[fltsim.0] title=Schweizer 2-32 Sailplane sim=Schweizer2_32 model= panel= sound= texture= kb_checklists=Schweizer2_32_check kb_reference=Schweizer2_32_ref atc_id=N700MS ui_manufacturer=Schweizer ui_type=2-32 Sailplane ui_variation=Yellow with gold and blue 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 [General] atc_type=Schweizer atc_model= editable=0 performance=Maximum Speed\t\n137 kts 158 mph 254 kmh\n\nEngine\t\nnone\n\nGlide Ratio\t\n36 to 1\n\nEmpty Weight\t\n850 lb 386 kg\n\nLength\t\n26.75 ft \t 8.78 m\n\nWingspan\n57 ft\t 18.7 m\n\nWing Area\t\n180 sq ft \t 19.37 m2\n\nAspect Ratio\t\n18.05\n\nMaximum L\/D (Calculated) \t\n~57 kts ~66 mph ~106 kmh\n\nMinimum Sink (Calculated) \t\n~47 kts ~54 mph\t ~87 kmh\n\nSeating\t\nUp to 2\n\nUseful Load\t\n580 lb \t264 kg [WEIGHT_AND_BALANCE] max_gross_weight = 1430 // (pounds) empty_weight = 1000 // (pounds) reference_datum_position = 1.25, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -1.00, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = 170, -0.8, 0.0, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = 170, -3.3, 0.0, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 1800 empty_weight_roll_MOI = 2400 empty_weight_yaw_MOI = 1800 empty_weight_coupled_MOI = 0.0 [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 = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [GeneralEngineData] engine_type = 2 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop fuel_flow_scalar = 0 //Fuel flow scalar [pitot_static] vertical_speed_time_constant = 4 //Increasing this value will cause a more instantaneous reaction in the VSI //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] point.0=1, -2.0, 0.0, -2.5, 1574.8, 2, 0.509, 0.0, 0.40, 2.5, 1.22, 0.0, 0.0, 3, 0.0, 0.0 point.1=2, -1.25, -28.5, 0.5, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5, 0.0, 0.0 point.2=2, -1.25, 28.5, 0.5, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6, 0.0, 0.0 point.3=2, -15.42, 0.0, -0.7, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9, 0.0, 0.0 point.4=2, 6.25, 0.0, -2.2, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4, 0.0, 0.0 static_pitch = -4.65 static_cg_height = 2.17 [Views] eyepoint = 2.0, 0.0, 1.6 [flaps.0] type = 0 // 1 - tail, 2 - lead span-outboard = 0.5 // 0.0 .. 1.0 extending-time = 0 // seconds flaps-position.0 = 0 // degrees, KIAS damaging-speed = 250 // KIAS blowout-speed = 300 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 0 Com.1 = 1, 0 Nav.1 = 0, 0, 0 Adf.1 = 0 Transponder.1 = 0 Marker.1 = 0 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator = 160, 360 aileron = 160, 360 rudder = 160, 360 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type = 4 direction_indicator.0=0,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks [airplane_geometry] wing_area = 180.0 //Square feet wing_span = 57.0 //Feet wing_root_chord = 4.6 //Feet wing_dihedral = 3.5 //Degrees wing_incidence = 3.0 //Degrees wing_twist = -2.0 //Degrees oswald_efficiency_factor= 1.0 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 0.0 //Degrees, wing leading edge wing_pos_apex_lon = -0.5 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up htail_area = 21.0 //Square feet htail_span = 7.9 //Feet htail_pos_lon = -17.3 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up htail_incidence = 0.0 //Degrees htail_sweep = 0.0 //Degrees, horizontal tail leading edge vtail_area = 17.0 //Square feet vtail_span = 4.7 //Feet, tip to body vtail_sweep = 0.0 //Degrees, vertical tail leading edge vtail_pos_lon = -16.0 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 3.9 //Feet, vertical distance from reference point, positive going up elevator_area = 16.0 //Square feet aileron_area = 14.7 //Square feet rudder_area = 6.0 //Square feet elevator_up_limit = 26.0 //Degrees elevator_down_limit = 26.0 //Degrees aileron_up_limit = 30.0 //Degrees aileron_down_limit = 30.0 //Degrees rudder_limit = 30.0 //Degrees elevator_trim_limit = 15.0 //Degrees spoiler_limit = 70.0 //Degrees spoilerons_available = 0 //Spoilerons Available? aileron_to_spoileron_gain = 0 //Aileron to spoileron gain min_ailerons_for_spoilerons = 0 //Degrees min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed = 40.0 //Knots True (KTAS) full_flaps_stall_speed = 40.0 //Knots True (KTAS) cruise_speed = 47.0 //Knots True (KTAS) [autopilot] autopilot_available= 0 flight_director_available= 0 [forcefeedback] ground_bumps_magnitude1=2500 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=10.0 ground_bumps_slope1=0.300 ground_bumps_magnitude2=350 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds