[fltsim.0]
title = Bristol Scout D
sim = Bristol Scout D
model =
panel =
sound =
texture =
kb_checklists =
kb_reference =
atc_id =7055
atc_airline =
atc_flight_number =
ui_manufacturer = Bristol
ui_type = Scout
ui_variation = RFC
ui_typerole = Fighter
ui_createdby = Wingsnwheels
[General]
atc_type = Bristol
atc_model = Scout
editable = 1
performance = Maximum Speed\t95 mph\nEngine\t\t80hp Gnome\nService Ceiling\t15,500 ft\nEndurance\t2hr 30min\nLength\t\t20ft 8in\nWingspan\t\t24ft 7in\nHeight\t\t8ft 6in\n
Category = airplane
[WEIGHT_AND_BALANCE]
max_gross_weight = 1250 // (pounds)
empty_weight = 760 // (pounds)
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 = 1
station_load.0 = 180.000000, -1.128000, 0.000000, 0.000000, Pilot
;Moments = of Inertia
empty_weight_pitch_MOI = 146
empty_weight_roll_MOI = 148
empty_weight_yaw_MOI = 367
empty_weight_coupled_MOI = 0.0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.5
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 1.4
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
hi_alpha_on_roll = 0.3
hi_alpha_on_yaw = 0.3
p_factor_on_yaw = 0.5
torque_on_roll = 0.0
gyro_precession_on_yaw = 0.3
gyro_precession_on_pitch = 0.3
[Flaps.0]
type = 0
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 4.000, 0.0, -0.05 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 0.66 //Fuel flow scalar
min_throttle_limit = 0.100000
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement = 55.0 //Cubic inches per cylinder
compression_ratio = 6.5 //Compression ratio
number_of_cylinders = 9 //Number of cylinders
max_rated_rpm = 2500 //Max rated RPM
max_rated_hp = 80 //Max rated HP
fuel_metering_type = 1 //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter
cooling_type = 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque = 3.1 //Starter torque factor
turbocharged = 0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp = 0 //Max design manifold pressure, (inHg)
min_design_mp = 0 //Min design manifold pressure, (inHg)
critical_altitude = 0 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type = 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset = 0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset = 0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture = 1 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition = 0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar = 1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar = 1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar = 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar = 1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar = 0.5 //Propeller thrust scalar
propeller_type = 1 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter = 6.2 //Propeller Diameter, (feet)
propeller_blades = 2 //Number of propeller blades
propeller_moi = 1.7 //Propeller moment of inertia
beta_max = 31.8 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min = 17.0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm = 1400 //Minimum governed RPM
prop_tc = 0.1 //Prop time-constant
gear_reduction_ratio = 1.0 //Propeller gear reduction ratio
fixed_pitch_beta = 20 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit = 80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available = 0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available = 0 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available = 0 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available = 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather = 0 //Minimum RPM for prop feathering
beta_feather = 0 //Feathering pitch angle (degrees)
power_absorbed_cf = 0 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available = 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available = 0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta = 0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta = 0 //Minimum pitch angle in reverse, (degrees)
//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]
max_number_of_points = 20
point.0 = 3, -12.737, 0, -1.81, 1500.0, 0, 0, 180, 0.304, 2.5, 0.695, 0, 0, 1 //t skid
point.1 = 1, 0.666, 2.05, -4.46, 1500, 2, 1.05, 0, 0.304, 2.5, 0.695, 0, 0, 3 //r wheel
point.2 = 1, 0.666, -2.05, -4.46, 1500, 1, 1.05, 0, 0.304, 2.5, 0.695, 0, 0, 2 //l wheel
point.3 = 2, 4.286, 0, 0, 950.0, 0, 0, 0, 0, 0, 0, 0, 0, 4 //nose
point.4 = 2, -13.951, 0, 0.612, 950.0, 0, 0, 0, 0, 0, 0, 0, 0, 4 //tail
point.5 = 2, -0.629, 9.086, -1.543, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 6 //r wing
point.6 = 2, -0.629, -9.086, -1.543, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 5 //l wing
gear_system_type = 4
static_pitch = 14.2
static_cg_height = 4.0
tailwheel_lock = 0
[Views]
eyepoint = -3.2, 0.0, 1.79
[Radios]
// = Radio Type=availiable, standby frequency, has glide slope
Audio.1 = 0
Com.1 = 1, 0
Nav.1 = 0, 0, 0
Adf.1 = 0
Transponder.1 = 0
Marker.1 = 0
[LIGHTS]
//Types: = 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 5, 0.75, 0, 2.77, fx_scout_gun
[AUTOPILOT]
autopilot_available = 1
flight_director_available = 1
default_pitch_mode = 0
default_bank_mode = 0
autothrottle_available = 1
autothrottle_arming_required= 0
autothrottle_takeoff_ga = 1.0
autothrottle_max_rpm = 2250.0
max_throttle_rate = 0.1
default_vertical_speed = 500.0
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= 10000.0
max_pitch_velocity_hi_alt_breakpoint= 14000.0
max_bank = 25.0
max_bank_acceleration = 1.8
max_bank_velocity = 3.0
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=0.000000
yaw_damper_gain
[keyboard_response]
//Breakpoint = speeds (knots) on the keyboard increments of control surfaces.
//Speed = at which the increment is reduced to 1/2 and 1/8 respectively.
elevator = 200, 1000
aileron = 200, 1000
rudder = 200, 1000
[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 = 0,0
[EFFECTS]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
[electrical]
max_battery_voltage = 0
generator_alternator_voltage = 0
[fuel]
Center1 = 1.0, 0.0, -0.3, 20.0, 0.2 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump = 0
[SMOKESYSTEM]
smoke.0 = 3.259, 0, -1.48, fx_smoke_w.fx
[airplane_geometry]
wing_area = 160.0 //Square feet
wing_span = 24.55 //Feet
wing_root_chord = 5.0 //Feet
wing_dihedral = 3.0 //Degrees
wing_incidence = 0.0 //Degrees
wing_twist = -1.0 //Degrees
oswald_efficiency_factor = 0.8 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 0.0 //Degrees, wing leading edge
wing_pos_apex_lon = 1.2 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 25.0 //Square feet
htail_span = 8.0 //Feet
htail_pos_lon = -11.7 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 0.0 //Degrees, horizontal tail leading edge
vtail_area = 11.0 //Square feet
vtail_span = 3.0 //Feet, tip to body
vtail_sweep = 0.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -12.6 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 0.6 //Feet, vertical distance from reference point, positive going up
elevator_area = 17.0 //Square feet
aileron_area = 28.3 //Square feet
rudder_area = 8.0 //Square feet
elevator_up_limit = 30.0 //Degrees
elevator_down_limit = 30.0 //Degrees
aileron_up_limit = 24.0 //Degrees
aileron_down_limit = 24.0 //Degrees
rudder_limit = 30.0 //Degrees
elevator_trim_limit = 30.0 //Degrees
rudder_trim_limit = 30.0 //Degrees
spoiler_limit = 0.0 //Degrees
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
auto_spoiler_available = 0
positive_g_limit_flaps_up = 4.000000
positive_g_limit_flaps_down = 2.000000
negative_g_limit_flaps_up = -1.500000
negative_g_limit_flaps_down = -1.500000
[Reference Speeds]
flaps_up_stall_speed = 31.0 //Knots True (KTAS)
full_flaps_stall_speed = 31.0 //Knots True (KTAS)
cruise_speed = 88.0 //Knots True (KTAS)
max_indicated_speed = 120.000000
[forcefeedback]
ground_bumps_magnitude1 = 2600 ; 0 - 10000
ground_bumps_angle1 = 8900 ; 0 - 35999 degrees
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.6
ground_bumps_magnitude2 = 1200 ; 0 - 10000
ground_bumps_angle2 = 9100 ; 0 - 35999 degrees
ground_bumps_intercept2 = 0.085
ground_bumps_slope2 = 0.65
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 = 3500000 ; in microseconds
[brakes]
toe_brakes_scale = 0.000000
parking_brake = 0
[pitot_static]
pitot_heat = 0.000000
[hydraulic_system]
normal_pressure = 0.000000
[vacuum_system]
max_pressure = 5.150000
vacuum_type = 0
electric_backup_pressure = 0.000000
engine_map = 0,0,0,0
[pneumatic_system]
max_pressure = 0.000000
bleed_air_scalar = 1.000000
[stall_warning]
type = 0
stick_shaker = 0
[attitude_indicators]
attitude_indicator.0 = 1
[turn_indicators]
turn_indicator.0 = 1,0
[deice_system]
structural_deice_type = 0
