[fltsim.0] title=DG-101 sim=DG-100 V6 model= panel= sound= texture= kb_reference=dg-101_ref kb_checklists= ui_manufacturer=Glaser/Dirks ui_type=DG-101 ui_typerole="Glider" ui_createdby"Wolfgang Piper" ui_variation= atc_heavy=0 atc_id= atc_airline= atc_flight_number= description="DG-101 G (gedämpftes Höhenleitwerk und einteilige Haube). Ein Leistungssegler der Standardklasse." [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 Category=airplane [WEIGHT_AND_BALANCE] reference_datum_position=0,0,0 empty_weight_CG_position=-1.2,0,0 max_number_of_stations=1 station_load.0="170,3,0,0,Pilot" station_load.1="100,-0.5,0,0,Ballast" 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 [flight_tuning] //cruise_lift_scalar=1.1 //parasite_drag_scalar=1.2 //induced_drag_scalar=0.70 cruise_lift_scalar=1.1 parasite_drag_scalar=1.10 induced_drag_scalar=0.9 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=2.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_tchdwn_s touchdown=fx_tchdwn_s [airplane_geometry] wing_area=118.000000 wing_span=49.0 wing_root_chord=2.8 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 auto_spoiler_available=0 spoiler_extension_time=0.400000 positive_g_limit_flaps_up=5.500000 positive_g_limit_flaps_down=5.500000 negative_g_limit_flaps_up=-3.500000 negative_g_limit_flaps_down=-3.500000 [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, -0.45, 1574.8, 0, 0.5065, 0, 0.3 , 2.5, 0.3344, 0.5, 0, 0, 0, 0 // Gear Tail point.1=1, 0.75, -0.2, -2.15, 1574.8, 1, 0.5065, 0, 0.30, 2.5, 0.5117, 0.5, 0.8, 2, 0, 0 // Gear Main point.2=1, 0.75, 0.2, -2.15, 1574.8, 2, 0.5065, 0, 0.30, 2.5, 0.5117, 0.5, 0.8, 3, 0, 0 // Gear Main point.3=2, -0.15, -24.3, 1.65, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 // Wing Tip point.4=2, -0.15, 24.3, 1.65, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 // Wing Tip point.5=2, -15.7, 0.0, 0.0, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 // Tail point.6=2, 4.84, 0, -1.23, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 // Nose //Converted with CPA V.1.05 by Wolfgang Piper static_pitch=6.5 static_cg_height=2.20 gear_system_type=0 [Views] eyepoint=1.77,0.00,0.86 static_pitch=5 static_cg_height=1.333910 gear_system_type=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 [autopilot] autopilot_available=0 flight_director_available=0 [direction_indicators] direction_indicator.0=0,0 [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 //[variometers] //variometer.0=54,-116 [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 stick_shaker=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [GeneralEngineData] engine_type=2 fuel_flow_scalar=1.000000 [fuel] fuel_type=1.000000 [pitot_static] pitot_heat=0.000000 [vacuum_system] max_pressure=0.000000 vacuum_type=0 electric_backup_pressure=0.000000 engine_map=1,1,1,1 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=0.000000 [deice_system] structural_deice_type=0 [Water Ballast System] ;/Tank.n = Gallons, Long, Lat, Vert, iValve Tank.0=13.21, 0.0, 0.0, 0.0, 1 //Water 50 l Tank.1=13.21, 0.0, 0.0, 0.0, 1 //Water 50 l NumberOfReleaseValves=2 DumpRate=0.18494 //Gallons per second/ =42 l/min