_ga = 8;
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=1.5
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=16.00
nav_integrator_control=0.17
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control = 18.0
gs_integrator_control = 0.33
gs_derivative_control = 0.00
gs_integrator_boundary = 0.70
gs_derivative_boundary = 0.00
yaw_damper_gain = 1.0
[contact_points]
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
point.0 = 1, 63.96, 0.0, -20.3, 1000.0, 0, 3.0, 70.0, 1.5, 1.5, 0.300, 12.0, 12.0, 0, 200, 230
point.1 = 1, -48.214, -13.5, -20.5, 3000.0, 1, 3.5, 13.0, 1.0, 2.5, 0.300, 15.0, 15.0, 2, 200, 230
point.2 = 1, -48.214, 13.5, -20.5, 3000.0, 2, 3.5, 13.0, 1.0, 2.5, 0.300, 15.0, 15.0, 3, 200, 230
point.3 = 2, 96.432, 0.0, -4.592, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 5, 0, 0
point.4 = 2, 63.632, 0.0, -14.76, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 6, 0, 0
point.5 = 2, -53.136, 0.0, -17.056, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 9, 0, 0
point.6 = 2, -101.352, 0.0, -10.824, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0
point.7 = 2, 11.48, 0.0, 24.928, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0
point.8 = 2, -179.744, 53.135, 13.776, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0
point.9 = 2, -179.744, -53.136, 13.776, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0
point.10 = 2, -65.6, 146.144, 5.249, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0
point.11 = 2, -65.6, -146.144, 5.249, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0
static_pitch = -1.5
static_cg_height = 18.6
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available = 0 //Normal
pct_throttle_limit =0.01 //Percent throttle that activates warning
flap_limit_idle = 5.0 //Flap angle that activates warning at idle
flap_limit_power = 25.5 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.24 //Brake scalar
auto_brakes=4
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,1,1 //pumps on Eng1,2,3,4
[Views]
eyepoint = 71.176, -1.968, 9.512 ; Longitude, Latitude and Vertical position from Reference Point, (FEET)
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot = 0, 5 , 17.0
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_taxi = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 1, 1
Nav.2 = 1, 1, 0
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.5 = 2, -163.344, 50.427, 36.408, fx_strobeh ,
light.6 = 2, -163.344, -50.427, 36.408, fx_strobeh ,
light.7 = 1, 46.58, 0.00, 12.9, fx_strobeh ,
light.8 = 1, 55.68, 0.00, -15.1, fx_strobeh ,
light.9 = 4, 71.18 0.00, 11.2, fx_vclighth,
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[exits]
number_of_exits = 2
exit_rate.0 = 0.2 ;Percent per second
exit_rate.1 = 0.05 ;Percent per second
[TailHook]
tailhook_length=4 ;(feet)
tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0.9
[folding_wings]
wing_fold_system_type=4
fold_rates=0.11,0.13 ;Percent per second
[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
[stall_warning]
type=2
stick_shaker=1
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=1
