[fltsim.0]
title=RO57
sim=RO57
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer=IMAM
ui_type= RO57 bis
ui_variation=Regia Aeronautica-97°Gr.Tuffatori-226°Sq.
description=The Ro.57 consisted of an all metal, semi-monocoque fuselage with a steel skeleton and Duralumin structure. The wings were also Duralumin.Powered by two 840 hp (630 kW) Fiat A.74 radial engines giving a maximum speed of 516 km/h, involved the addition of dive brakes, provision for 500 kg bombs and an improved forward firing armament (adding two 20 mm cannon).The resulting aircraft was ordered into production in 1942 and entered service with the 97° Gruppo in 1943. About 50-60 aircraft were delivered
[WEIGHT_AND_BALANCE]
empty_weight= 13068.000
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=170.000000, -3.000000, 0.000000, 3.000000, longitudinal
empty_weight_roll_MOI=80989.000000
empty_weight_pitch_MOI=102454.000000
empty_weight_yaw_MOI=190603.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=19857.000000
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.1 = 3, 1.66, -20.50, -1.430, fx_navred
light.2 = 3, 1.66, 20.35, -1.430, fx_navgre
light.3=4,2.41, 7.96, -4.10 , fx_sm95_scarico //dx eng 0
light.4=4, 2.41, 4.31, -4.10, fx_sm95_scarico //sx eng 0
light.5=4,2.41,-4.54, -4.10, fx_sm95_scarico //dx eng 1
light.6=4, 2.41,-8.10, -4.10, fx_sm95_scarico //sx eng 1
light.7=4, 1.300,0.00,0.100, fx_vclight_ro57 //cabina
[Moments of Inertia]
empty_weight_pitch_MOI= 23052.000
empty_weight_roll_MOI= 15602.000
empty_weight_yaw_MOI= 30691.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 19857.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[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
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.000
induced_drag_scalar =1.000
elevator_effectiveness =1.000
aileron_effectiveness =0.701
rudder_effectiveness =1.000
pitch_stability =0.701
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[piston_engine]
//power_scalar =0.954
power_scalar =1
cylinder_displacement= 130.700
compression_ratio= 6.000
number_of_cylinders= 14
max_rated_rpm= 2400.000
max_rated_hp= 840.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.035
turbocharged= 1
max_design_mp= 46.000
min_design_mp= 1.000
critical_altitude= 17000.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
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=0.600
[propeller]
thrust_scalar=1.000
rotation= -1,1
propeller_type= 0
propeller_diameter= 9.500
propeller_blades= 3
propeller_moi= 23.000
beta_max= 45.000
beta_min= 25.000
min_gov_rpm= 1800.000
prop_tc= 0.010
gear_reduction_ratio= 1.710
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 1
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= 0.000
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
[electrical]
max_battery_voltage=24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=60.0
[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, -16.00, 0.000,-5.250, 1574.800, 0.000, 0.190, 25.000, 0.150, 2.500, 1.020, 5.000, 5.000, 0.000, 0.000, 0.000
point.1= 1.000, 3.3700, -6.000, -7.7000, 1574.800, 1.000, 0.590, 1.1500, 0.210, 2.500, 1.010, 5.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, 3.3700, 6.000, -7.7000, 1574.800, 2.000, 0.590, 1.1500, 0.210, 2.500, 1.010, 5.000, 5.000, 3.000, 0.000, 0.000
point.3= 2.000, 10.533, -1.683, 0.098, 1574.800, 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, -19.592, -1.248, 0.098, 1574.800, 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, 20.827, -1.39, 1.515, 1574.800, 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, -20.827, -1.39, 1.515, 1574.800, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 11.124
static_cg_height= 8.600
gear_system_type= 0
tailwheel_lock = 0
[exits]
number_of_exits = 5
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4
exit_rate.2 = 0.4
exit_rate.3 = 0.4
[Views]
eyepoint=0.78,0.000000,0.26
[fuel]
LeftMain= 0.000, -4.200, 0.300, 110.000, 0.000
RightMain= 0.000, 4.200, 0.300, 110.000, 0.000
fuel_type= 1.000
number_of_tank_selectors= 1
electric_pump= 0
[airplane_geometry]
wing_area= 529.000
wing_span= 51.167
wing_root_chord= 8.083
wing_dihedral= 5.999
wing_incidence= 0.000
wing_twist= 1.000
oswald_efficiency_factor= 0.726
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 77.000
htail_span= 17.167
htail_pos_lon= -24.250
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 37.000
vtail_span= 6.935
vtail_sweep= 0.000
vtail_pos_lon= -24.250
vtail_pos_vert= 10.667
elevator_area= 31.810
aileron_area= 22.900
rudder_area= 13.950
elevator_up_limit= 27.502
elevator_down_limit= 20.626
aileron_up_limit= 19.481
aileron_down_limit= 14.897
rudder_limit= 23.491
elevator_trim_limit= 19.481
spoiler_limit= 59.989
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000
[brakes]
toe_brakes_scale= 1.000
parking_brake= 1
[gear_warning_system]
gear_warning_available= 0
pct_throttle_limit= 0.000
flap_limit_power= 0.000
flap_limit_idle= 0.000
[GeneralEngineData]
engine_type= 0
Engine.0= 8.333, -9.167, -1.250
Engine.1= 8.333, 9.167, -1.250
fuel_flow_scalar= 1.000
min_throttle_limit= 0.000
[Reference Speeds]
flaps_up_stall_speed= 70.000
full_flaps_stall_speed= 56.000
cruise_speed= 250.000
max_indicated_speed= 321.00
[keyboard_response]
elevator= 150.000, 250.000
aileron= 150.000, 250.000
rudder= 150.000, 250.000
[General]
performance=Length:8,80 m\nSpan:12.50 m\nWeight: 5000 kg\nPower: 2× Fiat A.74 R.C.38 14-cylinder air-cooled radial engines, 627 kW (840 hp) each \nRange: 1200 km\nCeiling: 7800m\nmax speed :516km/h\n cruise speed:390 km/h\
atc_type=
atc_model=
[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 700.000
autothrottle_available= 0
pitch_takeoff_ga= 8.000
max_pitch= 10.000
max_pitch_acceleration= 1.000
max_pitch_velocity_lo_alt= 2.000
max_pitch_velocity_hi_alt= 1.500
max_pitch_velocity_lo_alt_breakpoint= 20000.000
max_pitch_velocity_hi_alt_breakpoint= 28000.000
max_bank= 25.000
max_bank_acceleration= 1.800
max_bank_velocity= 3.000
max_throttle_rate= 0.100
nav_proportional_control= 9.000
nav_integrator_control= 0.250
nav_derivative_control= 0.000
nav_integrator_boundary= 2.500
nav_derivative_boundary= 0.000
gs_proportional_control= 9.520
gs_integrator_control= 0.260
gs_derivative_control= 0.000
gs_integrator_boundary= 0.700
gs_derivative_boundary= 0.000
yaw_damper_gain= 0.000
[hydraulic_system]
electric_pumps= 0
engine_map= 1, 1, 0, 0
normal_pressure= 6.931
[stall_warning]
type= 1
[attitude_indicators]
attitude_indicator.0= 1
[turn_indicators]
turn_indicator.0= 1, 0
[Flaps.0]
type= 1
span-outboard= 0.125
extending-time= 5.000
system_type= 0
damaging-speed= 191.000
blowout-speed= 290.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 25.000, 0.000
flaps-position.2= 50.000, 0.000
[direction_indicators]
direction_indicator.0=1,0
