[fltsim.0]
title=Schleicher ASK 21 - Rear
sim=ask 21
model=
panel=
sound=
texture=
ui_manufacturer=Schleicher
ui_type=ASK 21 V3b
ui_variation=Rear seat
description=Notes: The most popular trainer sailplane in the World, Fly from the rear seat...


checklists=
visual_damage=1


atc_heavy=0
atc_id=K21
atc_airline=
atc_flight_number=



[General]
performance=Length: 8,35 m\nWing span:17 m\nWeight:360 Kg empty, 600 kg all up\nDetails:  Best gliding ratio 1:34 \/ 90 km\/h \nMinimum sink rate 072 m\/s \/ 75 km\/h  \nVNE: 280 km\/h\nDesigner: Wolfgang Piper\nGauges: Max Roodveldt\nDate:April 2003
[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


[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1


[WEIGHT_AND_BALANCE]

reference_datum_position=0,0,0
empty_weight_CG_position=-2.5,0,0
max_number_of_stations=5
station_load.0="170, 4.5,0,0,Pilot"       
station_load.1="170, 0, 0,0,Guest"    
empty_weight=794.000000
empty_weight_roll_MOI=2200.000000
empty_weight_pitch_MOI=2000.000000
empty_weight_yaw_MOI=1000.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=1323.000000




[flight_tuning]
cruise_lift_scalar=0.9
parasite_drag_scalar=1.2
induced_drag_scalar=1.2
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.1
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=2
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0



[airplane_geometry]
wing_area=170.000000
wing_span=55.833333
wing_root_chord=4.600000
wing_dihedral=0
wing_incidence=1.647949
wing_twist=1.999512
oswald_efficiency_factor=0.875082
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=1.150000
wing_pos_apex_vert=0.000000
htail_area=25.000000
htail_span=6.333333
htail_pos_lon=-16.416667
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=32.000000
vtail_span=6.449806
vtail_sweep=0.000000
vtail_pos_lon=-14.750000
vtail_pos_vert=3.916667
elevator_area=13
aileron_area=11.900000
rudder_area=7.700000
elevator_up_limit=27
elevator_down_limit=10
aileron_up_limit=17
aileron_down_limit=15
rudder_limit=23.491270
elevator_trim_limit=35
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

//          Lang.   Breit.  Vert.
//          Pos.    Pos.    Pos.
//  0        1       2       3       4     5    6        7       8       9       10      11    12    13    14    15
//-------------------------------------------------------------------------------------------------------------------------------- 
point.0=1, 5.9,   0.0833,  -1.55, 1574.8, 2,   0.5,     0,      0.3,    2.5,    1.1,    0,    0,    3,    0,    0    // Gear Nose
point.1=1, -2.00,     0.0, -1.38, 1574.8, 2,   0.509,   0,      0.4,    2.5,    1.22,   0,    0,    3,    0,    0    // Gear Main(?)
point.2=2, -0.5,   -28.08, 2.44,  787.4,  0,   0,       0,      0,      0,      0,      0,    0,    5,    0,    0    // Wing Tip
point.3=2, -0.5,   28.083, 2.44,  787.4,  0,   0,       0,      0,      0,      0,      0,    0,    6,    0,    0    // Wing Tip
point.4=2, -25.75, 0,      0.25,  787.4,  0,   0,       0,      0,      0,      0,      0,    0,    9,    0,    0    // Tail
point.5=2, 8.7,    0,      -0.333,787.4,  0,   0,       0,      0,      0,      0,      0,    0,    4,    0,    0    // Nose


//Converted with CPA by Wolfgang Piper
//built: 02.02.03 18:41:10 


static_pitch = 3
static_cg_height = 1.12


[Views]
eyepoint=0.9,0.000000,1.9 // rear view



[GeneralEngineData]
engine_type=2
fuel_flow_scalar=1.000000

[Reference Speeds]
flaps_up_stall_speed=40.000000
full_flaps_stall_speed=32.000000
cruise_speed=55
max_indicated_speed=152.734375

[keyboard_response]
elevator=100.000000,150.000000
aileron=100.000000,150.000000
rudder=100.000000,150.000000

[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