[fltsim.0]
title=USSR_V-4
sim=USSR_V-4
model=
panel=
sound=
texture=
kb_checklists=
atc_id=
atc_airline=USSR
atc_flight_number=005
atc_heavy=1
ui_manufacturer=AI Dirizablestroy
ui_type=USSR_V-4
ui_variation=USSR_V-4
prop_anim_ratio=0.45
[General]
atc_type=V4
atc_model=V4
editable=1
performance=\n
[weight_and_balance]
// ACM V2.3
max_gross_weight = 935
empty_weight = 1
reference_datum_position = 3.6, 0, 0
empty_weight_CG_position = -4, 0, 0
empty_weight_pitch_MOI = 2672
empty_weight_roll_MOI = 1037
empty_weight_yaw_MOI = 1760
empty_weight_coupled_MOI = 0
max_number_of_stations = 3
station_load.0 = 170, -3.0, -1.5, 0.0
station_load.1 = 170, 0.0, 1.5, 0.0
station_load.2 = 0, -8.0, 0.0, 0.0
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4, -4.8, 0, 4.6, fx_vclitecub.fx
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 0.350000
engine.0 = 1.4, 0, 8.7,
//engine.1 = 1.4, -8, 8.7,
min_throttle_limit=0.000000
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_dustrun
concrete = fx_sparksx
touchdown = fx_tchdwn_s, 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 1
Center1 = 3, 0, 0, 12, 0
electric_pump=1
[contact_points]
static_pitch = 0
static_cg_height = 2.917387
max_number_of_points = 3
point.0 = 1, 17.416667, 0, -1.533333, 2377.95, 0, 0.512, 43, 0.7, 1.5, 0.7, 0, 0, 0, 0, 0
point.1 = 1, -24.816667, -10.75, -1.633333, 2468.5, 1, 0.512, 0, 0.7, 1.5, 0.7, 0, 0, 2, 0, 0
point.2 = 1, -24.816667, 10.75, -1.63333, 2468.5, 2, 0.512, 0, 0.7, 1.5, 0.7, 0, 0, 3, 0, 0
static_pitch=0.000000
static_cg_height=2.917387
[keyboard_response]
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 3000
[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
[airplane_geometry]
//ACM_AREAW1// 0,0,0,1.4986,0.6110,0.6110,0,1.4235,1.2220,1.2220
//ACM_AREAW2// 0,1.3487,1.8329,1.8329,0,1.2738,2.4440,2.4440,0,1.1987
//ACM_AREAW3// 3.0550,3.0550,0,1.1239,3.6659,3.6659,0,1.0490,4.2769,4.2769
//ACM_AREAW4// 0,0.9739,4.8880,4.8880,0,0.8991,5.4990,5.4990,0,0.8241
//ACM_AREAH1// 0,0,0,1.1852,0.1975,0.1975,0,1.1260,0.3950,0.3950
//ACM_AREAH2// 0,1.0666,0.5925,0.5925,0,1.0075,0.7901,0.7901,0,0.9481
//ACM_AREAH3// 0.9876,0.9876,0,0.8888,1.1852,1.1852,0,0.8296,1.3827,1.3827
//ACM_AREAH4// 0,0.7703,1.5803,1.5803,0,0.7110,1.7778,1.7778,0,0.6518
//ACM_AREAV1// 0,0,0,1.4744,0.1638,0.1638,0,1.3564,0.3276,0.3276
//ACM_AREAV2// 0,1.2384,0.4914,0.4914,0,1.1204,0.6553,0.6553,0,1.0025
//ACM_AREAV3// 0.8191,0.8191,0,0.8845,0.9829,0.9829,0,0.7667,1.1467,1.1467
//ACM_AREAV4// 0,0.6486,1.3106,1.3106,0,0.5307,1.4744,1.4744,0,0.4128
//ACM_CAREAW1// 2.7495,2.7495,0.7493,1.0490,3.0550,3.0550,0.7493,1.0340,3.3605,3.3605
//ACM_CAREAW2// 0.7493,1.0190,3.6659,3.6659,0.7493,1.0039,3.9714,3.9714,0.7493,0.9890
//ACM_CAREAW3// 4.2769,4.2769,0.7493,0.9739,4.5824,4.5824,0.7493,0.9591,4.8880,4.8880
//ACM_CAREAW4// 0.7493,0.9441,5.1935,5.1935,0.7493,0.9290,5.4990,5.4990,0.7493,0.9140
//ACM_CAREAH1// 0,0,0.5925,1.1852,0.1975,0.1975,0.5925,1.1555,0.3950,0.3950
//ACM_CAREAH2// 0.5925,1.1260,0.5925,0.5925,0.5925,1.0964,0.7901,0.7901,0.5925,1.0666
//ACM_CAREAH3// 0.9876,0.9876,0.5925,1.0370,1.1852,1.1852,0.5925,1.0075,1.3827,1.3827
//ACM_CAREAH4// 0.5925,0.9779,1.5803,1.5803,0.5925,0.9481,1.7778,1.7778,0.5925,0.9186
//ACM_CAREAV1// 0,0,0.3686,1.1058,0.1638,0.1638,0.3686,1.0468,0.3276,0.3276
//ACM_CAREAV2// 0.3686,0.9878,0.4914,0.4914,0.3686,0.9287,0.6553,0.6553,0.3686,0.8698
//ACM_CAREAV3// 0.8191,0.8191,0.3686,0.8108,0.9829,0.9829,0.3686,0.7519,1.1467,1.1467
//ACM_CAREAV4// 0.3686,0.6929,1.3106,1.3106,0.3686,0.6340,1.4744,1.4744,0.3686,0.5749
wing_area = 384.000000
wing_span = 36.083333
wing_root_chord = 4.916670
wing_dihedral = 30.0
wing_incidence = 1.0
wing_twist = 1.0
oswald_efficiency_factor = 0.9
wing_winglets_flag = 0
wing_sweep = 0.000000
wing_pos_apex_lon = -2.371000
wing_pos_apex_vert = 0.000000
htail_area = 39.000000
htail_span = 11.666667
htail_pos_lon = -18.266667
htail_pos_vert = 0.000000
htail_incidence = 3.246460
htail_sweep = 0.000000
vtail_area = 15.8
vtail_span = 4.837355
vtail_sweep = 0.000000
vtail_pos_lon = -12.183333
vtail_pos_vert = -16.00000
elevator_area = 16.610000
aileron_area = 18.300000
rudder_area = 23.20000
elevator_up_limit = 28.000447
elevator_down_limit = 20.998903
aileron_up_limit = 19.996227
aileron_down_limit = 15.000035
rudder_limit = 33.995472
elevator_trim_limit = 19.497754
spoiler_limit = 45.000000
aileron_to_spoileron_gain = 0.000000
min_ailerons_for_spoilerons = 0.000000
min_flaps_for_spoilerons = 0.000000
spoilerons_available = 0
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 0
avionics_bus = 0, 1, 3
avionics = 1, 1, 3
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 1, 2
light_panel = 0, 1, 2
[flight_tuning]
cruise_lift_scalar=1.1
parasite_drag_scalar=3.35
induced_drag_scalar=1.0
elevator_effectiveness=1.4
aileron_effectiveness=1.4
rudder_effectiveness=1.4
pitch_stability=1.3
roll_stability=1.1
yaw_stability=2.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[piston_engine]
power_scalar=1.0 //Piston power scalar
cylinder_displacement=44.0 //Cubic inches per cylinder
compression_ratio=7.5 //Compression ratio
number_of_cylinders=4 //Number of cylinders
max_rated_rpm=2300 //Max rated RPM
max_rated_hp=65 //Max rated HP
fuel_metering_type=1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3 //Starter torque factor
turbocharged=0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=0 //Max design manifold pressure, (inHg)
min_design_mp=0 //Min design manifold pressure, (inHg)
critical_altitude=0 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset=0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar=0.2 //Scalar on idle RPM friction
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=1 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=6 //Propeller Diameter, (feet)
propeller_blades=2 //Number of propeller blades
propeller_moi=0.80 //Propeller moment of inertia
beta_max=0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=0 //Miminum governed RPM
prop_tc=0.1 //Prop time-constant
gear_reduction_ratio=1.0 //Propeller gear reduction ratio
fixed_pitch_beta=13.75 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=0 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=0 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=0 //Minimum RPM for prop feathering
beta_feather=0 //Feathering pitch angle (degrees)
power_absorbed_cf=0 //Coefficient of friction for power absorbed by propeller in feather
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0 //Minimum pitch angle in reverse, (degrees)
[Views]
eyepoint=-5.9, 0.1, 1.2 //(feet) longitudinal, lateral, vertical distance from reference datum
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=0
Com.1=1, 0
Nav.1=0, 0, 0
Adf.1=0
Transponder.1=1
Marker.1=0
[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
[Reference Speeds]
flaps_up_stall_speed=10.0
full_flaps_stall_speed=7.0
cruise_speed=45.0
max_indicated_speed=110.0
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
autoland_available=0
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
[brakes]
parking_brake = 0 //Parking brake available
toe_brakes_scale = 0.35 //Brake scalar
differential_braking_scale = 9.0 //Delta on the amount of brake when the rudder pedals deflected
[flaps.0] //Trailing Edge Flaps
type=1 // 1 - tail, 2 - lead
span-outboard=0.5 // 0.0 .. 1.0
extending-time=1 // seconds
flaps-position.0=60 // degrees
flaps-position.1=32.7 // degrees
// degrees
// degrees
damaging-speed=120 // KIAS
blowout-speed=150 // KIAS
lift_scalar=1.0
drag_scalar=1.0
pitch_scalar=1.0
system_type=0
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000