[fltsim.0] title=DG-100 V6 Winde sim=DG-100 V6 model= panel= sound= texture= checklists= description=DG-100 G ( gedämpftes Höhenleitwerk). Die DG-100 wurde von vielen Segelfliegern als eines der schönsten Segelflugzeuge der Standard-Klasse bezeichnet. Erstflug 1974.\n ui_manufacturer=Natur ui_type=Adler ui_variation= atc_heavy=0 atc_id=DG100 atc_airline= 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=Spannweite: 15.0 m\nRüstgewicht: 235 kg,Max.Fluggewicht 418 kg\nBetes Sinken: 0.59m\/sec bei 74 km\/h\nBestes Gleiten 39.2 bei 105 km\/h\n [WEIGHT_AND_BALANCE] reference_datum_position=0,0,0 empty_weight_CG_position=-1.5,0,0 max_number_of_stations=1 station_load.0="170,3,0,0,Pilot" empty_weight=519.000000 max_gross_weight=922.000000 empty_weight_roll_MOI=700.000000 empty_weight_pitch_MOI=800.000000 empty_weight_yaw_MOI=1000.000000 empty_weight_coupled_MOI=0.000000 [fuel] Center1=0.000000,0.000000,0.000000,10.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=0 [flight_tuning] cruise_lift_scalar=1.1 parasite_drag_scalar=0.5 induced_drag_scalar=0.5 elevator_effectiveness=1.9 aileron_effectiveness=1.9 rudder_effectiveness=1.9 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.2 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [airplane_geometry] wing_area=119.000000 wing_span=54.500000 wing_root_chord=2.166667 wing_dihedral=1.499146 wing_incidence=0.000000 wing_twist=0.999756 oswald_efficiency_factor=0.756348 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=22.000000 htail_span=7.916667 htail_pos_lon=-13.750000 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=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=14.896903 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, -14, -0.083, -0.166, 1574.8, 0, 0.5065, 0, 0.3 , 2.5, 0.3344, 0.5, 0.5, 0, 0, 0 // Gear Tail point.1=1, 0.75, 0.0833, -2.083, 1574.8, 1, 0.5065, 0, 0.30, 2.5, 0.5117, 0.5, 0.5, 2, 0, 0 // Gear Main point.2=1, 0.75, -0.083, -2.083, 1574.8, 2, 0.5065, 0, 0.30, 2.5, 0.5117, 0.5, 0.5, 3, 0, 0 // Gear Main point.3=1, 0.6666, 0.0833, -2.083, 1574.8, 0, 0, 0, 0.30, 2.5, 0.5627, 0, 0, 1, 0, 0 // Gear Main point.4=2, 0.8333, -25.08, 2.0833, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 // Wing Tip point.5=2, 0.8333, 25.083, 2.0833, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 // Wing Tip point.6=2, -14, 0, -0.083, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 // Tail point.7=2, 4.1666, 0, -1.25, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 // Nose //Converted with CPA V.1.05 by Wolfgang Piper //Sonntag, 9. Februar 2003 13:25 static_pitch=5 static_cg_height=1.333910 gear_system_type=0 [GeneralEngineData] engine_type=1 Engine.0=0,0.000000,0.000000 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [TurbineEngineData] fuel_flow_gain=0.002170 inlet_area=6 rated_N2_rpm=29920.000000 static_thrust=900 afterburner_available=0 reverser_available=0 [Reference Speeds] flaps_up_stall_speed=41.000000 full_flaps_stall_speed=32.800000 cruise_speed=50 max_indicated_speed=152.734375 max_mach=0.229980 [keyboard_response] elevator=60.000000,90.000000 aileron=60.000000,90.000000 rudder=60.000000,90.000000 [Views] eyepoint=2.358104,0.000000,1.358473 [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 [brakes] toe_brakes_scale=1.000031 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [Flaps.0] type=0 span-outboard=0.500000 extending-time=0.000000 system_type=0 [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=4 ;(feet) tailhook_position=-21.0, 0.0, -0.81, ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=1.4
