[fltsim.0]
title=J1N
sim=J1N
model=
panel=
sound=
texture=
kb_checklists=
atc_id=J1N
atc_flight_number=
ui_manufacturer="Nakajima"
ui_type="J1N1"
ui_variation="S"
ui_typerole="Twin Engine Prop"
ui_createdby="haditahir"
description="Penempur Malam Nakajima Tipe 11 (J1N1-S) 202 Kokutai, Manggar Balikpapan"
[general]
atc_type=Nakajima
atc_model=Gekko
performance="Höchstgeschwindigkeit\t 507 km/h\n
Reichweite\t3.778 km\n
Antrieb\t2× Nakajima Sakae, je 843 kW (1.130 PS)\n
Dienstgipfelhöhe\t9.320 m\n
Leergewicht\t4.840 kg\n
Fluggewicht\t7.010 kg\n
Max. Fluggewicht\t8.184 kg\n
Steigrate\t522 m/min"
category = airplane
[CameraDefinition.0]
Title = "Ekor"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = 0, 5, -30.0
InitialPbh = 10, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.1]
Title = "Kanan"
Guid = {04AE8F1C-D397-487a-A5D7-DDB983AFBE2F}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 15.8, 1.3, 0.0
InitialPbh = 8, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum
[CameraDefinition.2]
Title = "Kiri"
Guid = {2A5E64FD-F106-4d29-83E8-14647BDD7DF8}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -15.8, 1.3, 0.0
InitialPbh = 8, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum
[CameraDefinition.3]
Title = "Belakang"
Guid = {5413EC9E-1908-42da-9791-EDA891D80AF0}
Description = Pilot
Origin = Virtual Cockpit
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 0.0, 0, -1.25
InitialPbh = 0, 0, 0
XyzAdjust = TRUE
Category=Cockpit
MomentumEffect=TRUE
ClipMode=Minimum
[WEIGHT_AND_BALANCE]
max_gross_weight = 18005 // (pounds)
empty_weight = 10648 // (pounds)
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations =50
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.0= 145.0, 11.0524, 0.0,1.6236
station_load.1= 145.0, 7.0242, 0.0,1.6662
station_name.0= "Pilot"
station_name.1= "Kawan sang Pilot"
;Moments of Inertia
empty_weight_pitch_MOI=13200
empty_weight_roll_MOI=29160
empty_weight_yaw_MOI=40630
empty_weight_coupled_MOI=0.0
[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
p_factor_on_yaw = 0.5
torque_on_roll = 1.0
gyro_precession_on_yaw = 1.0
gyro_precession_on_pitch = 1.0
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 7 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 5 // degrees
flaps-position.2 = 10 // degrees
flaps-position.3 = 15 // degrees
flaps-position.4 = 20 // degrees
flaps-position.5 = 25.0 // degrees
flaps-position.6 = 30.0 // degrees
damaging-speed = 140 // KIAS
blowout-speed = 175 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 7.4087, -6.5997, 1.0967 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 7.4087, 6.5997, 1.0967 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0 //Fuel flow scalar
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
master_ignition_switch = 1 //Master Ignition Switch
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 121.64 //Cubic inches per cylinder
compression_ratio= 7.0 //Compression ratio
number_of_cylinders=14 //Number of cylinders
max_rated_rpm= 2750 //Max rated RPM
max_rated_hp= 1130 //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= 1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 46 //Max design manifold pressure, (inHg)
min_design_mp= 14 //Min design manifold pressure, (inHg)
critical_altitude= 7000 //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= 1.0 //Scalar on idle RPM friction
magneto_order_left_right_both = 1 //sets the order of the magneto switch direction
[propeller]
thrust_scalar = 1.0 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 10.78 //Propeller Diameter, (feet)
propeller_blades= 3 //Number of propeller blades
propeller_moi= 78.0 //Propeller moment of inertia
beta_max= 65 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 17 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1400 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 2.38 //Propeller gear reduction ratio
fixed_pitch_beta= 0 //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= 0.0 //Coefficient of friction for power absorbed by propeller
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)
//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,-15.8856, 0.0000, -3.5518, 1200.0, 0, 0.645, 60.0, 0.700, 2.5, 0.30, 2.0, 2.0, 0.0, 0.0, 0.0
point.1=1, 11.4502, -7.0554, -8.2362, 1600.0, 1, 1.480, 0.0, 0.628, 2.5, 0.80, 7.0, 8.0, 2.0, 184.0, 184.0
point.2=1, 11.4502, 7.0554, -8.2362, 1600.0, 2, 1.480, 0.0, 0.628, 2.5, 0.80, 6.0, 9.0, 3.0, 184.0, 184.0
point.3=2, 9.3591, -28.4647, 2.1717, 800.0, 0, 0.000, 0.0, 0.000, 0.0, 0.00, 0.0, 0.0, 5.0, 0.0, 0.0 //LWingtip
point.4=2, 9.3591, 28.4647, 2.1717, 800.0, 0, 0.000, 0.0, 0.000, 0.0, 0.00, 0.0, 0.0, 6.0, 0.0, 0.0 //RWingtip
point.5=2,-18.4596, 0.0000, 7.8447, 800.0, 0, 0.000, 0.0, 0.000, 0.0, 0.00, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2,-20.0245, 0.0000, 1.7822, 1574, 0, 0.000, 0.00, 0, 0, 0.00, 0, 0.0, 4.0, 0, 0 //-- Tail
point.7=2, 20.5031, 0.0000, 0.7431, 800.0, 0, 0.000, 0.0, 0.000, 0.0, 0.00, 0.0, 0.0, 4.0, 0.0, 0.0 //--Nose
static_pitch = 13.43
static_cg_height = 5
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 0.0 //Flap angle that activates warning at idle
flap_limit_power = 16.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.7 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
auto_brakes = 0
[hydraulic_system]
normal_pressure = 732.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint = 11.0368, 0.0, 3.534
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//light.0 = 3, 7.3749, -23.6485, 1.7556, fx_navredm ,
//light.1 = 3, 7.3749, 23.6485, 1.7556, fx_navgrem ,
light.2 = 3, 7.0308, -13.8154, 0.0014, fx_navwhi ,
light.3 = 3, 7.0308, 13.8154, 0.0014, fx_navwhi ,
light.4 = 4, 12.7211, 0.0000, 2.7339, fx_vclight,
light.5 = 4, 7.75000, 0.0000, 2.7339, fx_vclight,
//light.6 = 3, 7.3749, -13.7076, 1.0719, fx_navredm ,
//light.7 = 3, 7.3749, 13.7076, 1.0719, fx_navgrem ,
//light.8 = 3, 7.7742, -23.7557, 1.2556, fx_navred ,
//light.9 = 3, 7.7742, 23.7557, 1.2556, fx_navgre ,
light.10 =3, 10.4909, -27.6724, 2.051, fx_navred ,
light.11 =1, 10.4909, -27.6724, 2.051, fx_beacon ,
light.12 = 3,10.4909, 27.6724, 2.051, fx_navgre ,
light.13 = 1,10.4909, 27.6724, 2.051, fx_beacon ,
light.14 = 1,13.2164, -6.6683, -3.7802, fx_navwhi ,
light.15 = 1,13.2164, 6.6683, -3.7802, fx_navwhi ,
[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
Adf.2 = 1
Transponder.1 = 0
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 =200, 1000
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
direction_indicator.1=2,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
attitude_indicator.1 = 2
[altimeters]
altimeter.0=1
altimeter.1=1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=2,0
[vacuum_system]
max_pressure=5.0 //PSI
vacuum_type=2 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
engine_map=1,1
[pneumatic_system]
max_pressure=18.000000
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 1.0 //Scalar on heat effectiveness, 0 = not available
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt_jenny
touchdown=fx_tchdwn_s, 1
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 30
max_generator_alternator_amps = 400
[fuel]
//tanki: internal 2460 liter eksternal 330 liter x 2. 1 US gallon = 3.78541178 liter
LeftMain = -5.9055, -6.5617, -0.164, 216, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain= -5.9055, 6.5617, -0.164, 216, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1 = -5.9055, 0.0000, -1.2139, 216, 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 = 2
electric_pump=1
[airplane_geometry]
wing_area = 430 //Square feet
wing_span = 55.67 //Feet
wing_root_chord = 26.63 //Feet
wing_dihedral = 20.0 //Degrees
wing_incidence = 2.0 //Degrees
wing_twist = -1.0 //Degrees
oswald_efficiency_factor= 0.90 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 6.00 //Degrees, wing leading edge
wing_pos_apex_lon = 12.225 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 6.394 //Feet, vertical distance from reference point, positive going up
htail_area = 80.0 //Square feet
htail_span = 20.25 //Feet
htail_pos_lon = -17.33 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = -1.7475 //Feet, vertical distance from reference point, positive going up
htail_incidence = -1.0 //Degrees
htail_sweep = 43 //Degrees, horizontal tail leading edge
vtail_area = 29.7 //Square feet
vtail_span = 8.3 //Feet, tip to body
vtail_sweep = 31 //Degrees, vertical tail leading edge
vtail_pos_lon = -13.49 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 7.7 //Feet, vertical distance from reference point, positive going up
elevator_area = 81 //Square feet
aileron_area = 41.6 //Square feet
rudder_area = 26.3 //Square feet
elevator_up_limit = 30.0 //Degrees
elevator_down_limit = 20.0 //Degrees
aileron_up_limit = 27.0 //Degrees
aileron_down_limit = 18.0 //Degrees
rudder_limit = 30.0 //Degrees
elevator_trim_limit = 12.0 //Degrees
spoiler_limit = 0.0 //Degrees
spoilerons_available = 0 //Spoilerons Available?
aileron_to_spoileron_gain = 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available = 0
positive_g_limit_flaps_up = 4.0 //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down= 2.0 //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up = -1.5 //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down= -1.5 //Design G load tolerance (negative, flaps down)
load_safety_factor = 1.5 //Design G load safety factor
[Reference Speeds]
flaps_up_stall_speed = 67.5 //Knots True (KTAS)
full_flaps_stall_speed = 61.5 //Knots True (KTAS)
cruise_speed = 95.0 //Knots True (KTAS)
max_indicated_speed = 224 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 0
pitch_takeoff_ga=0.0
default_vertical_speed=700.000000
autothrottle_available=0
direction_indicator=1
attitude_indicator =1
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 = 0.0
default_bank_mode=2 //Default to Heading Hold
[forcefeedback]
ground_bumps_magnitude1=2600 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
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=3500000 ; in microseconds
[stall_warning]
type=1
stick_shaker=0
[exits]
//openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
number_of_exits = 3
exit.0 = 0.4, 10.9782, -0.4023, 3.8447, 0
exit.1 = 0.4, 7.2827, -0.1985, 3.9588, 0
exit.2 = 0.4, -3.0626, -0.3302, 2.7928, 1
[deice_system]
structural_deice_type=0 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots