Albatros_DIII.zip > Albatros DIII > Aircraft.cfg.txt
 
Back to zip content
[fltsim.0]
title=Albatross_DVa Jasta 37 Ernst Udet
sim=Albatross_DVa
model=
panel=
sound=
texture=1
checklists=
ui_manufacturer=Albatros
description=Country: Germany \nManufacturer: Albatros Werke GmbH \nType: Fighter \nFirst Introduced: January 1917 \nNumber Built: 1,350





[contact_points]
	//0  Class
	//1  Longitudinal Position    z    (feet)
	//2  Lateral Position          x   (feet)
	//3  Vertical Position         y   (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
	//14 Airspeed limit for retraction (KIAS)
	//15 Airspeed that gear gets damage at (KIAS)
point.0= 1.000, -13.75, 0.000, -0.950, 1181.102, 0.000, 0.512, 0.000, 0.187, 2.500, 3.275, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, 2.50, -3.083, -4.42, 1574.803, 0.000, 0.530, 0.000, 0.20, 2.5, 0.83, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000, 2.50, 3.083, -4.42, 1574.803, 0.000, 0.530, 0.000, 0.20, 2.5, 0.83, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, 1.95, -15.00, -1.20, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, 1.95, 15.00, -1.20, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -16.50, 0.000, 1.90, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 9.50, 0.000, 3.00, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 11.997
static_cg_height= 5.00

[brakes]
parking_brake = 1       //Parking brake available
//toe_brakes_scale = 0.5  //Brake scalar
//differential_braking_scale = 1.0        //Delta on the amount of brake when the rudder pedals deflected
//auto_brakes = 0

[Views]
eyepoint=-2.10, 0.0,3.85    //-3.237156,0.000000,2.593840  

[General]
performance=Maximum Speed\t109 kts at 3281ft\nMaximum Range\t? mi\nService Ceiling\t18,044 ft\nGross Weight\t1,949 lb\nCrew\t1\n\nEngine: Mercedes DIIIa liquid cooled 6 cylinder inline 200hp.
Category=airplane

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
empty_weight=1470.00
empty_weight_roll_MOI=1486.000000
empty_weight_pitch_MOI=2530.000000
empty_weight_yaw_MOI=3782.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=2066.00
station_load.0=170,  -1.00, 0.0, 1.0		//Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

[fuel]
Center1=1.0,0,-1.7,60.00,5.00 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0


[airplane_geometry]
wing_area=220.000000
wing_span=29.666667
wing_root_chord=6.916667
wing_dihedral=6.300659
wing_incidence=0.999756
wing_twist=0.000000
oswald_efficiency_factor=1.056428
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=24.000000
htail_span=11.000000
htail_pos_lon=-18.833333
htail_pos_vert=0.000000
htail_incidence=-0.999756
htail_sweep=0.000000
vtail_area=15.000000
vtail_span=4.415880
vtail_sweep=0.000000
vtail_pos_lon=-18.833333
vtail_pos_vert=0.583333
elevator_area=13.000000
aileron_area=20.400000
rudder_area=13.060000
elevator_up_limit=26.000825
elevator_down_limit=26.000825
aileron_up_limit=21.497376
aileron_down_limit=20.345731
rudder_limit=28.997394
elevator_trim_limit=19.996227
spoiler_limit=0.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
auto_spoiler_available=0
positive_g_limit_flaps_up=10.000000
positive_g_limit_flaps_down=10.000000
negative_g_limit_flaps_up=-10.000000
negative_g_limit_flaps_down=-10.000000

[Flaps.0]
type=0

[GeneralEngineData]
engine_type=0
Engine.0=7.000000,0.000000,0.000000
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000

[piston_engine]
cylinder_displacement=148.13   //903.15    //130.700000
compression_ratio=6.70    ///6.700000
number_of_cylinders=6
max_rated_rpm=1600.000000
max_rated_hp=200.000000
fuel_metering_type=1
cooling_type=1
normalized_starter_torque=0.055000
turbocharged=0
max_design_mp=29.999999
min_design_mp=1.000000
critical_altitude=18700.000000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000

[propeller]
//propeller_type=1
propeller_diameter=10.833000
propeller_blades=2
propeller_moi=33.370000
beta_max=53.500000
beta_min=18.500000
min_gov_rpm=200.000000
prop_tc=0.010000
gear_reduction_ratio=1.778000
fixed_pitch_beta=0.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0.000000
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000
propeller_type=0

[Reference Speeds]
flaps_up_stall_speed=41.000000
full_flaps_stall_speed=32.800000
cruise_speed=98.121134
max_indicated_speed=260.500000

[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000

[autopilot]
autopilot_available=0
flight_director_available=0
[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=6.930556

[stall_warning]
type=1
stick_shaker=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[direction_indicators]
direction_indicator.0=1,0
[pitot_static]
pitot_heat=0.000000
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,1,1
[pneumatic_system]
max_pressure=120.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0


[CameraDefinition.0]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
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 = 1.0
ShowWeather = Yes
InitialXyz = 9.0, 0.38, -1.5
InitialPbh = 5, 0, 280
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.1]
Title = "Left Wing"
Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED}
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 = 1.0
ShowWeather = Yes
InitialXyz = -9.0, 0.38, -1.5
InitialPbh = 5, 0, 80
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.2]
Title = "Tail"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description = Looking forward from the tip of the vertical stabilizer
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
ShowWeather = Yes
InitialXyz = 0, 1.9, -10.75
InitialPbh = 11, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum