[fltsim.0] title=Schweizer v2 sim=Schweizer v2 model= panel= sound= texture= kb_checklists=Schweizer2_32_check kb_reference=Schweizer2_32_ref atc_id=N874GL ui_manufacturer=Schweizer ui_type="2-32 Sailplane" v2 ui_variation="Yellow with red trim" description="Through the late 1960s and much of the 1970s, one aircraft stood apart as the world's highest performance multiseat sailplane: the Schweizer SGS 2 32. Many world soaring records were set in 2 32s in both men's and women's categories, including a distance run of 505 miles." visual_damage=1 [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 [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [General] performance=Length: 6,58 m\nWing span: 15,00 m\nWeight: 235 Kg empty, Max: 525 kg all up\nDetails: Best gliding ratio 1:45\n Minimum sink rate 0.55 m\/s\n VNE: 285 km\/h\nDesigner: Peter Franke\nGauges: Max Roodveldt\nDate: April 2002 [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=-0.75.000000,0.000000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=500.00 empty_weight_roll_MOI=735.000000 empty_weight_pitch_MOI=700.000000 empty_weight_yaw_MOI=1000.000000 empty_weight_coupled_MOI=0.000000 max_gross_weight= 500.000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=0.300 induced_drag_scalar=0.300 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=3.000 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=2.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [fuel] LeftMain=-0.0000,-0.000,0.000,0.000,0.000000 RightMain=-0.0000,0.000,0.00,0.00,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=96.000000 wing_span=49.166667 wing_root_chord=2.166667 wing_dihedral=3.499146 wing_incidence=0.000000 wing_twist=0.999756 oswald_efficiency_factor=0.836806 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=21.000000 htail_span=7.916667 htail_pos_lon=-13.333333 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=45 elevator_down_limit=45 aileron_up_limit=20 aileron_down_limit=12 rudder_limit=35 elevator_trim_limit=45 spoiler_limit=90 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 //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 [contact_points] // 0 1 2 3 4 5 6 7 8 9 10 11 12 13 //Tailwheel point.0= 2, -13.495, 0, -1.233, 1575, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 //Mainwheel point.1= 1, 0.279, 0, -2.720, 1575, 1, 0.504506, 0, 0.183448, 2.5, 0.45, 0.5, 0.5, 2, 0, 0 //L Wingtip point.2= 2, -1.312, -23.73, 1.117, 1575, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 //R Wingtip point.3= 2, -1.312, 23.73, 1.117, 1575, 0, 0, 0, 0, 0, 0, 0, 0 6, 0, 0 //Nose point.4= 2, 5.669, 0, -1.833, 1575, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 static_pitch=7.393798 static_cg_height=2.333910 gear_system_type=0 [GeneralEngineData] engine_type=2 fuel_flow_scalar=1.000000 [Reference Speeds] flaps_up_stall_speed=41.000000 full_flaps_stall_speed=20 cruise_speed=71.087706 max_indicated_speed=152.734375 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=1.781,0.000000,0.328 [autopilot] autopilot_available=0 flight_director_available=0 [direction_indicators] direction_indicator.0=0,0 [Exits] number_of_exits=2 exit_rate.0=0.5 exit_rate.1=0.75 [brakes] toe_brakes_scale=0.610370 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=1 span-outboard=0.500000 extending-time=0.300000 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
