[fltsim.0]
title=Schleicher ASK 21 - Front
sim=ask 21
model=
panel=
sound=
texture=
ui_manufacturer=Schleicher
ui_type=ASK 21
ui_variation=White and Red
description=The ASK 21 is a popular training glider but also capable of aerobatics.
kb_reference=ask 21_ref
kb_checklists=ask 21_check
visual_damage=1
atc_heavy=0
atc_id=D-2612
atc_airline=
atc_flight_number=
[General]
atc_type=Schleicher
atc_model=ASK21
performance=Lenghts: 8,35 m\nWingspan: 17 m\nEmpty Weight: 360 Kg\nGlide ratio: 34\nRate of sind: 0,65 m/s\nMaximum speed: 280 km/h
[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=0,0,0
empty_weight_CG_position=-3,0,0
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 = 0.8
parasite_drag_scalar = 0.7
induced_drag_scalar = 0.7
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 = 3
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=9.460000
aileron_area=11.900000
rudder_area=7.700000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=1.896903
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, 5.9166, 0, -1.38, 1574.8, 0, 0.5083, 0, 0.2 , 2.5, 0.5321, 0, 0, 0, 0, 0 // Gear Nose
point.1=1, -1.37, -0.02, -1.35, 1574.8, 2, 0.5083, 0, 0.3 , 2.5, 0.5321, 0, 0, 3, 0, 0 // Gear Main
point.2=1, -1.37, 0.02, -1.35, 1574.8, 2, 0.5083, 0, 0.3 , 2.5, 0.5321, 0, 0, 3, 0, 0 // Gear Main
point.3=2, -0.5, -28.08, 2.424, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 // Wing Tip
point.4=2, -0.5, 28.083, 2.424, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 // Wing Tip
point.5=2, -25.75, 0, 0.25, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 // Tail
point.6=2, 8.7, 0, -0.333, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 // Nose
point.7=2, 3.05, 0, -1.11, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 // Zw.den Rädern
//Converted with CPA by Wolfgang Piper
static_pitch=3
static_cg_height=1.38
[Views]
eyepoint=4.17 ,0, 1.70 // front view
[GeneralEngineData]
engine_type=1
Engine.0=0,0.000000,-0.5000000
fuel_flow_scalar=3.0000000
min_throttle_limit=0.000000
[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=1.0000
rated_N2_rpm=29920.000000
static_thrust=780
afterburner_available=0
reverser_available=0
[jet_engine]
thrust_scalar=1.000
[fuel]
Center1=0.000000,0.000000,0.000000,1.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0
[Reference Speeds]
flaps_up_stall_speed=40.000000
full_flaps_stall_speed=32.000000
cruise_speed=55
max_indicated_speed=152.734375
max_mach=0.229980
[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
[brakes]
toe_brakes_scale=0.7
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
[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=1.200000
system_type=0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_tchdwn_s