[fltsim.0]
title=hortenIV
sim=hortenIV
model=
panel=
sound=
texture=
kb_checklists=
kb_checklists=
kb_reference=
description=The high-performance Horten H IV glider was built for comparative testing of flying wing designs against conventional gliders. The first Horten IV was completed in 1941, and three more were built in 1943. The achievements of the H IV in the air were impressive.
ui_manufacturer=Horten
ui_type=HoIVa
ui_typerole="Glider"
ui_createdby=David Rowberry
ui_variation=1959 USA
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=
[fltsim.1]
title=hortenIV_no26
sim=hortenIV
model=2
panel=
sound=
texture=1
kb_checklists=
kb_checklists=
kb_reference=
description=The high-performance Horten H IV glider was built for comparative testing of flying wing designs against conventional gliders. The first Horten IV was completed in 1941, and three more were built in 1943. The achievements of the H IV in the air were impressive.
ui_manufacturer=Horten
ui_type=HoIVa
ui_typerole="Glider"
ui_createdby=David Rowberry
ui_variation=Deutsches Museum
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=
[CameraDefinition.0]
Title = "Tail"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 0.0, 1.0, -3.0
InitialPbh = 15, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.1]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
ShowWeather = Yes
InitialXyz = 10.6, 0.98, -2.0
InitialPbh = 0, 0, 275
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = TRUE
ClipMode=Minimum
[CameraDefinition.2]
Title = "Left Wing"
Guid = {33320004-b71a-4f9f-9105-1eb674ab7f3c}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
ShowWeather = Yes
InitialXyz = -11.5, 1.0, -2.0
InitialPbh = 0, 0, 85
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = TRUE
ClipMode=Minimum
[CameraDefinition.3]
Title = "Nose"
Guid = {59181B43-9231-4fb0-8FF7-FB4318532141}
Description =Looking back from the nose of the glider
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 1, 0.1, 3.0
InitialPbh = 2, 0, 190
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
[Electrical]
max_battery_voltage=12.0
additional_system=0,0.0,0
avionics_bus=0,0.1,1
avionics=5,0.1,1
[General]
performance=Span - 20.3 m\nWt empty - 246 kg , all up - 366 kg\n Min Sink 0.55m/s @55km/h\nbest glide - 32:1 @73km/h kph\nVNE - 200 km\/h\nStall - 55 km/h\n
Category=airplane
atc_type=
atc_model=
[WEIGHT_AND_BALANCE]
max_gross_weight = 806.89
empty_weight = 524.33
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = -0.80, 0.000, 0.000
max_number_of_stations = 2
station_load.0 =176.000000, -0.500000, 0.000000, 0.000000, Pilot
station_load.1 =20.000000, 0.000000, 0.000000, 0.000000, ballast
empty_weight_pitch_MOI = 1109.000
empty_weight_roll_MOI = 1289.000
empty_weight_yaw_MOI = 1112.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar =1.2
parasite_drag_scalar =0.5
induced_drag_scalar =1.7
elevator_effectiveness =1.0
aileron_effectiveness =1.0
rudder_effectiveness =0.3
pitch_stability =0.3
roll_stability =0.7
yaw_stability =0.8
elevator_trim_effectiveness =1.904
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type= 2
fuel_flow_scalar=0.000000
[pitot_static]
vertical_speed_time_constant = 4 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=0.000000
//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]
point.0= 1.000, 1.00, 0.000, -2.42, 1500.000, 0.000, 0.000, 0.000, 0.300, 2.500, 0.75, 1.500, 1.500, 4.000, 0.000, 0.000
point.1= 3.000, -4.55, 0.001, -2.22, 1500.000, 0.000, 0.000, 0.000, 0.200, 0.500, 0.90, 0.000, 0.000, 9.000, 0.000, 0.000
point.2= 3.000, -4.55, -0.001, -2.22, 1500.000, 0.000, 0.000, 0.000, 0.200, 0.500, 0.90, 0.000, 0.000, 9.000, 0.000, 0.000
point.3= 2.000, -10.34, 33.300, 2.080, 900.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.4= 2.000, -10.34, -33.300, 2.080, 900.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.5= 2.000, 0.000, 0.000, -1.000, 1000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 1.800
static_cg_height= 2.1
gear_system_type=3
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.2 //Brake scalar
[fuel]
electric_pump=0
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
Center1= 0,0,0,0,0
number_of_tank_selectors=1
[Views]
eyepoint = 3.0, 0.0, 3.0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4, 2.7, 0.00, 1.50, fx_vclight,
[variometers]
variometer.0=54,-116
[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
[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 = 160, 360
aileron = 160, 360
rudder = 160, 360
[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
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 0
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[EFFECTS]
wake=fx_wake
water=fx_spray
concrete=fx_tchdwn_s
touchdown=0
dirt=fx_tchdrt
[airplane_geometry]
wing_area = 203.400
wing_span = 65.600
wing_root_chord = 5.100
wing_dihedral = 5.000
wing_incidence = 0.000
wing_twist = -2.100
oswald_efficiency_factor= 0.800
wing_winglets_flag = 0
wing_sweep = 17.00
wing_pos_apex_lon = 0.900
wing_pos_apex_vert = 0.000
htail_area = 0.100
htail_span = 0.100
htail_pos_lon = 0.000
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 0.000
vtail_area = 0.000
vtail_span = 0.000
vtail_sweep = 0.000
vtail_pos_lon = 0.000
vtail_pos_vert = 0.000
elevator_area = 21.60
aileron_area = 9.240
rudder_area = 4.500
elevator_up_limit = 15.000
elevator_down_limit = 9.000
aileron_up_limit = 16.000
aileron_down_limit = 10.000
rudder_limit = 90.000
elevator_trim_limit = 15.000
spoiler_limit = 70.000
spoilerons_available = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
auto_spoiler_available=0
spoiler_extension_time=0.500000
positive_g_limit_flaps_up=5.300000
positive_g_limit_flaps_down=5.300000
negative_g_limit_flaps_up=-2.6500000
negative_g_limit_flaps_down=-2.6500000
[Reference Speeds]
flaps_up_stall_speed = 29.600
full_flaps_stall_speed = 29.600
cruise_speed = 41.400
max_indicated_speed = 110.000 //Red line (KIAS)
max_mach=0.260010
[autopilot]
autopilot_available= 0
flight_director_available= 0
[forcefeedback]
ground_bumps_magnitude1=2500 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=10.0
ground_bumps_slope1=0.300
ground_bumps_magnitude2=350 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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
[yaw_string]
yaw_string_available=1
[stall_warning]
type=1
stick_shaker=0
[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=0.000000
[deice_system]
structural_deice_type=0
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[Flaps.0]
type= 1
[hydraulic_system]
normal_pressure=0.000000
