[fltsim.0]
title=Huetter H 17 HDT
sim=hdt
model=
panel=
sound=
texture=
kb_checklists=
description=The Huetter H-17 was built by two Austrian brothers, Ulrich and Wolfgang, who lived in Salisburg. They felt that the larger slower German sailplanes were not suitable for the conditions found in their country. After learning to fly in a Grunau Baby, Ulrich designed their first model, the H-17 and after the first sucessful flights, about a dozen plans were sold. In 1934 fhe brothers flew the H-17 in the Austrian National Competition at Gaisberg. They joined the Schempp-Hirth company about 18 months later as designers. This company built about 5 Goeppingen 5 sailplanes from the Huetter Bros. plans of the H-17, adding a landing wheel and canopy.
ui_manufacturer=Huetter Brothers
ui_type=Huetter H17
[general]
editable=0
atc_type=SAILPLANE
atc_model=Holci
performance=Lippisch: Hols Der Teufel 1929
[WEIGHT_AND_BALANCE]
max_gross_weight = 471
empty_weight = 287
reference_datum_position = 3.6, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -3.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = "170, -3.0, -0.0, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 1400.0
empty_weight_roll_MOI = 1137.0
empty_weight_yaw_MOI = 2360.0
empty_weight_coupled_MOI= 0.0
[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 = 2.0
pitch_stability = 1.8
roll_stability = 1.0
yaw_stability = 3.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[GeneralEngineData]
engine_type = 2 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
fuel_flow_scalar=1.000000
//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)
//12 Retraction Time (seconds)
//13 Sound Type
[contact_points]
point.0 = 2, -2.80, -16.5, 2.8, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.1 = 2, -2.80, 16.5, 2.8, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.2 = 2, -10.00, 0.0, -0.04, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.3 = 2, -0.40, 0.0, -1.72, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
point.4 = 2, -10.93, 0.0, 4.00, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7, 0.0, 0.0
point.5 = 2, -0.40, 0.0, -1.74, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8, 0.0, 0.0
max_number_of_points = 7
static_pitch=9.0 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=1.0 //feet, altitude of CG when at rest on the ground
[fuel]
//Tanks Position and capacity:
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1 = 0, 0, 0, 0, 0
//Fuel type: 1 = Avgas, 2 = JetA
fuel_type=1.000000
[Views]
eyepoint= -0.1, 0.0, 1.6 //(feet) longitudinal, lateral, vertical distance from reference datum
[flaps.0]
type = 0 // 1 - tail, 2 - lead
system_type = 4 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[folding_wings]
wing_fold_system_type = 4
fold_rates = 0.12, 0.11
[TailHook]
tailhook_length = 4
tailhook_position = -15, 0, -1
cable_force_adjust = 1
[exits]
number_of_exits = 1
exit_rate.0 = 0.5
[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 = 100, 180
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
[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 //Turn AND Bank
[airspeed_indicators]
airspeed_indicator.0 = 0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[airplane_geometry]
wing_area = 128.5 //Square feet
wing_span = 34.0 //Feet
wing_root_chord = 4.9 //Feet
wing_dihedral = 6.3 //Degrees
wing_incidence = 1.5 //Degrees
wing_twist = -3.0 //Degrees
oswald_efficiency_factor= 0.7 //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 = -2.4 //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 = 78.0 //Square feet
htail_span = 11.7 //Feet
htail_pos_lon = -18.3 //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 = 3.2 //Degrees
htail_sweep = 10.0 //Degrees, horizontal tail leading edge
vtail_area = 18.0 //Square feet
vtail_span = 4.8 //Feet, tip to body
vtail_sweep = 40.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -16.2 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 1.5 //Feet, vertical distance from reference point, positive going up
elevator_area = 16.6 //Square feet
aileron_area = 18.3 //Square feet
rudder_area = 6.7 //Square feet
elevator_up_limit = 28.0 //Degrees
elevator_down_limit = 21.0 //Degrees
aileron_up_limit = 20.0 //Degrees
aileron_down_limit = 15.0 //Degrees
rudder_limit = 18.0 //Degrees
elevator_trim_limit = 19.5 //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
[Reference Speeds]
flaps_up_stall_speed = 28.0 //Knots True (KTAS)
full_flaps_stall_speed = 28.0 //Knots True (KTAS)
cruise_speed = 35.0 //Knots True (KTAS)
max_indicated_speed = 130 //Red line (KIAS)
[autopilot]
autopilot_available= 0
flight_director_available= 0
[forcefeedback]
gear_bump_nose_magnitude=6000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=6000 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=6000 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=3250 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750 ; 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
[stall_warning]
type=1
[brakes]
toe_brakes_scale=0
parking_brake=0
[hydraulic_system]
normal_pressure=0.000000
