[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