[fltsim.0]
title=HP-50
sim=HP-50
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer=Handley Page
atc_id_color=0000000000
visual_damage=0
Description= The Handley Page Heyford was the last of the RAF's biplane bombers. It first flew in 1930 and served until the delivery of the Vickers Wellington
[General]
atc_type=
atc_model=
editable=0
performance="Top Speed\n142 mph\n\nEngines\nTwo Rolls Royce 575 hp Kestrels\n\nMaximum range\n920 miles\n\nService ceiling\n21.000 ft \n\nFuel capacity\\n\nEmpty weight\n9,200 lb\n\nMaximum gross weight\n16,900 lb\n\nLength\n58 ft\n\nWingspan\n75 ft\n\nHeight\n17 ft 6 in 5.18\n\nDesigner P. Clawson\n\n8/2003"
[weight_and_balance]
// ACM V2.0
max_gross_weight = 16900
empty_weight = 9200
reference_datum_position = 19.25, 0, 0
empty_weight_CG_position = -20.9, 0, 0
empty_weight_pitch_MOI = 69699.03
empty_weight_roll_MOI = 61179.1
empty_weight_yaw_MOI = 131797.97
empty_weight_coupled_MOI = 0
max_number_of_stations = 0
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -15.65, -34.9, 4.8, fx_navredm ,
light.1 = 3, -15.65., 34.9, 4.8, fx_navgrem ,
light.2 = 3, -58.93, 0, -0.15, fx_navwhi
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.0
engine.0 = -12.90, -9.10, 0.97,
engine.1 = -12.89, 9.10, 0.97,
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 2
Center1 = -22.55, 0, -2.7, 200, 0
LeftMain = -22.55, -6.7, -3, 202, 0
RightMain = -22.55, 6.7, -3, 202, 0
electric_pump=0
[contact_points]
static_pitch = 12.76
static_cg_height = 10.7
tailwheel_lock = 1
max_number_of_points = 7
point.0 = 1, -54.9928, 0, -3.5603, 1200, 0, 0.6, 180, 0.2, 2.5, 0.695, 0, 0, 0, 0, 0
point.1 = 1, -17.9234, -8.9975, -12.1615, 1600, 1, 1.35, 0, 0.704, 2.5, 0.686, 7, 9, 2, 166, 166
point.2 = 1, -17.9235, 8.9975, -12.1618, 1600, 2, 1.35, 0, 0.704, 2.5, 0.682, 3, 5, 3, 166, 166
point.3 = 2, -23.2568, -35.3353, -6.2314, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -23.38, 34.8316, -6.33, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -58.0939, 0, -1.1285, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, -1.9551, 0, -2.474, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
gear_system_type=0
[keyboard_response]
elevator = 200, 1000
aileron = 200, 1000
rudder = 200, 1000
[forcefeedback]
ground_bumps_magnitude1 = 2600
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.6
ground_bumps_magnitude2 = 1200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.085
ground_bumps_slope2 = 0.65
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 3500000
[airplane_geometry]
wing_area = 750
wing_span = 75.0
wing_root_chord = 10.0
wing_dihedral = 5.0
wing_incidence = 2.0
wing_twist = -1.0
oswald_efficiency_factor = 0.65
wing_winglets_flag = 0
wing_sweep = 14.5
wing_pos_apex_lon = -13.00
wing_pos_apex_vert = -2.7
htail_area = 120
htail_span = 28.25
htail_pos_lon = -52
htail_pos_vert = -52
htail_incidence = -1.0
htail_sweep = 27.0
vtail_area = 28
vtail_span = 11.49
vtail_sweep = 50.4
vtail_pos_lon = -51.4
vtail_pos_vert = 6.7
elevator_area = 52
aileron_area = 102.8
rudder_area = 23
elevator_up_limit = 22.0
elevator_down_limit = 22.0
aileron_up_limit = 22.0
aileron_down_limit = 22.0
rudder_limit = 22.0
elevator_trim_limit = 12.0
spoiler_limit = 0.0
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 25
max_generator_alternator_amps = 100
electric_always_available = 0
[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
p_factor_on_yaw = 0.5
torque_on_roll = 1.0
gyro_precession_on_yaw = 1.0
gyro_precession_on_pitch = 1.0
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 7 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 11 // degrees
flaps-position.2 = 23 // degrees
flaps-position.3 = 34 // degrees
flaps-position.4 = 45.0 // degrees
damaging-speed = 140 // KIAS
blowout-speed = 175 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[piston_engine]
power_scalar=1.0 //Piston power scalar
cylinder_displacement=130.71 //Cubic inches per cylinder
compression_ratio=6.7 //Compression ratio
number_of_cylinders=12 //Number of cylinders
max_rated_rpm=2700 //Max rated RPM
max_rated_hp=575 //Max rated HP
fuel_metering_type=1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3 //Starter torque factor
turbocharged=1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=47 //Max design manifold pressure, (inHg)
min_design_mp=10 //Min design manifold pressure, (inHg)
critical_altitude=7000 //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=0 //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=1.0 //Propeller thrust scalar
propeller_type=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=12.5 //Propeller Diameter, (feet)
propeller_blades=2 //Number of propeller blades
propeller_moi=40.2 //Propeller moment of inertia
beta_max=30.0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=18.0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=1400 //Miminum governed RPM
prop_tc=0.1 //Prop time-constant
gear_reduction_ratio=1.778 //Propeller gear reduction ratio
fixed_pitch_beta=0.0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80.0 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=1 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=700.0 //Minimum RPM for prop feathering
beta_feather=89.5 //Feathering pitch angle (degrees)
power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller in feather
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=0.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0.0 //Minimum pitch angle in reverse, (degrees)
feathering_switches = 1 //Switches which invoke feathering
//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
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 0.0 //Flap angle that activates warning at idle
flap_limit_power = 16.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.3 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure = 732.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint=-6.495, -1.512, 3.217
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Adf.2 = 1
Transponder.1=0
Marker.1=1
[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=1,0
direction_indicator.1=2,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
attitude_indicator.1 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=2,0
[Reference Speeds]
flaps_up_stall_speed=67.5 //Knots True (KTAS)
full_flaps_stall_speed=61.5 //Knots True (KTAS)
cruise_speed=95.0 //Knots True (KTAS)
max_indicated_speed = 224 //Red line (KIAS)
[autopilot]
autopilot_available=1
flight_director_available=0
pitch_takeoff_ga=0.0
default_vertical_speed=700.000000
autothrottle_available=0
direction_indicator=1
attitude_indicator =1
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 = 0.0
default_bank_mode=2 //Default to Heading Hold
[stall_warning]
type=1
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
