[fltsim.0]
title=Mig 15 Show
sim=Mig15
model=
panel=
sound=
texture=USSR
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Mikhoyan-Gurevitch
ui_type=MiG-15
ui_variation=Mig-USSR
Description= Designed by: Mikoyan & Gurevich Design Bureau
Built By: Russian State Industries & China under license Total Built: Approximately 12,000; 227 were built in Poland from Jan 1953 to Sept 1954 as the Lim.1, another 815 were built in Czechoslovakia as the S.102 during the same time period.
//----------------------------------------
[fltsim.1]
title=MIG-15 USSR-Camo
sim=MIG15
model=
panel=
sound=
texture=USSR-Camo
kb_checklists=
kb_reference=
ui_manufacturer=Mikhoyan-Gurevitch
ui_type=MiG-15
ui_variation=USSR Air Force
description=Designed by: Mikoyan & Gurevich Design Bureau
visual_damage=1
atc_id=935
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
//--------------------------------------
[General]
atc_type=
atc_model=
performance= Power Plant: Klimov VK-1 (RD-45F) centrifugal flow turbojet. *Note: The engine was reverse-engineered from a British Rolls Royce Nene of 5,000 lb thrust.,& then developed further than the Nene. Thrust: 6,000 lbs Speed: 652 mph at Sea Level, 641mph at 16,405' Climb: 16,405' in 2.5 minutes Ceiling: 51,000' Range: 730 miles Wing Span: 33' 1" Length: 36' 4"" Height: Wing Area: Empty Wt: 7,767 lbs Gross Wt: 10,941 lbs Armament: (1) 37mm Nudelman N-37 cannon, (2) 23mm Nudelman NS-23 cannon; (2) 550 lb bombs or (2) 1,1000 bombs under wings. The 23mm cannon was smaller targets or to line a target for the larger cannon. The 37mm only carried 50 rounds & thus saved for bigger targets.
Category=airplane
//----------------------------------------
[WEIGHT_AND_BALANCE]
max_gross_weight = 10069.00
empty_weight = 5907.00
reference_datum_position = 0.00, 0.00, 0.00
empty_weight_CG_position = 0.00, 0.00, 0.00
max_number_of_stations = 50
station_load.0 = 170.00, 8.50, 0.00, 0.00
station_load.1 = 170.00, 4.60, 0.00, 0.00
;Moments of Inertia
empty_weight_pitch_MOI = 25000.00
empty_weight_roll_MOI = 14500.00
empty_weight_yaw_MOI = 17000.00
empty_weight_coupled_MOI = 0.00
CG_forward_limit= 0.00
CG_aft_limit= 1.00
//-------------------------------------------
[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, 5 , 9.5
avionics = 1, 5 , 9.5
additional_system = 0, 2 , 9.5
marker_beacon = 1, 2 , 9.0
fuel_pump = 0, 5 , 9.0
//------------------------------------------
[flight_tuning]
cruise_lift_scalar =1.0
parasite_drag_scalar =1.0
induced_drag_scalar =1.0
elevator_effectiveness =1.0
aileron_effectiveness =1.0
rudder_effectiveness =1.0
pitch_stability =1.0
roll_stability =1.0
yaw_stability =1.0
elevator_trim_effectiveness =1.0
aileron_trim_effectiveness =1.0
rudder_trim_effectiveness =1.0
//------------------------------------------
[GeneralEngineData]
engine_type = 1
Engine.0 = -16.00, 0.00, 0.90
fuel_flow_scalar = 1.00
min_throttle_limit=0.00
//-------------------------------------------
[TurbineEngineData]
fuel_flow_gain = 0.002
inlet_area = 3.00
rated_N2_rpm = 11500.00
static_thrust = 3360.00
afterburner_available = 0
reverser_available = 0
//------------------------------------------
[jet_engine]
thrust_scalar =1.00
//----------------------------------------------
[Reference Speeds]
flaps_up_stall_speed = 112.00
full_flaps_stall_speed = 90.00
cruise_speed = 220.00 knots indicated at 37,000 ft.
max_mach = 0.90
max_indicated_speed = 600 //Red line (KIAS)
max_level_speed = 466 knots over the ground at 37,000 ft.
//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]
point.0 = 1, 8, 0, -4.32, 1574.803, 0, 0.8, 36.72, 0.3, 2.5, 0.95, 5, 5, 0, 0, 0
point.1 = 1, -2.30, -6.75, -3.92, 2952.756, 1, 1.0, 0.00, 0.45, 2.5, 0.78, 5, 5, 2, 0, 0
point.2 = 1, -2.30, 6.75, -3.92, 2952.756, 2, 1.0, 0.00, 0.45, 2.5, 0.78, 5, 5, 3, 0, 0
point.3 = 2, -7.882, -16.366, -0.659, 1574.8032, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -7.882, 16.366, -0.659, 1574.8032, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.7368, 0, -1.35, 1574.8032, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 12.0554, 0, -1.152, 1574.8032, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
static_pitch = 3 //2.9226
static_cg_height = 3.58
tailwheel_lock = 0
gear_system_type = 0
//--------------------------------------------
//[gear_warning_system]
//gear_warning_available = 1 //Normal
//pct_throttle_limit = 0.1 //Percent throttle that activates warning
//flap_limit_idle = 15.0 //Flap angle that activates warning at idle
//flap_limit_power = 30.0 //Flap angle that activates warning at above idle
//--------------------------------------------
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.2 //Brake scalar
//-----------------------------------------------
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
//---------------------------------------
[Views]
eyepoint = 10.0, 0.0, 3.0
//---------------------------------------
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Com.2 = 1, 0
Nav.1 = 1, 0, 1
Nav.2 = 1, 0, 0
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
//------------------------------------------
[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 = 150, 250
aileron = 150, 250
rudder = 150, 250
//----------------------------------------
[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=3,0
//--------------------------------------
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 1
//----------------------------------
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
//-------------------------------------
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
startup=fx_AB_StartupSmoke.fx //smoke puff and 5 seconds of heat at engine startup
//------------------------------------------------------
[SMOKESYSTEM]
smoke.0=-11.0, 0, -.5, fx_AB-Grey-Smoke_.fx
smoke.1=-7.5, 0, -.25, fx_AB_Smaller_Blueflame.fx
//-----------------------------------------------
[fuel]
Center1 = 0.00, 0.00, 0.00, 200.00, 0.00
LeftMain = 2.00,-5.00, 0.00, 100.00, 0.00
RightMain = 2.00, 5.00, 0.00, 100.00, 0.00
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
//---------------------------------
[airplane_geometry]
wing_area = 208.26
wing_span = 34.80
wing_root_chord = 7.10
wing_dihedral = 5.00
wing_incidence = 0.00
wing_twist = 0.00
oswald_efficiency_factor= 0.80
wing_winglets_flag = 0
wing_sweep = 10.00
wing_pos_apex_lon = 3.70
wing_pos_apex_vert = 0.00
htail_area = 26.00
htail_span = 13.40
htail_pos_lon = -12.30
htail_pos_vert = 1.80
htail_incidence = 0.00
htail_sweep = 15.00
vtail_area = 15.00
vtail_span = 5.40
vtail_sweep = 30.00
vtail_pos_lon = -9.00
vtail_pos_vert = 2.60
elevator_area = 10.00
aileron_area = 25.00
rudder_area = 8.00
elevator_up_limit = 18.00
elevator_down_limit = 18.00
aileron_up_limit = 18.00
aileron_down_limit = 18.00
rudder_limit = 18.00
elevator_trim_limit = 15.00
spoiler_limit = 30.00
spoilerons_available = 0
aileron_to_spoileron_gain = 4.60
min_ailerons_for_spoilerons = 5.00
min_flaps_for_spoilerons= 0.00
auto_spoiler_available=0
spoiler_extension_time=1.000000
positive_g_limit_flaps_up=7.500000
positive_g_limit_flaps_down=6.000000
negative_g_limit_flaps_up=-3.500000
negative_g_limit_flaps_down=-3.000000
//----------------------------------------
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 0
autothrottle_max_rpm = 100
autothrottle_takeoff_ga= 0
pitch_takeoff_ga = 8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=11.00
nav_integrator_control=0.20
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
//---------------------------------
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
gear_bump_nose_magnitude=3000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2700 ; 0 - 10000
gear_bump_left_direction=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1300 ; 0 - 10000
ground_bumps_angle1=08900 ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200 ; 0 - 10000
ground_bumps_angle2=09100 ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000 ; 0 - 10000
crash_direction1=01000 ; 0 - 35999 degrees
crash_magnitude2=10000 ; 0 - 10000
crash_direction2=9000 ; 0 - 35999 degrees
crash_period2=75000 ; in microseconds
crash_duration2=2500000 ; in microseconds
//-------------------------------------------------
[stall_warning]
type=2
stick_shaker=1
//------------------------------------------------
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -8.66, -16.4, -0.6, fx_navred
light.1 = 3, -8.66, 16.4, -0.6, fx_navgre
light.2 = 3, -3.3, 0, 2, fx_navwhi
light.5 = 4, 5.5, 0, 3.2, fx_vclight
light.4 = 9, -9.5, 0, -.75, fx_AB2_Smallest _flame.fx
//--------------------------------------------------------
[Flaps.0]
type= 1
span-outboard= 0.80
extending-time= 5.00
system_type= 0
damaging-speed= 250.00
blowout-speed= 300.00
lift_scalar= 1.00
drag_scalar= 1.00
pitch_scalar= 1.00
flaps-position.0= 0.00, 0.00
flaps-position.1= 8.00, 0.00
flaps-position.2= 20.00, 0.00
flaps-position.3= 40.00, 0.00
//--------------------------
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=33.750000
flap_limit_idle=16.875000
//----------------------------
[pitot_static]
pitot_heat=1.00
//-----------------------------
[vacuum_system]
max_pressure=5.15
vacuum_type=2
electric_backup_pressure=0.00
engine_map=0,0,0,0
//------------------------------
[pneumatic_system]
max_pressure=18.00
bleed_air_scalar=1.00
//----------------------------------
[deice_system]
structural_deice_type=0
