[fltsim.0] title=XFR-4 sim=XFR-4 model= panel= sound= texture= kb_checklists= ui_manufacturer=Ryan Aeronatical Company ui_type=Fighter/Bomber ui_variation=XFR-4 Test Aircraft description=Experimental aircraft using twin engine configuration of Wright Cyclone R-1820-72W radial and Genetral Electric I-16 turbojet.\nFirst flight was on June 25th 1944, entering service in March 1945. \n\nArmament was 4 .50" machine guns with optional warload of 2x 1000lb bombs or 4x wing mounted rockets. This variant had the jet intakes moved from the wing root to NACA type inlets in the fuselage. This resulted in an up to 100 mph speed increase. atc_heavy=0 atc_id=XFR 4 atc_airline= atc_flight_number=2 [General] atc_type=EXPERIMENTAL atc_model=XFR performance=Span : 40'\nLength : 32' 4"\nEmpty Weight : 7,915 lbs\nMaximum Speed : 426 mph\nCeiling : 42,000 ft\nRange : 1,430 miles\n [forcefeedback] gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 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 [WEIGHT_AND_BALANCE] empty_weight = 7915.000 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = 0.000, 0.000, 0.000 max_number_of_stations = 50 station_load.0 = 170.000, -3.000, 0.000, 3.000 ;Moments of Inertia empty_weight_pitch_MOI = 11059.000 empty_weight_roll_MOI = 7243.000 empty_weight_yaw_MOI = 14484.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 11259.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 station_load.1= 1076.000, 9.795, 0.000, 0.000 station_load.2= 850.000, -8.280, 0.000, 0.000 [flight_tuning] cruise_lift_scalar =1.000 parasite_drag_scalar =0.503 induced_drag_scalar =1.000 elevator_effectiveness =0.857 aileron_effectiveness =1.000 rudder_effectiveness =0.508 pitch_stability =1.000 roll_stability =1.000 yaw_stability =1.000 elevator_trim_effectiveness =0.714 aileron_trim_effectiveness =1.000 rudder_trim_effectiveness =1.000 [EFFECTS] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 startup.0=6.062992, 2.257035, -1.198352,fx_engstrt.fx startup.1=6.062992, 2.257035, -1.198352,fx_engstar.fx startup.2=6.062992, 2.257035, -1.198352,fx_engsmoke.fx startup.3=6.062992, 2.257035, -1.198352,fx_engstar.fx startup.4=6.062992, -1.962160, -1.198352,fx_engstar.fx startup.5=6.062992, -2.079905, -1.198352,fx_engsmoke.fx startup.6=6.062992, -2.236898, -1.198352,fx_engstar.fx startup.7=6.062992, -2.217274, -1.198352,fx_engstar.fx [piston_engine] power_scalar =2.002 cylinder_displacement= 202.550 compression_ratio= 8.830 number_of_cylinders= 9 max_rated_rpm= 2500.000 max_rated_hp= 1475.000 fuel_metering_type= 2 cooling_type= 0 normalized_starter_torque= 0.035 turbocharged= 1 max_design_mp= 61.000 min_design_mp= 1.000 critical_altitude= 21500.000 emergency_boost_type= 1 emergency_boost_mp_offset= 15.000 emergency_boost_gain_offset= 0.910 fuel_air_auto_mixture= 0 auto_ignition= 0 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [propeller] thrust_scalar =2.002 propeller_type= 0 propeller_diameter= 9.829 propeller_blades= 3 propeller_moi= 62.170 beta_max= 65.000 beta_min= 13.000 min_gov_rpm= 1800.000 prop_tc= 0.010 gear_reduction_ratio= 2.000 fixed_pitch_beta= 0.000 low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 0 prop_feathering_available= 0 prop_auto_feathering_available= 0 min_rpm_for_feather= 0.000 beta_feather= 0.000 power_absorbed_cf= 0.000 defeathering_accumulators_available= 0 prop_reverse_available= 0 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.12,0.11 ;Percent per second [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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) point.0= 1.000, 6.125, 0.000, -7.950, 3200.000, 0.000, 1.644, 30.000, 0.250, 2.500, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000 point.1= 1.000, -1.528, -7.040, -8.150, 3500.000, 1.000, 2.204, 0.000, 0.540, 2.500, 0.760, 7.500, 8.500, 2.000, 0.000, 0.000 point.2= 1.000, -1.528, 7.040, -8.150, 3500.000, 2.000, 2.204, 0.000, 0.540, 2.500, 0.760, 7.000, 8.000, 3.000, 0.000, 0.000 point.3= 2.000, -0.880, -20.000, -1.450, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -0.880, 20.000, -1.450, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -21.240, 0.000, -2.310, 2400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 8.110, 0.000, -3.810, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_cg_height = 8.100 static_pitch = 3.000 [Views] eyepoint= 0.328, 0.0, 2.49, //(feet) longitudinal, lateral, vertical distance from reference datum [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 4, 1.805, 0.00, 0.18, fx_vclight [fuel] Center1= 0.000, 0.000, 0.000, 225.000, 0.000 Center2= 0.000, 0.000, 0.000, 87.000, 0.000 LeftMain= 0.000, -12.250, 0.000, 82.000, 0.000 RightMain= 0.000, 12.250, 0.000, 82.000, 0.000 External1= 1.940, 0.000, -3.870, 175.000, 0.000 fuel_type=1.000000 number_of_tank_selectors=1 [Views] eyepoint= 0.328, 0.0, 2.09, //(feet) longitudinal, lateral, vertical distance from reference datum [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, 0.826, -19.920, -1.013, fx_navred light.1 = 3, 0.826, 19.920, -1.013, fx_navgre light.3 = 4, 1.805, 0.00, 0.18, fx_vclight [airplane_geometry] wing_area= 380.000 wing_span= 40.000 wing_root_chord= 11.268 wing_dihedral= 4.398 wing_incidence= -1.000 wing_twist= 1.000 oswald_efficiency_factor= 0.930 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 3.192 wing_pos_apex_vert= -2.590 htail_area= 38.360 htail_span= 17.930 htail_pos_lon= -15.406 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 23.040 vtail_span= 4.950 vtail_sweep= 0.000 vtail_pos_lon= -18.038 vtail_pos_vert= 0.000 elevator_area= 23.390 aileron_area= 23.440 rudder_area= 10.930 elevator_up_limit= 26.001 elevator_down_limit= 26.001 aileron_up_limit= 21.497 aileron_down_limit= 20.346 rudder_limit= 28.997 elevator_trim_limit= 19.996 spoiler_limit= 0.000 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [GeneralEngineData] engine_type= 0 Engine.0= 7.795, 0.000, 0.000 fuel_flow_scalar= 1.000 [Reference Speeds] flaps_up_stall_speed= 65.000 full_flaps_stall_speed= 52.000 cruise_speed= 288.725 [keyboard_response] elevator=350.000000,500.000000 aileron=450.000000,1000.000000 rudder=200.000000,1000.000000 [Flaps.0] type= 1 span-outboard= 0.125 extending-time= 5.000 system_type= 0 damaging-speed= 201.000 blowout-speed= 305.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 0.200 flaps-position.0= 0.000, 0.000 flaps-position.1= 6.000, 0.000 flaps-position.2= 9.000, 0.000 flaps-position.3= 15.000, 0.000 flaps-position.4= 20.000, 0.000 flaps-position.5= 28.000, 0.000