[fltsim.0] title=Ka8 V5 sim=Ka8 V5 model= panel= sound= texture= kb_checklists= description=Notes: a real glider of the canadian air cadets ui_manufacturer= Shleicher CGVQM ui_type= ui_variation=C-GVQM atc_heavy=0 atc_id= atc_airline=Air Cadets atc_flight_number= [fltsim.1] title=Ka8 V5 CFZIQ sim=Ka8 V5 model= panel= sound= texture=ziq kb_checklists= description=Notes: a real glider of the canadian air cadets ui_manufacturer= Shleicher CFZIQ ui_type= ui_variation=C-FZIQ atc_heavy=0 atc_id= atc_airline=Air Cadets 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 atc_type= atc_model= [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= -1.500, 0.000, 0.000 max_number_of_stations=5 station_load.0=170.000000, 3.000000, 0.000000, 0.000000, Pilot empty_weight= 419.000 empty_weight_roll_MOI= 480.000 empty_weight_pitch_MOI= 900.000 empty_weight_yaw_MOI= 700.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 684.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [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= 161.000 wing_span= 55.833 wing_root_chord= 3.167 wing_dihedral= -1.000 wing_incidence= 0.000 wing_twist= -1.000 oswald_efficiency_factor= 0.670 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 27.000 htail_span= 9.583 htail_pos_lon= -13.750 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 30.000 vtail_span= 6.245 vtail_sweep= 0.000 vtail_pos_lon= -15.000 vtail_pos_vert= 3.917 elevator_area= 9.460 aileron_area= 11.900 rudder_area= 7.700 elevator_up_limit= 27.502 elevator_down_limit= 22.345 aileron_up_limit= 19.481 aileron_down_limit= 14.897 rudder_limit= 23.491 elevator_trim_limit= 19.481 spoiler_limit= 59.989 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [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= 1.000, -13.700, 0.083, -1.100, 1574.800, 0.000, 0.505, 10.000, 0.100, 2.500, 0.500, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, 0.100, 0.083, -2.800, 1574.800, 1.000, 0.505, 0.000, 0.300, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000 point.2= 2.000, 3.860, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000 point.3= 2.000, 0.260, -24.240, 2.380, 1574.800, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, 0.260, 24.240, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000 point.5= 2.000, -13.850, 0.000, -0.640, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000 point.6= 2.000, 6.260, 0.000, -2.480, 1574.800, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Converted with CPA V.1.05 by Wolfgang Piper //Sonntag, 1. Mai 2003 13:25 static_pitch= 0.000 static_cg_height= 2.750 [GeneralEngineData] engine_type= 2 fuel_flow_scalar=1.000000 [Reference Speeds] flaps_up_stall_speed= 27.000 full_flaps_stall_speed= 21.600 cruise_speed= 45.000 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 [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 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 1.000 system_type= 0 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 39.992, 0.000
