[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