[fltsim.0]
title=Ka8 V5
sim=Ka8 V5
model=
panel=
sound=
texture=
kb_checklists=
description=Notes: Übungs- und Leistungseinsitzer. Gleitzahl 27. Sinkgeschwindigkeit 0.65m\/sec. Baujahr: 1958. Gebaut wurden ca.1200 Stück.

ui_manufacturer=Schleicher
ui_type=Ka 8 V5
ui_variation=
atc_heavy=0
atc_id=K 8
atc_airline=
atc_flight_number=


[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

[General]
performance=Length: 7m\nWing span: 15 m\nWeight: 190 kg leer, 310 kg max.\nDesigner: Wolfgang Piper\nDate: Nov. 2003
[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=-1.5000000,0.000000,0.000000
max_number_of_stations=5
station_load.0="170,3,0,0,Pilot"
empty_weight=419.000000
empty_weight_roll_MOI=480.000000
empty_weight_pitch_MOI=900.000000
empty_weight_yaw_MOI=700.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=684.000000


[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=1.5
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0


[airplane_geometry]
wing_area=161.000000
wing_span=55.833333
wing_root_chord=3.166667
wing_dihedral=-1
wing_incidence=0.000000
wing_twist=-0.999756
oswald_efficiency_factor=0.670429
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=27.000000
htail_span=9.583333
htail_pos_lon=-13.750000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=30.000000
vtail_span=6.244998
vtail_sweep=0.000000
vtail_pos_lon=-15.000000
vtail_pos_vert=3.916667
elevator_area=9.460000
aileron_area=11.900000
rudder_area=7.700000
elevator_up_limit=27.501974
elevator_down_limit=22.345354
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000


[contact_points]

//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

//          Long.   Lat.    Vert.
//          Pos.    Pos.    Pos.
//  0        1       2       3       4     5    6        7       8       9       10      11    12    13    14    15
//-------------------------------------------------------------------------------------------------------------------------------- 
point.0=1, -13.7,  0.083,  -1.1,   1574.8, 0,   0.5048,  10,     0.10,   2.5,    0.5,    0,    0,    0,    0,    0    // Gear Tail
point.1=1,  0.1,   0.083,  -2.8,   1574.8, 1,   0.5048,  0,      0.30,   2.5,    0.7,    0,    0,    2,    0,    0    // Gear Main
point.2=2, 3.86,   0.0   , -2.42,  1574.8, 0,   0,       0,      0,      0,      0,      0,    0,    4,    0,    0    // Skid
point.3=2, 0.26,  -24.24,  2.38,   1574.8, 0,   0,       0,      0,      0,      0,      0,    0,    5,    0,    0    // Wing Tip
point.4=2, 0.26,   24.24 , 2.38,   1574.8, 0,   0,       0,      0,      0,      0,      0,    0,    6,    0,    0    // Wing Tip
point.5=2, -13.85, 0,      -0.64 , 1574.8, 0,   0,       0,      0,      0,      0,      0,    0,    9,    0,    0    // Tail
point.6=2, 6.26,   0,      -2.48,  1574.8, 0,   0,       0,      0,      0,      0,      0,    0,    4,    0,    0    // Nose

//Converted with CPA V.1.05 by Wolfgang Piper
//Sonntag, 1. Mai 2003  13:25


static_pitch=0
static_cg_height=2.75

[GeneralEngineData]
engine_type=2
fuel_flow_scalar=1.000000

[Reference Speeds]
flaps_up_stall_speed=27.000000
full_flaps_stall_speed=21.600000
cruise_speed=45
max_indicated_speed=152.734375


[keyboard_response]
elevator=60.000000,90.000000
aileron=60.000000,90.000000
rudder=60.000000,90.000000


[Views]
eyepoint=2.49,0,0.82

[autopilot]
autopilot_available=0
flight_director_available=0

[direction_indicators]
direction_indicator.0=0,0


[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5#
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1#
crash_magnitude1=10000
crash_direction1=1000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000



[Flaps.0]
type=1
span-outboard=0.500000
extending-time=1.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=39.992454,0.000000

[fuel]
fuel_type=1.000000

[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