[fltsim.0]
title=Huetter H-17
sim=Huetter H-17
model=
panel=
sound=
texture=
kb_checklists=Huetter H-17
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 H-17
[electrical]
max_battery_voltage=24
avionics_bus=0, 0 , 0
avionics=0, 0 , 0
additional_system=0, 0 , 0
flap_motor=0, 0 , 0
gear_motor=0, 0 , 0
[WEIGHT_AND_BALANCE]
reference_datum_position = 0.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position= -0.500, 0.000, 0.000
max_number_of_stations= 50
station_load.0=180.000000, 1.850000, 0.000000, -0.500000, Station 1
empty_weight= 355.000
empty_weight_roll_MOI= 285.000
empty_weight_pitch_MOI= 463.000
empty_weight_yaw_MOI= 595.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 575.000
CG_forward_limit= 1.000
CG_aft_limit= 0.000
[fuel]
Center1=0.000000,0.000000,0.000000,50.000000,0.000000
fuel_type= 2.000
number_of_tank_selectors= 1
electric_pump=0
[airplane_geometry]
wing_area= 97.000
wing_span= 31.790
wing_root_chord= 3.28
wing_dihedral= 0.000
wing_incidence= 2.000
wing_twist= 0.000
oswald_efficiency_factor= 0.700
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.770
wing_pos_apex_vert= 0.000
htail_area= 22.000
htail_span= 7.917
htail_pos_lon= -13.750
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 22.000
vtail_span= 5.348
vtail_sweep= 0.000
vtail_pos_lon= -13.750
vtail_pos_vert= 0.000
elevator_area= 9.460
aileron_area= 11.900
rudder_area= 7.700
elevator_up_limit= 25.000
elevator_down_limit= 25.000
aileron_up_limit= 30.626
aileron_down_limit= 30.626
rudder_limit= 30.000
elevator_trim_limit= 19.481
spoiler_limit= 0
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000
//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, -0.100, 0.000, -1.250, 1574.803, 2.000, 0.506, 0.000, 0.150, 2.200, 0.800, 0.000, 0.000, 0.000, 0.000, 0.000
point.1 = 2, 1.950, 16.000, 2.470, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0
point.2 = 2, 1.950, -16.200, 2.470, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0
point.3 = 2, 5.532, -0.100, -0.969, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0
point.4 = 2, -6.750, 0.000, -0.100, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0
point.5 = 0.21, 0.00, -1.53, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.6= 2, 2.95, 0.5, -1.75, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.0= 1.000, -0.600, 0.000, -1.200, 1574.803, 2.000, 0.506, 0.000, 0.150, 2.200, 0.800, 0.000, 0.000, 0.000, 0.000, 0.000
//point.1= 2.000, -2.417, -19.833, 1.250, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
//point.2= 2.000, -2.417, 19.833, 1.250, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
//point.3= 2.000, -11.667, 0.000, -0.600, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
//point.4= 2.000, 3.667, 0.000, -0.98, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
//point.5= 2.000, 3.667, 0.000, -0.98, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.6 = -0.08, -0.04, -1.74, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.7 = -0.08, -0.04, -1.74, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.8 = -0.08, -0.04, -1.74, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.9 = -0.08, -0.04, -1.74, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.10 = -0.08, -0.04, -1.74, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.11 = -0.08, -0.04, -1.74, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.12 = -0.08, -0.04, -1.74, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.13 = 3.10, 0.00, -1.30, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.14 = 3.10, 0.00, -1.30, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.15 = 3.50, 0.00, -1.40, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.16 = 3.50, 0.00, -1.40, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.17 = 3.50, 0.00, -1.40, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
static_pitch= 4.993
static_cg_height= 1.100
[GeneralEngineData]
engine_type = 2
fuel_flow_scalar = 0
//[GeneralEngineData]
//engine_type= 1
//Engine.0= -1.833, 0.000, 0.000
//fuel_flow_scalar= 1.000
//min_throttle_limit=0.000000
//[TurbineEngineData]
//fuel_flow_gain= 0.002
//inlet_area= 0.247
//rated_N2_rpm= 29920.000
//static_thrust= 205.500
//afterburner_available= 0
//reverser_available= 0
[Reference Speeds]
flaps_up_stall_speed= 30.000
full_flaps_stall_speed= 30.000
cruise_speed= 55.000
max_indicated_speed=90.429688
max_mach=0.153467
[keyboard_response]
elevator= 150.000, 250.000
aileron= 150.000, 250.000
rudder= 150.000, 250.000
[Views]
//eyepoint= 1.845, 0.000, 2.563
eyepoint= 2.7, 0.00, 2.0 //(feet) longitudinal, lateral, vertical distance from reference datum
[General]
performance=Length: 21.25 feet\nHeight: 7.2ft\nWing span:40 feet\nAspect Ratio: 10\nEmpty Weight: 355 lbs.\nGross Weight: 575 lbs.\nBest Glide Speed: 48 mph\nStall Speed (level) 28 mph\nVne: 104mph\n\n
atc_type=Glider
atc_model=H-17
[autopilot]
autopilot_available= 0
flight_director_available= 0
[jet_engine]
thrust_scalar=1.000
[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
parasite_drag_scalar=1.400
induced_drag_scalar=0.950
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[direction_indicators]
direction_indicator.0=3,0
[brakes]
toe_brakes_scale=1.000031
parking_brake=1
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[propeller]
thrust_scalar=1.000
[piston_engine]
power_scalar=1.000
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
[Flaps.0]
type= 0
span-outboard= 0.500
extending-time= 0.100
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
