[fltsim.0]
title=L2 Blender (#01)
sim=L2
model=SL_E
panel=VC
sound=L2
texture=L2B
kb_checklists=
kb_reference=
kb_notes=
atc_id=TEST101
atc_airline=Lockheed Martin
atc_flight_number=101
ui_manufacturer=Lockheed Martin
ui_type=L2_Blender with VC
ui_variation=Hypersonic Test Aircraft
ui_typerole=Military Jet
ui_createdby=Pedro Mayorga
atc_heavy=0
visual_damage=0
atc_type=Blender
atc_model=L2
Description=L2 Hypersonic Concept Aircraft, \n\nwingspan=13M \nLength=23.4M \npowerplant=(2) Pulse Detonation w\/ Scramjets Engines \n\nThe blueprints of L2_Blender was inspired in "Blender" original concept of Turbosquid® \nThis 3D Model was developed with educational purposes. \nUse of USAF, Lockheed Martin, P&W, Boeing, Nasa and JPL Logos are with educational purposes. \nNo copyright infringement intended. July 2011.\n\n\n
[fltsim.1]
title=L2 Blender (#02)
sim=L2
model=GBU
panel=VC
sound=L2
texture=101
kb_checklists=
kb_reference=
kb_notes=
atc_id=USAF101
atc_airline=USAF
atc_flight_number=101
ui_manufacturer=Lockheed Martin
ui_type=L2_Blender with VC
ui_variation=L2B w/ GBU
ui_typerole=Military Jet
ui_createdby=Pedro Mayorga
atc_heavy=0
visual_damage=0
atc_type=Blender
atc_model=L2
Description=L2 Hypersonic Concept Aircraft, \n\nwingspan=13M \nLength=23.4M \npowerplant=(2) Pulse Detonation w\/ Scramjets Engines \n\nThe blueprints of L2_Blender was inspired in "Blender" original concept of Turbosquid® \nThis 3D Model was developed with educational purposes. \nUse of USAF, Lockheed Martin, P&W, Boeing, Nasa and JPL Logos are with educational purposes. \nNo copyright infringement intended. July 2011.\n\n\n
[fltsim.2]
title=L2 Blender (#03)
sim=L2
model=CAM
panel=VC
sound=L2
texture=CAM
kb_checklists=
kb_reference=
kb_notes=
atc_id=USAF101
atc_airline=USAF
atc_flight_number=101
ui_manufacturer=Lockheed Martin
ui_type=L2_Blender with VC
ui_variation=L2B w/ H-CAM
ui_typerole=Military Jet
ui_createdby=Pedro Mayorga
atc_heavy=0
visual_damage=0
atc_type=Blender
atc_model=L2
Description=L2 Hypersonic Concept Aircraft, \n\nwingspan=13M \nLength=23.4M \npowerplant=(2) Pulse Detonation w\/ Scramjets Engines \n\nThe blueprints of L2_Blender was inspired in "Blender" original concept of Turbosquid® \nThis 3D Model was developed with educational purposes. \nUse of USAF, Lockheed Martin, P&W, Boeing, Nasa and JPL Logos are with educational purposes. \nNo copyright infringement intended. July 2011.\n\n\n
[fltsim.3]
title=L2 Blender (#04)
sim=L2
model=A120
panel=VC
sound=L2
texture=A120
kb_checklists=
kb_reference=
kb_notes=
atc_id=USAF101
atc_airline=USAF
atc_flight_number=101
ui_manufacturer=Lockheed Martin
ui_type=L2_Blender with VC
ui_variation=L2B w/ AIM120
ui_typerole=Military Jet
ui_createdby=Pedro Mayorga
atc_heavy=0
visual_damage=0
atc_type=Blender
atc_model=L2
Description=L2 Hypersonic Concept Aircraft, \n\nwingspan=13M \nLength=23.4M \npowerplant=(2) Pulse Detonation w\/ Scramjets Engines \n\nThe blueprints of L2_Blender was inspired in "Blender" original concept of Turbosquid® \nThis 3D Model was developed with educational purposes. \nUse of USAF, Lockheed Martin, P&W, Boeing, Nasa and JPL Logos are with educational purposes. \nNo copyright infringement intended. July 2011.\n\n\n
[fltsim.4]
title=L2 Blender (#05)
sim=L2
model=A17
panel=VC
sound=L2
texture=101
kb_checklists=
kb_reference=
kb_notes=
atc_id=USAF101
atc_airline=USAF
atc_flight_number=101
ui_manufacturer=Lockheed Martin
ui_type=L2_Blender with VC
ui_variation=L2B w/ MK17 Atomic Bomb
ui_typerole=Military Jet
ui_createdby=Pedro Mayorga
atc_heavy=0
visual_damage=0
atc_type=Blender
atc_model=L2
Description=L2 Hypersonic Concept Aircraft, \n\nwingspan=13M \nLength=23.4M \npowerplant=(2) Pulse Detonation w\/ Scramjets Engines \n\nThe blueprints of L2_Blender was inspired in "Blender" original concept of Turbosquid® \nThis 3D Model was developed with educational purposes. \nUse of USAF, Lockheed Martin, P&W, Boeing, Nasa and JPL Logos are with educational purposes. \nNo copyright infringement intended. July 2011.\n\n\n
[fltsim.5]
title=L2 Blender (#06)
sim=L2
model=M82
panel=VC
sound=L2
texture=101
kb_checklists=
kb_reference=
kb_notes=
atc_id=USAF101
atc_airline=USAF
atc_flight_number=101
ui_manufacturer=Lockheed Martin
ui_type=L2_Blender with VC
ui_variation=L2B w/ MK82 Bombs
ui_typerole=Military Jet
ui_createdby=Pedro Mayorga
atc_heavy=0
visual_damage=0
atc_type=Blender
atc_model=L2
Description=L2 Hypersonic Concept Aircraft, \n\nwingspan=13M \nLength=23.4M \npowerplant=(2) Pulse Detonation w\/ Scramjets Engines \n\nThe blueprints of L2_Blender was inspired in "Blender" original concept of Turbosquid® \nThis 3D Model was developed with educational purposes. \nUse of USAF, Lockheed Martin, P&W, Boeing, Nasa and JPL Logos are with educational purposes. \nNo copyright infringement intended. July 2011.\n\n\n
[fltsim.6]
title=L2 Blender (#07)
sim=L2
model=CAM
panel=VC
sound=L2
texture=101
kb_checklists=
kb_reference=
kb_notes=
atc_id=USAF101
atc_airline=USAF
atc_flight_number=101
ui_manufacturer=Lockheed Martin
ui_type=L2_Blender with VC
ui_variation=L2B Dark w/ H-CAM
ui_typerole=Military Jet
ui_createdby=Pedro Mayorga
atc_heavy=0
visual_damage=0
atc_type=Blender
atc_model=L2
Description=L2 Hypersonic Concept Aircraft, \n\nwingspan=13M \nLength=23.4M \npowerplant=(2) Pulse Detonation w\/ Scramjets Engines \n\nThe blueprints of L2_Blender was inspired in "Blender" original concept of Turbosquid® \nThis 3D Model was developed with educational purposes. \nUse of USAF, Lockheed Martin, P&W, Boeing, Nasa and JPL Logos are with educational purposes. \nNo copyright infringement intended. July 2011.\n\n\n
[fltsim.7]
title=L2 Blender (#8)
sim=L2
model=VCCAM
panel=VCCAM
sound=L2
texture=101
kb_checklists=
kb_reference=
kb_notes=
atc_id=USAF101
atc_airline=USAF
atc_flight_number=101
ui_manufacturer=Lockheed Martin
ui_type=L2_Blender with VCCAM
ui_variation=L2B Dark w/ H-CAM
ui_typerole=Military Jet
ui_createdby=Pedro Mayorga
atc_heavy=0
visual_damage=0
atc_type=Blender
atc_model=L2
Description=L2 Hypersonic Concept Aircraft, \n\nwingspan=13M \nLength=23.4M \npowerplant=(2) Pulse Detonation w\/ Scramjets Engines \n\nThe blueprints of L2_Blender was inspired in "Blender" original concept of Turbosquid® \nThis 3D Model was developed with educational purposes. \nUse of USAF, Lockheed Martin, P&W, Boeing, Nasa and JPL Logos are with educational purposes. \nNo copyright infringement intended. July 2011.\n\n\n
[fltsim.8]
title=L2 Blender (#9)
sim=L2
model=PW2
panel=VC
sound=L2
texture=101
kb_checklists=
kb_reference=
kb_notes=
atc_id=USAF101
atc_airline=USAF
atc_flight_number=101
ui_manufacturer=Lockheed Martin
ui_type=L2_Blender with VC
ui_variation=L2B w/ Paveway-II Bomb
ui_typerole=Military Jet
ui_createdby=Pedro Mayorga
atc_heavy=0
visual_damage=0
atc_type=Blender
atc_model=L2
Description=L2 Hypersonic Concept Aircraft, \n\nwingspan=13M \nLength=23.4M \npowerplant=(2) Pulse Detonation w\/ Scramjets Engines \n\nThe blueprints of L2_Blender was inspired in "Blender" original concept of Turbosquid® \nThis 3D Model was developed with educational purposes. \nUse of USAF, Lockheed Martin, P&W, Boeing, Nasa and JPL Logos are with educational purposes. \nNo copyright infringement intended. July 2011.\n\n\n
[fltsim.9]
title=L2 Blender (#10)
sim=L2
model=VCCAM
panel=VCCAM
sound=L2
texture=CAM
kb_checklists=
kb_reference=
kb_notes=
atc_id=USAF101
atc_airline=USAF
atc_flight_number=101
ui_manufacturer=Lockheed Martin
ui_type=L2_Blender with VCCAM
ui_variation=L2B w/ H-CAM
ui_typerole=Military Jet
ui_createdby=Pedro Mayorga
atc_heavy=0
visual_damage=0
atc_type=Blender
atc_model=L2
Description=L2 Hypersonic Concept Aircraft, \n\nwingspan=13M \nLength=23.4M \npowerplant=(2) Pulse Detonation w\/ Scramjets Engines \n\nThe blueprints of L2_Blender was inspired in "Blender" original concept of Turbosquid® \nThis 3D Model was developed with educational purposes. \nUse of USAF, Lockheed Martin, P&W, Boeing, Nasa and JPL Logos are with educational purposes. \nNo copyright infringement intended. July 2011.\n\n\n
[General]
atc_type=Lockheed
atc_model=L2B
Performance=1720+ KIAS sea level - 97,000 ft ceiling - Max Speed: Mach 5.1
Category=airplane
[Weight_And_Balance]
reference_datum_position= 0.00,0.0,0.0
empty_weight_CG_position=-2.19,0.0,0.0
CG_forward_limit=5.0
CG_aft_limit= -5.0
empty_weight=12982.0
max_gross_weight=19000.0
max_number_of_stations=50
station_load.0=170.0,14.3,0.0,0.0
//Moments of Inertia
empty_weight_roll_MOI=253103.5
empty_weight_pitch_MOI=822901.3
empty_weight_yaw_MOI=814707.9
empty_weight_coupled_MOI=50.0
[Fuel]
LeftMain= -3.13,-8.4,0.0,150.0,0.0
RightMain=-3.13, 8.4,0.0,150.0,0.0
Center1= 0.00, 0.0,0.0,300.0,0.0
fuel_type=2
number_of_tank_selectors=1
electric_pump=1
[contact_points]
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS) //SA //SC MSC /DR //ET /RT /SN KRTR KDMG
//Center Gear
point.0 = 1, 14.4, 0.00, -7.9, 8662, 0, 1, 60, 0.25, 0.3, 0.94, 3.5, 3.5, 0, 0, 0
//Left Gear
point.1 = 1, -19.8,-9.70, -7.6, 8662, 1, 1, 0, 0.75, 0.2, 0.58, 3.5, 3.5, 0, 0, 0
//Right Gear
point.2 = 1, -19.8, 9.70, -7.6, 8662, 2, 1, 0, 0.75, 0.2, 0.58, 3.5, 3.5, 0, 0, 0
//Structural contact points
point.3 = 2, 26.10, 0.00, -2.6, 780, 0, 0.0000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.0, 0.0
point.4 = 2, -24.00, -17.25, -2.45, 780, 0, 0.0000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.0, 0.0
point.5 = 2, -24.00, 17.25, -2.45, 780, 0, 0.0000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.0, 0.0
point.6 = 2, -13.00, -9.7, -4.50, 780, 0, 0.0000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.0, 0.0
point.7 = 2, -13.00, 9.7, -4.50, 780, 0, 0.0000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.0, 0.0
point.8 = 2, -29.0, -4.5, -4.00, 780, 0, 0.0000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9, 0.0, 0.0
point.9 = 2, -29.0, 4.5, -4.00, 780, 0, 0.0000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9, 0.0, 0.0
// Details:
// 14.4, 0.00, -7.5, // Contact point specific position CG
// -19.8,-9.7, -7.0, // Contact point specific position LG
// -19.8, 9.7, -7.0, // Contact point specific position RG
// 26.10, 0.00, -2.6, // Structural contact point specific position Nose
// -24.00, -17.25, -2.45, // Structural contact point specific position LWing
// -24.00, 17.25, -2.45, // Structural contact point specific position RWing
// -13.00, -9.7, -4.50, // Structural contact point specific position LFlap
// -13.00, 9.7, -4.50, // Structural contact point specific position RFlap
// -29.0, -4.5, -4.00, // Structural contact point specific position LEngine
// -29.0, 4.5, -4.00, // Structural contact point specific position REngine
static_pitch = 0.0
static_cg_height = 6.7
max_number_of_points = 10 // 7
gear_system_type=1 // 0
[airplane_geometry]
wing_area = 400.0 //Square feet
wing_span = 37.4 //Feet
wing_root_chord = 13.3 //Feet
wing_dihedral = 2.5 //Degrees
wing_incidence = -1.0 //Degrees
wing_twist = -1.5 //Degrees
oswald_efficiency_factor= 0.85 //Measure of lift effeciency of wing
wing_winglets_flag = 1 //Are winglets available?
wing_sweep = 20.0 //Degrees, wing leading edge
wing_pos_apex_lon = -27.7 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 88.26 //Square feet
htail_span = 21.6 //Feet
htail_pos_lon = -47.6 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 42.8 //Degrees, horizontal tail leading edge
vtail_area = 1050 //Square feet
vtail_span = 7.8 //Feet, tip to body
vtail_sweep = 45.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -42.3 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 4.5 //Feet, vertical distance from reference point, positive going up
elevator_area = 27.0 //Square feet
aileron_area = 13.5 //Square feet
rudder_area = 45.0 //Square feet 27.3
elevator_up_limit = 19.0 //Degrees
elevator_down_limit = 19.5 //Degrees
aileron_up_limit = 19.0 //13 Degrees
aileron_down_limit = 18.0 //12 Degrees
rudder_limit = 45.0 // used for nosewheel animation //Degrees
elevator_trim_limit = 15.0 //Degrees
spoiler_limit = 80.0 //Degrees
spoiler_extension_time = 0.4 //Seconds
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons= 0.0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available = 0
positive_g_limit_flaps_up = 37.5 //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down= 37.5 //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up = -35.0 //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down= -35.0 //Design G load tolerance (negative, flaps down)
[Views]
eyepoint=0,0,0 // VC origin datum
zoom=1.0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi
light.0=4, 15.00, 0.0, 1.5, fx_litewash // cockpit lighting interior view
light.1=6, 15.00, 0.00, -4.36, fx_vclight
light.2=2, -24.00, 0.00, -2.40, fx_strobe
light.3=3, -24.50, -11.16, 1.88, fx_kbeaconred //fx_navred
light.4=3, -24.50, 11.16, 1.88, fx_kbeacongreen //fx_navgre
light.5=3, -24.00, -17.02, -2.42, fx_navred
light.6=3, -24.00, 17.02, -2.42, fx_navgre
light.7= 9, -32.0, -4.5, -3.0, fx_reheat_Alpha Viggen
light.8=9, -32.0, 4.5, -3.0, fx_reheat_Alpha Viggen
light.9=7, -32.0, -4.5, -3.0, fx_engine_Alpha Viggen
light.10=7, -32.0, 4.5, -3.0, fx_engine_Alpha Viggen
light.11=4, 0.0, 0.0, 2.5, fx_litewash
[smokesystem]
smoke.0 = -22.00, -11.16, -1.00, F7MG_fx_afterburner
smoke.1 = -22.00, 11.16, -1.00, F7MG_fx_afterburner
smoke.2 = -20.50, -11.16, -0.50, F7MG_fx_exhaust_smoke
smoke.3 = -20.50, 11.16, -0.50, F7MG_fx_exhaust_smoke
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_m, 1
[flight_tuning]
cruise_lift_scalar = 0.8
parasite_drag_scalar = 2.0
induced_drag_scalar = 1.5
elevator_effectiveness = 0.9
aileron_effectiveness = 0.5
rudder_effectiveness = 1.2
pitch_stability = 2.0
roll_stability = 2.0
yaw_stability = 2.0
elevator_trim_effectiveness = 0.3
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[brakes]
toe_brakes_scale=5.000061
parking_brake=1
[Flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 10 // degrees
flaps-position.2 = 20 // degrees
damaging-speed = 350 // KIAS
blowout-speed = 450 // KIAS
[Flaps.1]
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 10 // degrees
flaps-position.2 = 20 // degrees
damaging-speed = 350 // KIAS
blowout-speed = 450 // KIAS
[Flaps.2]
type=1
span-outboard=0.45
extending-time=5.0
system_type=1
damaging-speed980.0
blowout-speed=990.0
lift_scalar=1.0
drag_scalar=1.0
pitch_scalar=0.0
flaps-position.0= 0.0,0.0
flaps-position.1= 0.0,0.0
flaps-position.2= 12.0,0.0
flaps-position.3= 25.0,0.0
[Flaps.3]
type=2
span-outboard=0.45
extending-time=5.0
system_type=1
damaging-speed=0.0
blowout-speed=0.0
lift_scalar=0.1
drag_scalar=0.1
pitch_scalar=0.0
flaps-position.0= 0.0,0.0
flaps-position.1= 25.0,0.0
flaps-position.2= 30.0,0.0
flaps-position.3= 35.0,0.0
[Reference Speeds]
flaps_up_stall_speed=130.000
full_flaps_stall_speed=85.0
cruise_speed=660.0
max_indicated_speed=3200.000000
max_mach=5.100000
[Folding_wings]
wing_fold_system_type=0
fold_rates=0.12,0.13
[TailHook]
tailhook_length=5.83
tailhook_position=-14.6, 0.0,-0.8
cable_force_adjust=1.0
[exits]
number_of_exits = 3
exit_rate.0 = 0.8 ;Percent per second
exit_rate.1 = 0.8 ;Percent per second
exit_rate.2 = 0.8 ;Percent per second
[GeneralEngineData]
engine_type = 1
Engine.0 = -15.8, -2.5, -0.1
Engine.1 = -15.8, 2.5, -0.1
fuel_flow_scalar = 0.001
min_throttle_limit = 0
[TurbineEngineData]
fuel_flow_gain = 0.006
inlet_area = 3.2895
rated_N2_rpm = 21728
static_thrust = 12000
afterburner_available = 1
afterburner_throttle_threshold = 0.90
reverser_available = 0
[jet_engine]
thrust_scalar = 1.0
[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=1,0,1
Adf.1=1
Transponder.1=1
Marker.1=1
[Autopilot]
autopilot_available=1
use_no_default_pitch=1
use_no_default_bank=1
flight_director_available=1
default_vertical_speed=500.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=95.0
pitch_takeoff_ga=8.0
default_pitch_mode=0
default_bank_mode=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
[Direction_indicators]
direction_indicator.0=3,0
[turn_indicators]
turn_indicator.0=1,0
[attitude_indicators]
attitude_indicator.0=1
[stall_warning]
type=1
stick_shaker=1
[GPWS]
max_warning_height = 0
sink_rate_fpm = -5000
excessive_sink_rate_fpm = -30000
climbout_sink_rate_fpm = -100
flap_and_gear_sink_rate_fpm= -10000
[hydraulic_system]
electric_pumps=1
engine_map=1,1,0,0
normal_pressure=4500.000000
[Electrical]
max_battery_voltage=27.9
generator_alternator_voltage=28.0
max_generator_alternator_amps=150.0
electric_always_available = 1
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
autopilot = 1, 5 , 17.0
avionics_bus = 0, 10, 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 20, 17.0
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pitot_static]
pitot_heat=1.000000
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=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=8900 ; 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
[Keyboard_response]
elevator=250.0, 500.0
aileron= 190.0, 380.0
rudder= 250.0, 500.0
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000