[fltsim.0]
title=L13SE Vivat
sim=l13SEvivat
model=
panel=
sound=
texture=
checklists=
ui_manufacturer=Aerotechnik
ui_variation=OK-9110
ui_type=L-13SE
atc_id=OK-9110
atc_flight_number=9110
atc_airline=Aero club
description=The L13 Vivat is an excellent all-metal two-place motorglider developed from the L13 Blanik. OK-9110 was made in 1989, it is in Zamberk - Aero club Airport.\nVersion 2.0\nAuthor: Jan Moravec, november 2004\[email protected]\n


[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


[General]
performance=Wingspan: 16,8 m \nLengt: 8.3 m \nHeight: 2.3 m \nWing Area: 20.2 m2 \nMax. Take-off Weight: 705 kg \nWeight Empty: 473 kg \nEngine: Walter Mikron S III \nEngine power: 48kW \nFuel: 50 l \nFuel consumption: 14 – 16 I\/h \nRange: 580km \nMax. Allowed Speed: 230 km\/h \nMin. Stalling Speed: 61 km\/h \nBest Glide Ratio at 90 km\/h: 1:24 \nMin. Rate of Sink: 0.97 m\/s \nG - limits: +5g \/ -2.5g
[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=-1.500000,0.000000,0.000000
max_number_of_stations=2
station_load.0=198.3468,0.000000,-1.500000,0.000000
station_load.1=142.3468,0.000000,1.500000,0.000000
empty_weight=1043.916500
empty_weight_roll_MOI=3900.000000
empty_weight_pitch_MOI=5000.000000
empty_weight_yaw_MOI=2900.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=1555.077700

[flight_tuning]
cruise_lift_scalar     = 1.0
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
elevator_effectiveness = 1.1
aileron_effectiveness  = 0.45
rudder_effectiveness   = 1.0
pitch_stability        = 1.5
roll_stability         = 1.0
yaw_stability          = 1.3
elevator_trim_effectiveness = 2.2
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0

[fuel]
Center1=-7.000000,0.000000,0.000000,13.20000,0.000000

fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area=218.000000
wing_span=55.750000
wing_root_chord=3.166667
wing_dihedral=3.499146
wing_incidence=0.999756
wing_twist=0.999756
oswald_efficiency_factor=1.324142
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=20.000000
htail_span=8.333333
htail_pos_lon=-15.416667
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=22.000000
vtail_span=5.347897
vtail_sweep=0.000000
vtail_pos_lon=-13.750000
vtail_pos_vert=3.916667
elevator_area=16.800000
aileron_area=14.000000
rudder_area=6.600000
elevator_up_limit=32.356059
elevator_down_limit=25.210143
aileron_up_limit=34.000000
aileron_down_limit=17.761692
rudder_limit=30.000000
elevator_trim_limit=49.274370
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                        <0=none,1=wheel, 2=scrape, 3=float>
        //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
        //14 Airspeed limit for retraction     (KIAS)
        //15 Airspeed that gear gets damage at (KIAS)                    
           0          1       2        3        4           5         6        7       8        9        10       11       12       13       14      15
point.0=1.000000,-16.000000,0.000000,-1.100000,961.183563,0.000000,0.509705,60.000000,0.149129,2.500000,1.049164,1.000000,1.000000,0.000000,0.000000,0.000000
point.1=1.000000,2.000000,  0.000000,-4.150000,961.183563,2.000000,0.509705,0.000000,0.309221,2.000000,0.460446,1.000000,1.000000,3.000000,0.000000,0.000000
point.2=2.000000,2.416667,-25.833333,-1.703333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.3=2.000000,2.416667,25.833333,-1.703333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.4=2.000000,-18.666667,0.000000,-1.086667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.5=2.000000,8.000000,0.000000,-3.900000 ,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=8.400000
static_cg_height=3.454431
gear_system_type=0

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=0.400000
flaps-position.0=0.000000,0.000000
flaps-position.1=6.000000,0.000000
flaps-position.2=16.000000,0.000000

[GeneralEngineData]
engine_type=0
Engine.0=6.333333,0.000000,1.000000
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000

[piston_engine]
//power_scalar = 1.0
//cylinder_displacement= 38.75
//number_of_cylinders=4         
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000
cylinder_displacement=83.060000
compression_ratio=8.000000
number_of_cylinders=5
max_rated_rpm=2800.000000
max_rated_hp=68.000000
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.300000
turbocharged=0
max_design_mp=0.000000
min_design_mp=0.000000
critical_altitude=0.000000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=0
auto_ignition=0

[propeller]
thrust_scalar = 1.0 
propeller_type=0
propeller_diameter=4.416667
propeller_blades=2
propeller_moi=3.119907
beta_max=9.460870
beta_min=15.000000
min_gov_rpm=1400.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=20.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000

[Reference Speeds]
flaps_up_stall_speed=35.000000
full_flaps_stall_speed=28.000000
cruise_speed=100.339287
max_indicated_speed=105.000000

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=0.702657,-0.676131,1.546421

[autopilot]
autopilot_available=0
flight_director_available=0

[direction_indicators]
direction_indicator.0=1,0

[brakes]
toe_brakes_scale=1.000031
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=19.996227
flap_limit_idle=25.897692

[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[TailHook]
tailhook_length=3.0                           ;(feet)
tailhook_position=0.0, 0.0, 3.5            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0