[fltsim.0] title=SG-38 sim=SG-38 model= panel= sound= texture= kb_reference=sg-38_ref kb_checklists=sg-38_check description=Notes: The SG-38 (Schulgleiter 38) was developed from the Zoegling 31 and Zoegling 35 as well as from the Grunau 9 ui_manufacturer=Rehberg/Schneider/Hofmann ui_type=SG-38 ui_variation=Austrian Colors ui_typerole="Glider" ui_createdby"Wolfgang Piper" description="The SG-38 (Schulgleiter 38) was developed from the Zoegling 31 and Zoegling 35 as well as from the Grunau 9" [fltsim.1] title=SG-38 Paint1 sim=SG-38 model= panel= sound= texture=1 kb_reference=sg-38_ref kb_checklists=sg-38_check description=Notes: The SG-38 (Schulgleiter 38) was developed from the Zoegling 31 and Zoegling 35 as well as from the Grunau 9 ui_manufacturer=Rehberg/Schneider/Hofmann ui_type=SG-38 ui_variation=Spanish Colors ui_typerole="Glider" ui_createdby"Wolfgang Piper" description="The SG-38 (Schulgleiter 38) was developed from the Zoegling 31 and Zoegling 35 as well as from the Grunau 9" [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: 6,3 m\nWing span: 10,40 m\nWeight: 125 kg empty, 210 kg max\nGlide index: 10 at 52 km/h\nVsink: 1.3m/s at 40 km/h \nVmax: 115 km/h\nDesigner: Wolfgang Piper\nDate: June 2004\n Category=airplane [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=-2,0.000000,0.000000 max_number_of_stations=5 station_load.0="180,3.5,0,0,Pilot" //station_load.1="20,-6,0,0,Trimm" empty_weight=244.000000 max_gross_weight=463.000000 empty_weight_roll_MOI=500.000000 empty_weight_pitch_MOI=900.000000 empty_weight_yaw_MOI=700.000000 empty_weight_coupled_MOI=0.000000 [airplane_geometry] wing_area=170.000000 wing_span=34 wing_root_chord=4.8 wing_dihedral=1.000000 wing_incidence=1.000000 wing_twist=-0.999756 oswald_efficiency_factor=0.8 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.5000000 wing_pos_apex_vert=0.000000 htail_area=29.000000 htail_span=9.583333 htail_pos_lon=-12 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=30.000000 vtail_span=6.244998 vtail_sweep=0.000000 vtail_pos_lon=-13.000000 vtail_pos_vert=1.7 elevator_area=9.460000 aileron_area=11.900000 rudder_area=7.700000 elevator_up_limit=25 elevator_down_limit=20 aileron_up_limit=19.480565 aileron_down_limit=14.896903 rudder_limit=23.491270 elevator_trim_limit=19.480565 spoiler_limit=0 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 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 [flight_tuning] cruise_lift_scalar=1.4 parasite_drag_scalar=1.4 induced_drag_scalar=0.95 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.5 pitch_stability=1.0 roll_stability=1.0 yaw_stability=0.8 elevator_trim_effectiveness=2.5 aileron_trim_effectiveness=2 rudder_trim_effectiveness=1.0 [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, -11.7, 0.0, -1.28, 1574.8, 0, 0.5062, 0, 0.5, 2.5, 0.7662, 0, 0, 0, 0, 0 // Gear Tail point.1=1, -0.5, 0.0, -3.85, 1574.8, 2, 0.5062, 0, 0.5, 2.5, 0.837, 0, 0, 3, 0, 0 // Gear Main point.2=2, 0.55, -15.40, 0.8, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 // Wing Tip point.3=2, 0.55, 15.40, 0.8, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 // Wing Tip point.4=2, -11.9, 0, -1.09, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 // Tail point.5=2, 4.0, 0.0, -3.34, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 // Nose point.6=2, 2.95, 0.0 -3.68, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 // Skid //Converted with CPA V.1.05 by Wolfgang Piper //Donnerstag, 11. Juni 2004 gear.center -0.022750 0.000000 -3.684700 gear.center.1 -11.705753 0.000000 -1.231316 scrape.side 0.549135 15.416666 1.340737 scrape.side.1 0.549135 -15.416666 1.340737 scrape.rear -11.887022 0.000000 -1.090107 scrape.front 3.984239 0.000000 -3.347410 [Views] eyepoint=2.35,0,0.94 static_pitch=-2 static_cg_height=3.0 [GeneralEngineData] engine_type=2 fuel_flow_scalar=1.000000 [Reference Speeds] flaps_up_stall_speed=22.000000 full_flaps_stall_speed=24.000000 cruise_speed=30 max_indicated_speed=100 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [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=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 crash_direction1=01000 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 stick_shaker=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [Flaps.0] type=0 span-outboard=0.500000 extending-time=0.000000 system_type=0 [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
