[fltsim.0]
title=Il-10 1947
sim=Ilyushin Il-10
model=
panel=
sound=
texture=
atc_id=11
atc_airline=VVS USSR
atc_flight_number=11
ui_manufacturer=Ilyushin
ui_type="Il-10"
ui_variation="1947"
description="To provide replacement to attack plane Il-2, in 1943 it has been developed two different skilled planes. Variant Il-8, having kept close similarity with Il-2, has been equipped by more powerful engine AM-42, had a new wing, horizontal tail plumage and the chassis united with a fuselage of plane Il-2 of late manufacture. It has passed flight tests in April, 1944, but it have refused in favour of Il-10 which was absolutely new working out of an all-metal design and the advanced aerodynamic form. The main racks of the chassis were cleaned in a wing in this connection from a wing have disappeared big as at Il-2. Positive results of tests of the skilled plane have led to release of party of pre-series cars. Mass production has been begun in August, 1944, and an estimation in operating regiments - two months later. For the first time this plane began to be used in February, 1945, and by the spring its manufacture has reached peak. Before capitulation of Germany many regiments were these attack planes; their considerable quantity took part in short, but large-scale actions against the Japanese aggressors in Manchuria and Korea within August, 1945. Manufacture proceeded and during the post-war period. At factories of Soviet Union 4966 cars have been constructed. Last plane has left an assembly line in 1955. Besides planes Il-10 were under construction at the Czech aviation factory under designation B-33 and CB-33, and last was an equivalent of an uchebno-training variant of plane Il-10U. Manufacture of these devices in Czechoslovakia has stopped in 1954 after have been constructed more than 1200 copies. Since 1955 their manufacture in Soviet Union has concentrated on plane Il-10M which differed absolutely new form of a wing in the plan with thicker profile slightly extended with a fuselage, and also in the raised capacity of fuel and the modified chassis with the increased track. Il-10 was the basic plane consisting on arms of the Soviet assault regiments till 1956; it also was widely used by the countries of the Warsaw Contract. Democratic People's Republic of Korea used them at an initial stage of the Korean war in 1950 and has had considerable losses as these planes were absolutely worn out."
[fltsim.1]
title=Il-10 1944
sim=Ilyushin Il-10
model=
panel=
sound=
texture=1
atc_id=5
atc_airline=VVS USSR
atc_flight_number=5
ui_manufacturer=Ilyushin
ui_type="Il-10"
ui_variation="1944-45"
description="To provide replacement to attack plane Il-2, in 1943 it has been developed two different skilled planes. Variant Il-8, having kept close similarity with Il-2, has been equipped by more powerful engine AM-42, had a new wing, horizontal tail plumage and the chassis united with a fuselage of plane Il-2 of late manufacture. It has passed flight tests in April, 1944, but it have refused in favour of Il-10 which was absolutely new working out of an all-metal design and the advanced aerodynamic form. The main racks of the chassis were cleaned in a wing in this connection from a wing have disappeared big as at Il-2. Positive results of tests of the skilled plane have led to release of party of pre-series cars. Mass production has been begun in August, 1944, and an estimation in operating regiments - two months later. For the first time this plane began to be used in February, 1945, and by the spring its manufacture has reached peak. Before capitulation of Germany many regiments were these attack planes; their considerable quantity took part in short, but large-scale actions against the Japanese aggressors in Manchuria and Korea within August, 1945. Manufacture proceeded and during the post-war period. At factories of Soviet Union 4966 cars have been constructed. Last plane has left an assembly line in 1955. Besides planes Il-10 were under construction at the Czech aviation factory under designation B-33 and CB-33, and last was an equivalent of an uchebno-training variant of plane Il-10U. Manufacture of these devices in Czechoslovakia has stopped in 1954 after have been constructed more than 1200 copies. Since 1955 their manufacture in Soviet Union has concentrated on plane Il-10M which differed absolutely new form of a wing in the plan with thicker profile slightly extended with a fuselage, and also in the raised capacity of fuel and the modified chassis with the increased track. Il-10 was the basic plane consisting on arms of the Soviet assault regiments till 1956; it also was widely used by the countries of the Warsaw Contract. Democratic People's Republic of Korea used them at an initial stage of the Korean war in 1950 and has had considerable losses as these planes were absolutely worn out."
[WEIGHT_AND_BALANCE]
empty_weight =10305.00000
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.050, 0.000, 0.000
max_number_of_stations =2
empty_weight_pitch_MOI =14370.00000
empty_weight_roll_MOI =12663.00000
empty_weight_yaw_MOI =24996.00000
max_gross_weight=14410.0
empty_weight_coupled_MOI=0.00000
station_load.0= 200, -1.710, 0.000, 0.000, pilot
station_load.1= 200, -4.477, 0.000, 0.000, gunner
[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
[piston_engine]
power_scalar =1.00000
cylinder_displacement =237.25000
compression_ratio =6.00000
number_of_cylinders =12
max_rated_rpm =2500.00000
max_rated_hp =2000.00000
fuel_metering_type =2
cooling_type =1
normalized_starter_torque =0.03342
turbocharged =1
max_design_mp =55.00000
min_design_mp =9.00000
critical_altitude =8070.00000
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 =1.00000
emergency_boost_duration=0.00000
[propeller]
thrust_scalar =1.00000
propeller_type =0
propeller_diameter =10.50000
propeller_blades =3
propeller_moi =36.11158
beta_max =65.00000
beta_min =15.00000
min_gov_rpm =405.00000
prop_tc =0.01000
gear_reduction_ratio =2.38000
fixed_pitch_beta =30.00000
low_speed_theory_limit =80.00000
prop_sync_available =0
prop_deice_available =1
prop_feathering_available =0
prop_auto_feathering_available =0
min_rpm_for_feather =700.00000
beta_feather =88.50000
power_absorbed_cf =0.90000
defeathering_accumulators_available =0
prop_reverse_available =0
minimum_on_ground_beta =1.00000
minimum_reverse_beta =-14.00000
rotation = 1
[folding_wings]
wing_fold_system_type = 4
fold_rates = 0.12, 0.11
[TailHook]
tailhook_length = 4
tailhook_position = -15, 0, -1
cable_force_adjust = 1
[contact_points]
max_number_of_points =7
static_pitch= 12.365
static_cg_height= 6.522
gear_system_type=1
tailwheel_lock=0
point.0= 1, -18.083, 0.000, -3.100, 2575, 0, 0.562, 43.000, 0.143, 2.497, 1.220, 3.000, 3.000, 0
point.1= 1, 0.867, -3.917, -7.333, 3165, 1, 0.562, 0.000, 0.635, 2.499, 0.709, 7.500, 7.500, 2
point.2= 1, 0.867, 3.917, -7.333, 3165, 2, 0.562, 0.000, 0.635, 2.499, 0.709, 6.000, 6.000, 3
point.3= 2, -0.500, -24.104, -1.583, 1181, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.4= 2, -0.500, 24.104, -1.583, 1181, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
point.5= 2, -26.675, -0.083, -1.083, 1181, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.6= 2, 12.748, 0.083, -1.083, 1181, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
[Views]
eyepoint= -1.478155, 0, 2.969157
[flaps.0] //Trailing Edge Flaps
type = 1
span-outboard = 0.5
extending-time = 5
flaps-position.0 = 0
flaps-position.1 = 1, 136
flaps-position.2 = 11, 136
flaps-position.3 = 22, 130
flaps-position.4 = 33, 124
flaps-position.5 = 45, 119
damaging-speed = 136
blowout-speed = 147
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 160
electric_always_available = 1
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
starter2 = 0, 20, 17
starter3 = 0, 20, 17
starter4 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
prop_sync = 0, 15, 17
auto_feather = 0, 15, 17
auto_brakes = 0, 15, 17
standby_vacuum = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
[LIGHTS]
panel = 0, 0.2, 0.0, fx_vclight
[LSO]
LSOAdjustSpeed = 1.2
[exits]
number_of_exits = 2
exit_rate.0 = 0.4
exit_rate.1 = 0.6
[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 =500
gear_bump_right_duration =250000
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
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111
[General]
performance=ENGINE: Mikulin AM-42 2000hp MAX SPEED: 310mph @ Sea Level CEILING: 13510ft RANGE: 497mi WEIGHT: 10305lb (MTO 14410) DMENSIONS: Span 44ft 0in, Length 36ft 6in ARMAMENT: Two VYa-23 23mm cannon, two ShKAS 7.62mm machine guns, one UBT 12.7mm machine gun/Late Model: Four NS-23 23mm cannon, one B-20T 20mm cannon
editable=1
[GeneralEngineData]
Engine.0=6.800, 0.000, 0.500
engine_type=0
fuel_flow_scalar=1.00000
min_throttle_limit=0.000000
[fuel]
Center1= -3.500, 0.000, 0.500, 190.000, 0.000
fuel_type=1
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=414.00000
wing_span=47.92000
wing_root_chord=8.63940
wing_dihedral=3.00000
wing_incidence=0.00000
wing_twist=0.00000
oswald_efficiency_factor=0.88000
wing_winglets_flag=0
wing_sweep=0.00000
wing_pos_apex_lon=2.15974
wing_pos_apex_vert=0.00000
htail_area=52.00000
htail_span=18.17000
htail_pos_lon=-22.67000
htail_pos_vert=0.00000
htail_incidence=0.00000
htail_sweep=0.00000
vtail_area=31.00000
vtail_span=8.50000
vtail_pos_lon=-23.17000
vtail_pos_vert=0.00000
vtail_sweep=0.00000
elevator_area=28.60000
aileron_area=29.90000
rudder_area=19.50000
elevator_up_limit=22.00000
elevator_down_limit=20.00000
aileron_up_limit=15.00000
aileron_down_limit=15.00000
rudder_limit=30.00000
elevator_trim_limit=18.00000
spoiler_limit=90.00000
spoilerons_available=0
aileron_to_spoileron_gain=0.00000
min_ailerons_for_spoilerons=0.00000
min_flaps_for_spoilerons=0.00000
[brakes]
toe_brakes_scale=0.64089
[smokesystem]
smoke.0=0
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.00000
flap_limit_idle=33.75000
flap_limit_power=16.87500
[Reference Speeds]
flaps_up_stall_speed=82.55274
full_flaps_stall_speed=61.69731
cruise_speed=210.11845
max_indicated_speed=496.00000
max_mach=1.00000
[autopilot]
autopilot_available=1
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
[hydraulic_system]
normal_pressure=998.00000
engine_map=1,0,0,0
[AirWrench]
Aircraft_Length= 40.730
Vmax_sl=310.00000
Vmax_ca=340.00000
V_rc=110.90000
Climb_Rate=2931.60000
Climb_Weight=11576.00000
Max_gforce=7.50000
Emergency_hp=2000.00000
nose_position_lon= 14.260
ActualIncidence=0.00000
ActualTwist=0.00000
ActualTailIncidence=0.00000
Aircraft_Type=2
FlowCorrection=1.00000
Power_Correction=0.96045
JetAltitude=0.00000
turboprop_critical_altitude=0.00000
target_roll_Vopt=290.90000
target_roll_rate=53.30000
pitch_damping=1.00000
yaw_damping=1.00000
elevator_scalar=1.00000
rudder_scalar=1.00000
dihedral_scalar=1.00000
Elevator_FF=21.89100
Aileron_FF=-20.93900
Roll_Response=30.00000
Adverse_Yaw=100.00000
Control_Response=100.00000
V_Max_Control=455.70848
V_Zero_Control=911.41697
Spin_Stability=100.00000
Stall_Stability=100.00000
Elevator_Propwash=1.00000
Rudder_Propwash=1.00000
spoiler_time=2.00000
afterburner_thrust=0.00000
mach_scale=1.00000
spoiler_type=1
spoiler_cd=0.00490
spoiler_cl=0.00000
spoiler_cm=0.00000
flaps_type=1
flaps_cd_scalar=1.13169
flaps_cm_scalar=0.00000
vfe_enabled=0
gear_cd_scalar=0.25000
gear_cm_scalar=0.00000
cylinder_head_temperature=501.00000
exhaust_gas_temperature=1201.00000
fuel_pressure=20.00000
oil_pressure=60.00000
oil_temperature=241.00000
radiator_temperature=211.00000
exhaust_pressure_ratio=0.00000
interstage_turbine_temperature=-459.00000
knots_flag=0
cfs1_flag=0
laminar_flow=0
fixed_wing_pos=0
AirWrenchVersion=1.01.31
[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[direction_indicators]
direction_indicator.0=1,0