[fltsim.0]
title=R-5
sim=R-5
model=
panel=
sound=
texture=
kb_checklists=
prop_anim_ratio=0.5
atc_id=L-1579
ui_manufacturer=Policarpov
ui_type=R-5
ui_variation=USSR L-1579
description=version 2009.08.12
[General]
atc_type=R-5
atc_model=R-5
editable=0
performance="version 2009.08.10"
[WEIGHT_AND_BALANCE]
max_gross_weight = 8389 // (pounds)
empty_weight = 4788 // (pounds)
reference_datum_position = 0.0, 0.0, 0.0 // (feet) distance from FlightSim Ref. (1/4 chord, centerline).
empty_weight_CG_position = 0.0, 0.0, 0.0
max_number_of_stations =3
station_load.0 = "200.0, -4.65, 0.0, 1.31, Pilot" //Weight, longitudinal, lateral, vertical distance from specified datum
station_load.1 = "200.0, -8.29, 0.0, 0.46, Navigator" //Weight, longitudinal, lateral, vertical distance from specified datum
station_load.2 = "200.0, -11.80, 0.0, 0.0, Cargo" //Weight, longitudinal, lateral, vertical distance from specified datum
;Moments of Inertia
empty_weight_roll_MOI = 8464.0
empty_weight_pitch_MOI = 10136.0
empty_weight_yaw_MOI = 16082.0
empty_weight_coupled_MOI = 0.0
[flight_tuning]
cruise_lift_scalar =1.0
parasite_drag_scalar =1.165
induced_drag_scalar =1.0
elevator_effectiveness =1.0
aileron_effectiveness =1.0
rudder_effectiveness =1.0
pitch_stability =1.1
roll_stability =1.1
yaw_stability =1.0
elevator_trim_effectiveness =1.0
aileron_trim_effectiveness =1.0
rudder_trim_effectiveness =1.0
p_factor_on_yaw = 0.5
hi_alpha_on_roll =1.0
hi_alpha_on_yaw =1.0
torque_on_roll =1.0
gyro_precession_on_roll =1.0
gyro_precession_on_yaw =1.0
[GeneralEngineData]
engine_type = 0
Engine.0 = 9.51, 0.0, 0.0
fuel_flow_scalar = 1.0666
min_throttle_limit = 0.005 // Minimum percent throttle.
[piston_engine]
power_scalar = 1.0
cylinder_displacement = 233.8
compression_ratio = 6.0
number_of_cylinders = 12
max_rated_rpm = 1800.0
max_rated_hp = 730.0
fuel_metering_type = 1
cooling_type = 1
normalized_starter_torque = 0.3
turbocharged = 1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp = 30 //Max design manifold pressure, (inHg)
min_design_mp = 10 //Min design manifold pressure, (inHg)
critical_altitude = 8000.0
emergency_boost_type =0
emergency_boost_mp_offset =0.0
emergency_boost_gain_offset =0.0
fuel_air_auto_mixture =0
auto_ignition =0
max_rpm_mechanical_efficiency_scalar =0.98
idle_rpm_mechanical_efficiency_scalar =1.0
max_rpm_friction_scalar =1.0
idle_rpm_friction_scalar =1.0
emergency_boost_duration =0.0
power_scalar =1.0
[propeller]
thrust_scalar = 1.0
propeller_type = 1.0
propeller_diameter = 13.0
propeller_blades = 2
propeller_moi = 14.0
gear_reduction_ratio = 1.135
fixed_pitch_beta = 13.5
low_speed_theory_limit = 80.0
beta_max =0
beta_min =0
min_gov_rpm =0
prop_tc =0
prop_sync_available =0
prop_deice_available =0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather =0
beta_feather =0
power_absorbed_cf =0
defeathering_accumulators_available=0
prop_reverse_available =0
minimum_on_ground_beta =0
minimum_reverse_beta =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
max_number_of_points=7
; Ref:...0......1.....2......3......4.....5..6......7....8....9...10...11...12..13
point.0= 3, -18.69, 0.0, -2.50, 1200, 0, 0.1, 30.0, 0.3, 1.5, 0.8, 0.0, 0.0, 7
point.1= 1, 1.49, -3.42, -6.56, 1600, 1, 1.1, 0.0, 0.6, 1.5, 0.8, 0.0, 0.0, 2
point.2= 1, 1.49, 3.42, -6.56, 1600, 2, 1.1, 0.0, 0.6, 1.5, 0.8, 0.0, 0.0, 3
; Scrapes
point.3= 2, -1.6, -28.0, 4.00, 800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5
point.4= 2, -1.6, 28.0, 4.00, 800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6
point.5= 2, -29.5, 0.0, 2.00, 800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9
point.6= 2, 8.5, 0.0, -2.10, 800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4
static_pitch = 12.8
static_cg_height = 5.7
gear_system_type =4
[brakes]
parking_brake = 1 // Parking brake available?
toe_brakes_scale = 0.3
differential_braking_scale = 0 // Delta on the amount of brake when the rudder pedals deflected.
[hydraulic_system]
normal_pressure =0.0
[Views]
eyepoint = -5, 0.0, 2.75
[LIGHTS]
//Types: 4=cockpit.
//light.0 = 4, -5.00, 0.00, 2.00,NULL
; Remainder done by FSDS3 / fs9 materials.
[Radios]
// Radio Type = availiable, standby frequency, has glide slope.
Audio.1 = 1
Com.1 = 1, 0
Nav.1 = 0, 0, 0
Adf.1 = 1
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 =200, 1000
aileron =200, 1000
rudder =200, 1000
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro.
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0= 1,0
direction_indicator.1= 2,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro.
attitude_indicator.0 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro.
turn_indicator.0= 2,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt_vega
touchdown=fx_tchdwn_s, 1
[electrical]
autopilot= 0, 0.0, 17.0
avionics_bus= 4, 20.0, 20.0
avionics= 4, 20.0, 20.0
pitot_heat= 4, 0.0, 17.0
light_nav= 4, 0.1, 17.0
light_beacon= 4, 0.1, 17.0
light_landing= 4, 1.0, 17.0
light_panel= 4, 0.1, 17.0
starter1= 3, 20.0, 17.0
avionics= 4, 1.0, 17.0
electric_always_available=0
max_battery_voltage = 28
generator_alternator_voltage = 30
max_generator_alternator_amps = 60
[fuel]
Center1 = 2.13, 0.00, 2.13, 1.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = 0.00, 0.00, 5.88, 82.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = 0.82, 0.00, 0.69, 138.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
manual_transfer_pump=0
[airplane_geometry]
wing_area = 539.64
wing_span = 50.82
wing_root_chord = 6.62
wing_dihedral = 2.5
wing_incidence = 0.0
wing_twist = 0.0
oswald_efficiency_factor = 1.0
wing_winglets_flag = 0
wing_sweep = 2.3
wing_pos_apex_lon = 0.0
wing_pos_apex_vert = 1.0
htail_area = 71.4
htail_span = 15.7
htail_pos_lon = -20.6
htail_pos_vert = 0.0
htail_incidence = 0.0
htail_sweep = 0.0
vtail_area = 7.5
vtail_span = 5.0
vtail_sweep = 0.0
vtail_pos_lon = -20.6
vtail_pos_vert = 0.0
elevator_area = 31.4
aileron_area = 38.7
rudder_area = 17.2
elevator_up_limit = 20.0
elevator_down_limit = 19.0
aileron_up_limit = 32.0
aileron_down_limit = 10.5
rudder_limit = 22.0
elevator_trim_limit = 20.0
spoiler_limit=0.0
spoilerons_available=0
aileron_to_spoileron_gain =0.0
min_ailerons_for_spoilerons =0.0
min_flaps_for_spoilerons =0.0
spoiler_handle_available=0
auto_spoiler_available=0
positive_g_limit_flaps_up=4.0
negative_g_limit_flaps_up=-3.20000
positive_g_limit_flaps_down=2.80000
negative_g_limit_flaps_down=-2.40000
load_safety_factor=1.0
[Reference Speeds] // Knots True (KTAS)
flaps_up_stall_speed =45 // = 51 mph
full_flaps_stall_speed =45
cruise_speed =87 // = 100mph
max_indicated_speed =130 // (KIAS) = 150 mph.
[stall_warning]
type=1
[smokesystem]
smoke.0=0
[gear_warning_system]
gear_warning_available=0
[autopilot]
autopilot_available=1
flight_director_available=0
autothrottle_available=0
default_vertical_speed=0.000000
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
[forcefeedback] // You are on your own here!
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1
crash_magnitude1=10000
crash_direction1=1000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000
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=500
gear_bump_right_duration=250000
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=0.300000
system_type=4
flaps-position.0=0.000000,0.000000
flaps-position.1=40.000001,0.000000
