[fltsim.0]
title=XFR-1
sim=XFR-1
model=
panel=
sound=
texture=
kb_checklists=
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.
ui_manufacturer=Ryan Aeronatical Company
ui_type=Fighter/Bomber
ui_variation=XFR-1 Test Aircraft
atc_heavy=0
atc_id=XFR 1
atc_airline=
atc_flight_number=1
[General]
atc_type=EXPERIMENTAL
atc_model=XFR
performance=Span : 40'\nLength : 34' 6"\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 =0.800
induced_drag_scalar =1.000
elevator_effectiveness =0.858
aileron_effectiveness =1.000
rudder_effectiveness =0.509
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =0.715
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 =1.806
cylinder_displacement= 202.550
compression_ratio= 8.830
number_of_cylinders= 9
max_rated_rpm= 2500.000
max_rated_hp= 1425.000
fuel_metering_type= 2
cooling_type= 0
normalized_starter_torque= 0.035
turbocharged= 1
max_design_mp= 53.000
min_design_mp= 1.000
critical_altitude= 21500.000
emergency_boost_type= 1
emergency_boost_mp_offset= 12.000
emergency_boost_gain_offset= 0.840
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 =1.806
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, 2.09, //(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
[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= 0.899
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
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
[direction_indicators]
direction_indicator.0=1,0
[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
