// iss 0504131900 v1.08 : -{1234}- refers to the equivalent entry number in the *.AIR file
[fltsim.0]
title=brigandTF
sim=brigandTF
model=
panel=
sound=
texture=
kb_checklists=brigand_check
kb_reference=brigandTF_ref
atc_id_enable=1
atc_id=RH754
atc_airline=Air Force
atc_flight_number=RH754
ui_manufacturer=Bristol
ui_type=Brigand
ui_variation=TF Mk I
description=Light attack bomber.
visual_damage=0
prop_anim_ratio=-1.76
[General]
atc_type=Bristol
atc_model=Brigand
editable=1
performance="Maximum speed\n400 mph ~ 350 kts @ 15,000 ft.\nCruise speed\n207 mph ~ 180 kts\n\nEngines\nTwo Bristol Centaurus 57 2,810 hp. max.\n\nMaximum range\n2,800 nm with 2,000lb.+ bombload\n\nService ceiling\n25,000 ft\n\nFuel capacity\n1,270 gal.US. 1,058 gall.Imp.\n\nEmpty weight\n25,598 lb.\n\nMaximum gross weight\n39,000 lb. \n\nLength\n46 ft. 4 in.\n\nWingspan\n72 ft. 4in.\n\nHeight\n17 ft. 5 in.\"
[WEIGHT_AND_BALANCE]
max_gross_weight = 39000
empty_weight = 25598
reference_datum_position = 0, 0, 0 // (feet) from FSim Ref. pos: (Chord/4,centerline, waterline)
empty_weight_CG_position = 0.35, 0, 0 // z,x,y -- (feet) from specified datum.
max_number_of_stations =3
station_load.0 = "170, 5.00, 0.0, 1.3, P1" //Weight, Lat, Lon, Vert Position
station_load.1 = "170, 0.60, 0.0, 0.0, Nav"
station_load.2 = "170,-1.80, 0.0, 0.0, WOP"
;moments of inertia // -{no entries}-
empty_weight_pitch_MOI = 66857
empty_weight_roll_MOI = 77307
empty_weight_yaw_MOI = 136474
empty_weight_coupled_MOI = 0.0
[flight_tuning]
cruise_lift_scalar=0.8
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.5
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
p_factor_on_yaw=0.5
torque_on_roll=1.0
gyro_precession_on_yaw=1.0
gyro_precession_on_pitch=1.0
[fuel] //Long. Lat. Vertical (feet), Usable, Unusable (gallons US.)
LeftTip = 0.0, -18.7, 0.0, 183.0, 0.0
RightTip = 0.0, 18.7, 0.0, 183.0, 0.0 // 152.0 imp.
LeftAux = 0.0, -12.4, 0.0, 213.0, 0.0
RightAux = 0.0, 12.4, 0.0, 213.0, 0.0 // 177.0 imp.
LeftMain = 0.0, -4.2, 0.0, 240.0, 0.0
RightMain= 0.0, 4.2, 0.0, 240.0, 0.0 // 200.0 imp.
fuel_type = 1 // 1 = Avgas
number_of_tank_selectors = 2
electric_pump=1
[airplane_geometry]
wing_area = 726.0 //Square feet -{no entry}-
wing_span = 72.0 //Feet
wing_root_chord = 10.08 //Feet, MAC -- NOT Root
wing_dihedral = 2.0 //Degrees On thickness c/l
wing_incidence = 3.0 //Degrees
wing_twist = -1.0 //Degrees
oswald_efficiency_factor = 0.85 // Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 5.0 //Degrees,on Mean Average Chord (MAC)
wing_pos_apex_lon = 3.36 //Feet, long. dist. of MAC. LE. from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vert. dist. of MAC. LE. from reference point, positive going up
htail_area = 93.2 // Square feet -{no entry}-
htail_span = 22.0 // Feet
htail_pos_lon = -25.2 // Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 1.56 // Feet, vertical distance from reference point, positive going up
htail_incidence = -2.0 // Degrees
htail_sweep = 0.0 // Degrees, on MAC
vtail_area = 56.0 //Square feet -{no entry}-
vtail_span = 6.00 //Feet, tip to body [b=9.48]
vtail_sweep = 0.0 //Degrees, on MAC
vtail_pos_lon = -25.2 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 2.0 //Feet, vertical distance from reference point, positive going up
elevator_area = 52.2 //Square feet -{320}-
aileron_area = 37.0 //Square feet
rudder_area = 32.0 //Square feet
elevator_up_limit = 17.0 //Degrees = 0.30 rad
elevator_down_limit = 15.0 //Degrees = 0.26 rad
aileron_up_limit = 20.0 //Degrees = 0.35 rad
aileron_down_limit = 15.0 //Degrees = 0.26 rad
rudder_limit = 25.0 //Degrees = 0.44 rad
elevator_trim_limit = 12.0 //Degrees = 0.21 rad
spoiler_limit = 70.0 //Degrees = 1.22 rad
spoilerons_available = 0 //Spoilerons Available?
aileron_to_spoileron_gain = 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed = 105.0 //Knots True (KTAS)
full_flaps_stall_speed = 90.0 //Knots True (KTAS)
cruise_speed = 180.0 //Knots True (KTAS)
max_indicated_speed = 350.0 //Red line (KIAS)
//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
[contact_points]
// GEAR.
point.0=1, -30.39, 0.00, -3.80, 1200.0, 0, 0.88, 180.0, 0.42, 2.5, 0.87, 4.0, 4.0, 0, 185.0, 220.0
point.1=1, 2.52, -10.40, -9.75, 1600.0, 1, 2.00, 0.0, 0.50, 2.5, 0.85, 4.2, 5.2, 2, 185.0, 220.0
point.2=1, 2.52, 10.40, -9.75, 1600.0, 2, 2.00, 0.0, 0.50, 2.5, 0.85, 4.5, 5.8, 3, 185.0, 220.0
// SCRAPES.
//point.3=2, 12.0, 0.0, 0.0, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 4, 0.0, 0.0 // Nose.
//point.4=2, -33.2, 0.0, 1.0, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9, 0.0, 0.0 // Tail.
//point.5=2, -2.8, -36.3, 1.2, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5, 0.0, 0.0 // Left.
//point.6=2, -2.8, 36.3, 1.2, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6, 0.0, 0.0 // Right.
//point.7=2, 10.7, -10.4, -8.2, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9, 0.0, 0.0 // L.Prop.
//point.8=2, 10.7, 10.4, -8.2, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9, 0.0, 0.0 // R.Prop.
//point.9=2, -28.4, -10.9, 8.4, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 7, 0.0, 0.0 // L.Fin.
//point.10=2,-28.4, 10.9, 8.4, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 8, 0.0, 0.0 // R.Fin.
static_pitch = 10.8
static_cg_height = 8.5
gear_system_type=1 //Hydraulic -{no entry}-
tailwheel_lock = 1
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.33 //Percent throttle that activates warning
flap_limit_idle = 0.0 //Flap angle that activates warning at idle ~ NOT USED!
flap_limit_power = 70.0 //Flap angle that activates warning at above idle ~ NOT USED!
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.6 //Brake scalar ~ 0.3
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -0.82, -34.7, 1.075, fx_navredm ,
light.1 = 3, -0.82, 34.7, 1.075, fx_navgrem ,
light.2 = 3, -32.95, 0.0, 0.838, fx_navwhi ,
light.3 = 4, 5.50, 0.0, 3.000, fx_vclight,
light.4 = 5, 0.80, -25.4, 0.300, fx_landing, // Beam done in FSDS.
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 17
[flaps.0] //Trailing Edge Flaps -{524}-
type = 1 // 1 - tail.
span-outboard = 0.33 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees = 0.00 rad
flaps-position.1 = 15 // degrees = 0.26 rad
flaps-position.2 = 60 // degrees = 1.05 rad
damaging-speed = 145 // KIAS
blowout-speed = 250 // KIAS
lift_scalar = 1.0
drag_scalar = 2.0
pitch_scalar= 1.0
system_type = 1 // 1=Hydraulic.
[GeneralEngineData]
engine_type = 0 //0=Piston.
Engine.0 = 10.44, -10.4, -1.0 //(ft.) long, lat, vert. dist. from ref. datum
Engine.1 = 10.44, 10.4, -1.0
fuel_flow_scalar= 1.0 //Fuel flow scalar
min_throttle_limit = 0.0 //Minimum percent throttle.
max_contrail_temperature= -10 // A bit of fun.
[piston_engine]
power_scalar = 1
cylinder_displacement = 181.72
compression_ratio = 7.2
number_of_cylinders = 18
max_rated_rpm= 2700
max_rated_hp= 2810 //Max rated HP ( Sound effect only )
fuel_metering_type = 0
cooling_type = 0
normalized_starter_torque = 0.033
turbocharged = 1
max_design_mp = 49.26
min_design_mp = 9 // ~1
critical_altitude = 16000
emergency_boost_type = 0
emergency_boost_mp_offset = 0
emergency_boost_gain_offset = 0
fuel_air_auto_mixture = 1
auto_ignition = 0
max_rpm_mechanical_efficiency_scalar = 1.2
idle_rpm_mechanical_efficiency_scalar = 1
max_rpm_friction_scalar = 0.9
idle_rpm_friction_scalar = 1
emergency_boost_duration = 0
[propeller]
thrust_scalar = 1
propeller_type = 0
propeller_diameter = 13.68
propeller_blades = 4
propeller_moi = 70
beta_max = 65
beta_min = 15
min_gov_rpm = 400
prop_tc = 0.1
gear_reduction_ratio = 2.273
fixed_pitch_beta = 25
low_speed_theory_limit = 80
prop_sync_available = 0
prop_deice_available = 0
prop_feathering_available = 1
prop_auto_feathering_available = 0
min_rpm_for_feather = 700
beta_feather = 88.5
power_absorbed_cf = 0.9
defeathering_accumulators_available = 0
feathering_switches = 1 // Available? 1=TRUE
prop_reverse_available = 0
minimum_on_ground_beta = 0
minimum_reverse_beta =0
[keyboard_response]
elevator=150.0,250.0
aileron =150.0,250.0
rudder =150.0,250.0
[Views]
eyepoint = 3.4, 0.0, 3.80 // z,x,y.
[exits]
number_of_exits=2
exit_rate.0=0.1 ;Percent per second
exit_rate.1=0.1 ;Percent per second
[Radios]
Audio.1 =1
Com.1 =1, 0
Nav.1 =1, 0, 1
Nav.2 =1, 0, 0
Adf.1 =1
Transponder.1=1
Marker.1=0
[direction_indicators]
direction_indicator.0=1,0
[hydraulic_system]
normal_pressure = 800.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1 //pumps on Eng1,2
// Vacuum systems -{1512}- AIR file entry needed for vacuum selector and gauge.
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
//-------------------------------------------------------------------------------------------------
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.0
autothrottle_available=0
pitch_takeoff_ga=8.0
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=3.0
max_throttle_rate=0.1
nav_proportional_control=9.0
nav_integrator_control=0.25
nav_derivative_control=0.0
nav_integrator_boundary=2.5
nav_derivative_boundary=0.0
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.0
gs_integrator_boundary=0.7
gs_derivative_boundary=0.0
yaw_damper_gain=0.0
