[fltsim.0]
title = De Havilland Mosquito NFII
sim = Mosquito NFII
model = 
panel = 
sound =
texture =
panel_alias =
sound_alias =
kb_checklists =
kb_reference =
visual_damage=1
atc_id = GNFII
atc_id_color =
atc_parking_types =MIL_COMBAT
atc_parking_codes =DH98 Mosquito
ui_manufacturer = De Havilland
ui_type = Mosquito NFII
ui_variation = 23 Sqdn, 1942
description = RR Merlin 23 - 1390hp @ + 12lbs Boost, 3000 rpm @ Take Off, 1480hp @ 16 lbs Boost, 3000rpm @ 12250ft  (Climbing Boost + 9lbs @ 2850rpm

[General]
atc_type = DeHavilland
atc_model = Mosquito
editable = 1
performance = + Empty Weight: 14480 lbs + Max Power: 1480 Hp + Maneuver speed: 292 mph @ 7.5 g + Max speed: 370 mph @ 22000 ft + Max speed at sea-level: 317 mph + Climb rate: 3000 ft/min @ 170 mph Flight Dynamics By: Paul Bradford BRADBURGER FD Build 2 - 4/28/04 09:20 PM Flight Dynamics Workbook V2.84.63

[pitot_static]
vertical_speed_time_constant = 0.49

[WEIGHT_AND_BALANCE]
max_gross_weight = 19200
empty_weight = 14120

reference_datum_position = 0, 0, 0
empty_weight_CG_position  = -0.077122, 0, 0
CG_forward_limit = 0
CG_aft_limit = 1

max_number_of_stations = 2
station_load.0 = 180, 3.58, -0.81, -0.16, Pilot
station_load.1 = 180, 2.47, 0.89, -0.27, Navigator

empty_weight_pitch_MOI = 22994
empty_weight_roll_MOI = 24299
empty_weight_yaw_MOI = 44259
empty_weight_coupled_MOI = 0

[flight_tuning]
cruise_lift_scalar = 1
parasite_drag_scalar = 1
induced_drag_scalar = 1
elevator_effectiveness = 1
aileron_effectiveness = 1
rudder_effectiveness = 1
pitch_stability = 1
roll_stability = 1
yaw_stability = 1
elevator_trim_effectiveness = 1
aileron_trim_effectiveness = 1
rudder_trim_effectiveness = 1
hi_alpha_on_roll = 1
hi_alpha_on_yaw = 1
p_factor_on_yaw = 1
torque_on_roll = 1
gyro_precession_on_roll = 1
gyro_precession_on_yaw = 1

[GeneralEngineData]
engine_type = 0
Engine.0 = 7.87, -8.27, -0.46
Engine.1 = 7.87, 8.27, -0.46
fuel_flow_scalar = 1
min_throttle_limit = 0
max_contrail_temperature=-28

[piston_engine]
power_scalar = 1
cylinder_displacement = 137.416666666667
compression_ratio = 6
number_of_cylinders = 12
max_rated_rpm = 3000
max_rated_hp = 1390
fuel_metering_type = 2
cooling_type = 1
normalized_starter_torque = 0.035
turbocharged = 1
max_design_mp = 54.34
min_design_mp = 11
critical_altitude = 22000
emergency_boost_type = 3
emergency_boost_mp_offset = 2.17
emergency_boost_gain_offset = 0.174490600022515
fuel_air_auto_mixture = 1
auto_ignition = 0
emergency_boost_duration = 300
max_rpm_mechanical_efficiency_scalar = 1
idle_rpm_mechanical_efficiency_scalar = 1
max_rpm_friction_scalar = 1
idle_rpm_friction_scalar = 1

[propeller]
thrust_scalar = 1
propeller_type = 0
propeller_diameter = 12
propeller_blades = 3
propeller_moi = 56.6
beta_max = 65
beta_min = 15
min_gov_rpm = 450
prop_tc = 0.01
gear_reduction_ratio = 2.096
fixed_pitch_beta = 20
low_speed_theory_limit = 80
prop_sync_available = 0
prop_deice_available = 0
prop_feathering_available = 1
prop_auto_feathering_available = 0
feathering_switches = 1
min_rpm_for_feather = 700
beta_feather = 88.5
power_absorbed_cf = 0.9
defeathering_accumulators_available = 0
prop_reverse_available = 0
minimum_on_ground_beta = 1
minimum_reverse_beta = -14
rotation = 1, 1

[contact_points]
max_number_of_points = 12
point.0 = 1, -26.0511, 0, -2.83, 6153.30513, 0, 0.75, 30, 0.25, 2.5, 0.72631, 3, 3.9, 0, 157.52, 184.8
point.1 = 1, 2.3176, -8.4, -9.67, 6153.30513, 1, 2, 0, 1.15, 2.5, 0.72651, 8.9, 6.8, 2, 157.52, 184.8
point.2 = 1, 2.3176, 8.4, -9.67, 6153.30513, 2, 2, 0, 1.15, 2.5, 0.72651, 9.6, 8.2, 3, 157.52, 184.8
point.3 = 2, -25.2894, 0, 8.89, 3500, 0, 0, 0, 0, 0, 0, 0, 0, 9
point.4 = 2, 10.6331, 0, -0.8543, 5000, 0, 0, 0, 0, 0, 0, 0, 0, 4
point.5 = 2, 0.1091, -27.121, 1.1497, 4000, 0, 0, 0, 0, 0, 0, 0, 0, 5
point.6 = 2, 0.1091, 27.121, 1.1497, 4000, 0, 0, 0, 0, 0, 0, 0, 0, 6
point.7 = 2, -30.4069, 0, 0.9484, 2500, 0, 0, 0, 0, 0, 0, 0, 0, 9
point.8 = 2, -27.8842, 0, 0.1496, 2650, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 2.4845, 0, -3.8415, 2850, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.10 = 2, 8.1429, -8.27, -4.15, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0
point.11 = 2, 8.1431, 8.4, -4.13, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 7
point.12 = 2, -7.3435, 0, -3.301, 2800, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0

static_pitch= 12.5
static_cg_height= 7.9
gear_system_type = 1
tailwheel_lock = 0

[Views]
eyepoint= 3.24, -0.85, 2.15

[folding_wings]
wing_fold_system_type =  4
fold_rates =  0.12, 0.13

[flaps.0]       //Trailing Edge Flaps
type = 1
span-outboard = 0.5
extending-time = 4
flaps-position.0 = 0
flaps-position.1 = 10, 182
flaps-position.2 = 15, 173
flaps-position.3 = 25, 143
flaps-position.4 = 45, 133
damaging-speed = 186
blowout-speed = 208
system_type = 1
lift_scalar = 1
drag_scalar = 1
pitch_scalar = 1

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 30
max_generator_alternator_amps = 60
engine_generator_map= 0,1
electric_always_available = 0
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 2, 2, 17
additional_system = 3, 20, 17
marker_beacon = 2, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 4, 5, 17
starter1 = 0, 20, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
standby_vacuum = 2, 15, 17
fuel_transfer_pump = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17

[SMOKESYSTEM]
//(feet) vertical, longitudinal, lateral, 
SMOKE.0=0.00, -3.00, -27.00, FX_HB_CONTRAIL_S,
SMOKE.1=0.00, -3.00,  27.00, FX_HB_CONTRAIL_S,


[LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi, 7=recog, 8=wing, 9=logo,     
//    class   long    lat     vert   effect
light.0=3,   0.900, -26.650,  1.100, fx_HB_NAVREDSTROBE,
light.1=3,   0.900,  26.650,  1.100, fx_HB_NAVGRESTROBE,
light.2=3, -25.000,   0.000,  8.850, fx_beaconh,
light.3=3, -30.440,   0.000,  1.000, fx_navwhi,
light.4=4,   4.500,  -0.800,  0.900, fx_vclight                //pilot
light.5=4,   3.000,  -0.800,  0.900, fx_vclight                //co-pilot
light.6=6,   3.825, -10.132, -1.100, FX_HB_FS2002_HE111_EXH,   //port  outer
light.7=6,   3.825,  -6.400, -1.100, FX_HB_FS2002_HE111_EXH,   //port  inner
light.8=6,   3.825,  10.132, -1.100, FX_HB_FS2002_HE111_EXH,   //starb outer
light.9=6,   3.825,   6.400, -1.100, FX_HB_FS2002_HE111_EXH,   //starb inner
light.10=5, -0.200, -14.355, -0.850, fx_landing,               //port  landing light
light.11=5, -0.200,  14.355, -0.850, fx_landing,               //starb landing light
[Radios] // availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 1
Transponder.1 = 1

[keyboard_response]
elevator = 350, 500
aileron  = 450, 1000
rudder   = 200, 1000

[direction_indicators]
direction_indicator.0 = 1, 0

[exits]
number_of_exits = 1
exit_rate.0 = 0.5

[EFFECTS]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1

[autopilot]
autopilot_available = 1
flight_director_available = 0
default_vertical_speed = 1000
autothrottle_available = 0
autothrottle_arming_required = 0
autothrottle_max_rpm =  90
autothrottle_takeoff_ga = 1
pitch_takeoff_ga = 8
max_pitch_velocity_hi_alt = 1.5
max_pitch_velocity_lo_alt_breakpoint = 20000
max_pitch_velocity_hi_alt_breakpoint = 28000
max_pitch = 10
max_pitch_acceleration = 1
max_pitch_velocity_lo_alt = 2
max_bank= 25
max_bank_acceleration = 1.8
max_bank_velocity = 3
max_throttle_rate = 0.1
nav_proportional_control = 9
nav_integrator_control = 0.25
nav_derivative_control = 0
nav_integrator_boundary = 2.5
nav_derivative_boundary = 0
gs_proportional_control = 9.52
gs_integrator_control = 0.26
gs_derivative_control = 0
gs_integrator_boundary = 0.7
gs_derivative_boundary = 0
yaw_damper_gain = 0

[fuel]
Center2 = -3.077122, -0.8, 0.3, 30,  0
Center3 = -3.077122, 0.8, 0.3, 30,  0
LeftMain = -0.577122, -4, 0, 171.7,  0
RightMain = -0.577122, 4, 0, 171.7,  0
LeftAux = -1.077122, -16.5, 0.55, 69.7,  0
RightAux = -1.077122, 16.5, 0.55, 69.7,  0
fuel_type =  1
number_of_tank_selectors = 1
electric_pump=0

[airplane_geometry]
wing_area = 454
wing_span = 54.1666666666667
wing_root_chord = 8.38153846153846
wing_dihedral = 1.24
wing_incidence = 0
wing_twist = 0
oswald_efficiency_factor = 0.88419837495823
wing_winglets_flag = 0
wing_sweep  = 0
wing_pos_apex_lon = 2.01826261538462
wing_pos_apex_vert = 0
htail_area = 44.98
htail_span = 20.9
htail_pos_lon = -27.12
htail_pos_vert = 0
htail_incidence = 0
htail_sweep = 0
vtail_area = 13.3
vtail_span = 5.75
vtail_sweep = 0
vtail_pos_lon  = -24.9
vtail_pos_vert = 0
elevator_area = 34.08
aileron_area = 34.4
rudder_area = 16
elevator_up_limit = 25
elevator_down_limit = 25
aileron_up_limit = 26.5
aileron_down_limit = 11.5
rudder_limit = 25
elevator_trim_limit = 18
spoiler_limit = 0.6555
spoilerons_available = 0
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0

[Reference Speeds]
flaps_up_stall_speed    = 93
full_flaps_stall_speed  = 74.7
cruise_speed            = 169
max_indicated_speed = 435
max_mach = 0.5585

[forcefeedback]
gear_bump_nose_magnitude = 2000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6050
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6850
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 2860
stick_shaker_direction = 0
stick_shaker_period = 111111

[gear_warning_system]
gear_warning_available = 0
pct_throttle_limit = 0.1
flap_limit_idle = 33.75
flap_limit_power = 16.875

[brakes]
toe_brakes_scale = 0.569170201727348
parking_brake = 1
differential_braking_scale = 15

[stall_warning] //  0 = None, 1 = Suction, 2 = Electric.
type = 1

[hydraulic_system]
electric_pumps = 0
engine_map = 1, 1, 0, 0
normal_pressure = 1225

[attitude_indicators] // 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1

[turn_indicators] // 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0 = 1, 0

[direction_indicators] // 0=None, 1=Vac Gyro, 2=Elec Gyro, 3=EM Slave Compass, 4=Slave to other ind
direction_indicator.0 = 1, 0

[airspeed_indicators]
airspeed_indicator.0 = 1, 0