[fltsim.0]
title=Sukhoi_SU_31
sim=SU_31
model=
panel=
sound=
texture=
panel_alias =
sound_alias =
kb_checklists=
kb_reference=
atc_id=N711SU
ui_manufacturer=Sukhoi
ui_type=SU_31
ui_variation=Blue, Silver & Orange Custom
description=Russian built aerobatic plane. This plane quite possibly has the highest performance envelope of any prop plane in the world. If it can be done in a prop plane, this plane can do it.
atc_heavy=0
atc_airline=
atc_flight_number=
editable=1 

[General]
atc_type=
atc_model=SU31
performance=SU-31 Specifications\nLength 22.7 ft.\nHeight 9.1 ft.\nWingspan 25.7 ft.\nEngine (Radial) 360+ hp 9 Cylinders\nLG Track 8.0 ft.\nWheel Base 16.0 ft.\nEmpty Weight 1,650 lbs.\nMax Load 770 lbs.\nMax Take-off Weight 2,420 lbs.\nFuel, fuselage 129.3 lbs., 20.5 gals.\nFuel, wing 351.5 lbs., 55.8 gals.\nFuel, total 480.8 lbs, 76.3 gals.\nOil 11 liters aerobatic, 20 lbs.\nSmoke 8.4 gals., 57 lbs.\nG limits +12 -10\nSpar factory test +- 23\nRoll rate 400° sec.\\Rate of climb 3,543 fpm\nCruise speed\nHigh speed 185 mph\nLong range 130 mph\nStall speed 66 mph\nVne 279 mph\nVmo 241 mph\nVa 229 mph\nTakeoff run @ sl minimum weight 363 ft.\nDon Halcom
editable=1
Category=airplane
 
[WEIGHT_AND_BALANCE]
max_gross_weight =2420.0
empty_weight =1650.00000

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 0.000, 0.000, 0.000

max_number_of_stations =1


;Moments of Inertia
empty_weight_pitch_MOI   =1050.00000
empty_weight_roll_MOI    =583.00000
empty_weight_yaw_MOI     =1255.00000
empty_weight_coupled_MOI =0.00000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.0= 170, -3.700, 0.000, 0.800

[pitot_static]
vertical_speed_time_constant = 1.0              //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000

[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0

                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus       = 0, 10, 9.5
avionics           = 1, 5 , 9.5
additional_system  = 0, 20, 9.5
marker_beacon      = 1, 2 , 9.0
fuel_pump          = 0, 5 , 9.0

[flight_tuning]
cruise_lift_scalar     =1.00000
parasite_drag_scalar   =1.00000
induced_drag_scalar    =1.00000
elevator_effectiveness =1.00000
aileron_effectiveness  =1.00000
rudder_effectiveness   =1.00000
pitch_stability        =1.00000
roll_stability         =1.00000
yaw_stability          =1.00000
elevator_trim_effectiveness =1.00000
aileron_trim_effectiveness  =1.00000
rudder_trim_effectiveness   =1.00000
hi_alpha_on_roll=1.00000
hi_alpha_on_yaw=1.00000
p_factor_on_yaw=1.00000
torque_on_roll=1.00000
gyro_precession_on_roll=1.00000
gyro_precession_on_yaw=1.00000


[GeneralEngineData]
engine_type =0
Engine.0 =4.000, 0.000, 0.000
fuel_flow_scalar=1.00000
min_throttle_limit=0.000000


[piston_engine]
power_scalar =1.00000
cylinder_displacement=100.00000
compression_ratio=8.00000
number_of_cylinders=9
max_rated_rpm=2700.00000
max_rated_hp=400.00000
fuel_metering_type=0
cooling_type=0
normalized_starter_torque=0.20000
turbocharged=1
max_design_mp=29.92000
min_design_mp=0.00000
critical_altitude=20000.00000
emergency_boost_type=0
emergency_boost_mp_offset=0.00000
emergency_boost_gain_offset=0.00000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.00000
idle_rpm_mechanical_efficiency_scalar=1.00000
max_rpm_friction_scalar=1.00000
idle_rpm_friction_scalar=2.00000
emergency_boost_duration=0.00000

[propeller]
thrust_scalar =1.00000
propeller_type=0
propeller_diameter=7.50000
propeller_blades=3
propeller_moi=11.05457
beta_max=40.00000
beta_min=15.00000
min_gov_rpm=800.00000
prop_tc=0.10000
gear_reduction_ratio=1.00000
fixed_pitch_beta=0.00000
low_speed_theory_limit=80.00000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.00000
beta_feather=0.00000
power_absorbed_cf=0.00000
defeathering_accumulators_available=0 
prop_reverse_available=0
minimum_on_ground_beta=0.00000
minimum_reverse_beta=0.00000



        //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

[contact_points]

max_number_of_points =7

static_pitch = 9.700
static_cg_height = 3.850
gear_system_type=4
tailwheel_lock=0
point.0= 1, -14.000, 0.000, -1.900, 1181, 2, 0.300, 30.000, 0.296, 2.500, 1.000, 0.000, 0.000, 0
point.1= 1, 1.900, -3.900, -4.520, 1575, 1, 0.523, 0.000, 0.400, 4.000, 1.000, 0.000, 0.000, 2
point.2= 1, 1.900, 3.900, -4.520, 1575, 2, 0.523, 0.000, 0.400, 4.000, 1.000, 0.000, 0.000, 3
point.3= 2, -3.800, -12.700, -0.760, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.4= 2, -3.800, 12.700, -0.760, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
point.5= 2, -15.400, 0.000, 0.000, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.6= 2, 7.500, 0.000, 0.000, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4


[Views]
eyepoint = -4.2, 0.0, 2.5


[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1       = 1
Com.1         = 1, 1
Nav.1         = 1, 1, 1
Adf.1         = 1
Transponder.1 = 1
Marker.1      = 1

[SMOKESYSTEM]
smoke.0=1.00, 0.00, -1.30, fx_smoke_w

[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 = 100,  180
aileron  = 200, 1000
rudder   = 200, 1000


[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=1,0

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
light.0 = 3,  -1.62, -13.28,-0.15, fx_navred
light.1 = 3,  -1.62,  13.28,-0.15, fx_navgre
light.2 = 2,  -2.02, -13.28,-0.15, fx_strobe
light.3 = 2,  -2.02,  13.28,-0.15, fx_strobe
light.4 = 4,  -6.62,   0.00, 1.50, fx_vclight

[EFFECTS]
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1

[fuel]
LeftMain  = 0.000, -2.200, 0.000, 28.000, 0.500
RightMain = 0.000, 2.200, 0.000, 28.000, 0.500
fuel_type =1
number_of_tank_selectors =1                    
electric_pump=1

[airplane_geometry]
wing_area               =120.00000
wing_span               =25.70000
wing_root_chord         =6.50000
wing_dihedral           =0.00000
wing_incidence          =0.00000
wing_twist              =0.00000
oswald_efficiency_factor=0.80000
wing_winglets_flag      =0
wing_sweep              =0.00000
wing_pos_apex_lon       =0.93704
wing_pos_apex_vert      =0.00000
htail_area              =8.70000
htail_span              =9.00000
htail_pos_lon           =-12.40000
htail_pos_vert          =0.00000
htail_incidence         =0.00000
htail_sweep             =0.00000
vtail_area              =3.30000
vtail_span              =2.00000
vtail_sweep             =0.00000
vtail_pos_lon           =-12.40000
vtail_pos_vert          =0.00000
elevator_area           =13.20000
aileron_area            =19.00000
rudder_area             =10.00000
elevator_up_limit       =26.00000
elevator_down_limit     =26.00000
aileron_up_limit        =30.00000
aileron_down_limit      =30.00000
rudder_limit            =30.00000
elevator_trim_limit     =15.00000
spoiler_limit           =0.00000
spoilerons_available    =0
aileron_to_spoileron_gain =0.00000
min_ailerons_for_spoilerons =0.00000
min_flaps_for_spoilerons =0.00000
auto_spoiler_available=0
spoiler_extension_time=0.000000
positive_g_limit_flaps_up=12.00000
positive_g_limit_flaps_down=8.40000
negative_g_limit_flaps_up=-9.60000
negative_g_limit_flaps_down=-7.20000
load_safety_factor=1.00000


[Reference Speeds]
flaps_up_stall_speed    =56.99998
full_flaps_stall_speed  =56.99998
cruise_speed            =195.00000
max_indicated_speed=209.00000
max_mach=1.00000

[autopilot]
autopilot_available=0
flight_director_available=0
autothrottle_available=0
autothrottle_arming_required=0
default_pitch_mode=0
default_bank_mode=0
use_no_default_bank=1
use_no_default_pitch=1
default_vertical_speed=1000.00000
autothrottle_takeoff_ga=1.00000
autothrottle_max_rpm=90.00000
pitch_takeoff_ga=8.00000
max_pitch=10.00000
max_pitch_acceleration=1.00000
max_pitch_velocity_lo_alt=2.00000
max_pitch_velocity_hi_alt=1.50000
max_pitch_velocity_lo_alt_breakpoint=20000.00000
max_pitch_velocity_hi_alt_breakpoint=28000.00000
max_bank=25.00000
max_bank_acceleration=1.80000
max_bank_velocity=3.00000
max_throttle_rate=0.10000
nav_proportional_control=9.00000
nav_integrator_control=0.25000
nav_derivative_control=0.00000
nav_integrator_boundary=2.50000
nav_derivative_boundary=0.00000
gs_proportional_control=9.52000
gs_integrator_control=0.26000
gs_derivative_control=0.00000
gs_integrator_boundary=0.70000
gs_derivative_boundary=0.00000
yaw_damper_gain=0.00000

[forcefeedback]
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

[brakes]
toe_brakes_scale=0.79348
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.00000
flap_limit_idle=0.00000
flap_limit_power=0.00000
[hydraulic_system]
normal_pressure=0.00000
[AirWrench]
Aircraft_Length=22.70000
Vmax_sl=241.66359
Vmax_ca=265.71487
V_rc=132.33959
Climb_Rate=3543.00000
Climb_Weight=2162.00000
Max_gforce=12.00000
Emergency_hp=400.00000
WingConfig=0
Wing_Vert_Pos=0.00000
ActualSweep=5.00000
Aircraft_Type=3
FlowCorrection=1.00000
Power_Correction=1.56863
JetAltitude=0.00000
turboprop_critical_altitude=0.00000
target_roll_Vopt=310.71033
target_roll_rate=279.70000
pitch_damping=1.00000
yaw_damping=1.00000
elevator_scalar=1.00000
rudder_scalar=1.00000
Elevator_FF=60.00000
Aileron_FF=-60.00000
Control_Response=40.00000
V_Max_Control=281.94086
V_Zero_Control=563.88171
Spin_Stability=100.00000
Stall_Stability=100.00000
Elevator_Propwash=1.00000
Rudder_Propwash=1.00000
spoiler_time=0.00000
spoiler_cd=0.00000
spoiler_cl=0.00000
spoiler_cm=0.00000
flaps_cd_scalar=0.00000
flaps_cm_scalar=0.00000
gear_cd_scalar=0.00000
gear_cm_scalar=0.00000
cylinder_head_temperature=501.00000
exhaust_gas_temperature=1201.00000
fuel_pressure=30.00000
oil_pressure=60.00000
oil_temperature=241.00000
radiator_temperature=211.00000
exhaust_pressure_ratio=0.00000
interstage_turbine_temperature=-459.00000
knots_flag=1
cfs1_flag=0
tab_edit=0
AirWrenchVersion=1.01.35
nose_position_lon=7.94000
ActualIncidence=0.00000
ActualTwist=0.00000
ActualTailIncidence=0.00000
dihedral_scalar=1.00000
Roll_Response=30.00000
Adverse_Yaw=100.00000
afterburner_thrust=0.00000
mach_scale=1.00000
spoiler_type=0
flaps_type=0
vfe_enabled=0
cfs2_ai_flag=0
fs8_flag=1
laminar_flow=0
direct_edit_mach=0
fixed_wing_pos=0
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=0.150000
[stall_warning]
type=1
stick_shaker=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[deice_system]
structural_deice_type=0
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 0.100
system_type= 4
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000