//Short S.25V Sandringham flight dynamics. Jens B. Kristensen, 23 june 2005. [fltsim.0] title=Short Sandringham DNL sim=Short Sandringham model=Sand_6 panel= sound= texture=DNL kb_reference=Sandringham_ref description=Short S.25V Sandringham\n\nModel, flight dynamics and textures by Jens B. Kristensen may 2005.\n\nLN-IAV 'Kvitbjørn' of Norwegian Airlines 1945-47. ui_manufacturer=Short ui_type=Sandringham ui_variation=2. Norwegian Air Lines Mk.6 atc_heavy=0 atc_id=LN-LAI atc_airline=Scandinavian atc_flight_number=1947 [fltsim.1] title=Short Sandringham SAS sim=Short Sandringham model=Sand_6 panel= sound= texture=SAS kb_reference=Sandringham_ref description=Short S.25V Sandringham\n\nModel, flight dynamics and textures by Jens B. Kristensen may 2005.\n\nLN-LMK 'Polarbjørn' of SAS, taken over from Norwegian Air Lines. ui_manufacturer=Short ui_type=Sandringham ui_variation=3. SAS Mk.6 atc_heavy=0 atc_id=LN-LMK atc_airline=Scandinavian atc_flight_number=1950 [fltsim.2] title=Short Sandringham 5 BOAC sim=Short Sandringham model= panel= sound= texture=BOAC_Mk5 kb_reference=Sandringham_ref description=Short S.25V Sandringham\n\nModel, flight dynamics and textures by Jens B. Kristensen may 2005.\n\nSandringham 5 G-AHZA 'Penzance' of B.O.A.C. 1947-50 ui_manufacturer=Short ui_type=Sandringham ui_variation=1. BOAC Mk.5 atc_heavy=0 atc_id=G-AHZA atc_airline=SPEED BIRD atc_flight_number=1947 [fltsim.3] title=Short Sandringham 2 Aerolineas Argentinas sim=Short Sandringham model= panel= sound= texture=LVACT kb_reference=Sandringham_ref description=Short S.25V Sandringham\n\nModel, flight dynamics and textures by Jens B. Kristensen may 2005.\n\nSandringham 2 LV-ACT 'Paraguay' of Aerolineas Argentinas 1947-62 ui_manufacturer=Short ui_type=Sandringham ui_variation=4. Aerolineas Argentinas Mk.2 atc_heavy=0 atc_id=LV-ACT atc_airline= atc_flight_number=1960 [General] atc_type=Short atc_model=S25V editable=0 performance=Wingspan: 113' \nLength: 86'3''\nEmpty weight: 41000 lbs, Max. take-off 56000 lbs\nEngines: 4 Pratt&Whitney Twin Wasp 14-cylinder radial, 1200 HP each for takeoff.\nMaximum Speed 238 mph\/ 212 kts\nMax cruising speed 221 mph\/ 196 kts\nService ceiling: 18000 ft [weight_and_balance] max_gross_weight = 56000 empty_weight = 32500 reference_datum_position = 0, 0, 0 empty_weight_CG_position = -1, 0, -3 empty_weight_pitch_MOI = 217000 empty_weight_roll_MOI = 484170 empty_weight_yaw_MOI = 700000 empty_weight_coupled_MOI = 0 max_number_of_stations = 8 //Note: Numbers of passengers etc. varied between versions. station_load.0 = 360, 0,0,0, Pilots (2) station_load.1 = 540, 0,0,0, Other crew (3) station_load.2 = 6290, 0,0,0, 37 pax station_load.3 = 2000, 0,0,0, Freight [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 0 fuel_flow_scalar = 1 engine.0 = 3.0, -27.2, 1, engine.1 = 6.0, -13.8, 1, engine.2 = 6.0, 13.8, 1, engine.3 = 3.0, 27.2, 1, [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 number_of_tank_selectors = 1 LeftMain = 0, -7, 2.43, 625, 0 LeftAux = 0, -19.62, 2.43, 548, 0 RightMain = 0, 7, 2.43, 625, 0 RightAux = 0, 19.62, 2.43, 548, 0 electric_pump=0 [contact_points] static_pitch = 1 static_cg_height = 11.5 max_number_of_points = 18 point.0 = 4, -27.5, 0, -13.1207, 3500, 0, 0, 0, 0.2, 6.5, 0.4, 0, 0, 0, 0, 0 point.1 = 4, -3, -4.6999, -13.5, 3500, 0, 0, 0, 0.55, 5.2, 0.4, 0, 0, 2, 0, 0 point.2 = 4, -3, 4.6999, -13.5, 3500, 0, 0, 0, 0.55, 5.2, 0.4, 0, 0, 3, 0, 0 point.3 = 4, 25.578, 0, -13.552, 3500, 0, 0, 20, 0.2, 6.5, 0.6, 0, 0, 0, 0, 0 point.4 = 4, 0, -34.8, -11.0, 2500, 0, 0, 0, 0.5, 8, 0.45, 0, 0, 2, 0, 0 point.5 = 4, 0, 34.8, -11.0, 2500, 0, 0, 0, 0.5, 8, 0.45, 0, 0, 3, 0, 0 point.6 = 2, -6.4, -56, 0, 900, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.7 = 2, -6.4, 56, 0, 900, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.8 = 2, -62.113, 0, -2.5, 900, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.9 = 2, 21.2123, 0, -4.8005, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 point.10 = 2, -54, -17.4, -1.25, 500, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.11 = 2, -54, 17.4, -1.25, 500, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 //to activate the pushback feature, enable these lines: //point.12 = 1, -27.5, 0, -18, 3500, 0, 0, 0, 0.5, 3.2, 0.5, 0, 0, 2, 0, 0 //point.14 = 1, 5, -12.4, -18, 2500, 0, 0, 0, 0.5, 5.5, 0.5, 0, 0, 2, 0, 0 //point.15 = 1, 5, 12.4, -18, 2500, 0, 0, 0, 0.5, 5.5, 0.5, 0, 0, 3, 0, 0 [keyboard_response] elevator = 350.000000, 500.000000 aileron = 450.000000, 1000.000000 rudder = 200.000000, 1000.000000 [forcefeedback] ground_bumps_magnitude1 = 1800 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5.0 ground_bumps_slope1 = 0.6 ground_bumps_magnitude2 = 1900 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.085 ground_bumps_slope2 = 0.65 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 3500000 [airplane_geometry] wing_area = 1500.0 wing_span = 114 wing_root_chord = 18 wing_dihedral = 2.0 wing_incidence = 2.0 wing_twist = -3.0 oswald_efficiency_factor = 0.65 wing_winglets_flag = 0 wing_sweep = 4.3 wing_pos_apex_lon = 4.5 wing_pos_apex_vert = 3 htail_area = 135.0 htail_span = 36.0 htail_pos_lon = -43.2 htail_pos_vert = 0 htail_incidence = 0.0 htail_sweep = 12.0 vtail_area = 114.0 vtail_span = 18 vtail_sweep = 18.0 vtail_pos_lon = -45 vtail_pos_vert = 0 elevator_area = 80.0 aileron_area = 66.0 rudder_area = 64.0 elevator_up_limit = 26.0 elevator_down_limit = 18.0 aileron_up_limit = 15.0 aileron_down_limit = 9.0 rudder_limit = 29.0 elevator_trim_limit = 15.0 spoiler_limit = 57.0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 spoilerons_available = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 electric_always_available = 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 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [Views] eyepoint=11.246, -1.538, -2.15 //(feet) longitudinal, lateral, vertical distance from reference datum [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.50 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees, KIAS flaps-position.1=9 // degrees, KIAS flaps-position.2=18 // degrees, KIAS flaps-position.3=27 // degrees, KIAS flaps-position.4=35 // degrees, KIAS damaging-speed=155 // KIAS blowout-speed=165 // KIAS [Reference Speeds] flaps_up_stall_speed=83.000000 full_flaps_stall_speed=70.000000 cruise_speed=167 max_indicated_speed=255.000000 [lights] light.0 = 3, -3.4, -56.59, 0.88, fx_navred, light.1 = 3, -3.4, 56.59, 0.88, fx_navgre, light.2 = 4, 10.5, 0, -4, fx_vclighth, light.3 = 4, 4.0, 0, -2, fx_vclighth, [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 default_bank_mode=2 //Default to Heading Hold [piston_engine] power_scalar = 1.0 //Piston power scalar cylinder_displacement= 130.71 //Cubic inches per cylinder compression_ratio= 6.7 //Compression ratio number_of_cylinders=14 //Number of cylinders max_rated_rpm= 2700 //Max rated RPM max_rated_hp= 1200 //Max rated HP fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque= 0.3 //Starter torque factor turbocharged= 1 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp= 47 //Max design manifold pressure, (inHg) min_design_mp= 10 //Min design manifold pressure, (inHg) critical_altitude= 7000 //Altitude to which the turbocharger will provide max design manifold pressure (feet) emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction [propeller] thrust_scalar = 1.0 //Propeller thrust scalar propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter= 11.53 //Propeller Diameter, (feet) propeller_blades= 3 //Number of propeller blades propeller_moi= 40.2 //Propeller moment of inertia beta_max= 35.0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 18.0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm= 1400 //Miminum governed RPM prop_tc= 0.1 //Prop time-constant gear_reduction_ratio= 1.778 //Propeller gear reduction ratio fixed_pitch_beta= 0.0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit= 80.0 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available= 1 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available= 1 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather= 700.0 //Minimum RPM for prop feathering beta_feather= 89.5 //Feathering pitch angle (degrees) power_absorbed_cf= 0.9 //Coefficient of friction for power absorbed by propeller in feather defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available= 0 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta= 0.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta= 0.0 //Minimum pitch angle in reverse, (degrees) feathering_switches = 1 //Switches which invoke feathering rotation=1,1,1,1 [brakes] toe_brakes_scale=1.0 parking_brake=0 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,1 normal_pressure=6.930556 [stall_warning] type=-1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 0 Nav.2=1, 0, 0 Adf.1=1 Adf.2=1 Transponder.1=1 Marker.1=1
