[fltsim.0] title=airbike sim=airbike model= panel= sound= texture= kb_checklists= kb_reference= atc_type=Lear atc_id_enable=1 atc_id=airbike description=In late 2008 several sightings of a fantastic 'airbike' were made near the same time news stories appeared describing a military scandal, where the plans and protoype for a jet-powered 'superbike' went missing, an embarrassment for the government as the superbike was never to have existed. A mysterious black-clad figure has been spotted recently jetting low across the mountains of Afghanistan, spraying terrorist outposts with explosive-tipped bullets from a screaming-fast jet-bike. In numerous internet posts and blogs, the vehicle has beened dubbed the 'Black Shark Infiltrator' due to it's appearance, and is the subject of rampant speculation and buzz among tuners and speed freaks worldwide. Is 'The Black Shark' a super-hero of some kind? A super-villain? A vigilante? Assassin? Soldier of fortune? It seems that only time will tell....as we watch the skies. visual_damage=1 ui_manufacturer=Hark Aerospace Inc. ui_type=airbike ui_variation='Black Shark' Infiltrator [General] atc_type= atc_model= editable=1 performance=VTOL capability with full flaps. Cruises around 525 knots. Top end upgraded with triple-engine reheat. [WEIGHT_AND_BALANCE] reference_datum_position=0.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=20000.000 empty_weight_roll_MOI=300000.000000 empty_weight_pitch_MOI=300000.000000 empty_weight_yaw_MOI=950000.000000 empty_weight_coupled_MOI=1200.000000 max_gross_weight=20000.000000 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 1 LeftMain = 0, 1, 0, 100, 0 LeftAux = 0, -7.8, 0, 40, 0 RightMain = 0, -1, 0, 100, 0 RightAux = 0, 7.8, 0, 40, 0 electric_pump=0 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing: Fore/Aft, Left/Right, Up/down: Fx type light.0 = 3, -0.21, 0.00, 2.50, fx_vclight_whi , light.1 = 6, -6.41, 1.81, -1.50, RD_BATBURNER , light.2 = 6, -6.41, -1.81, -1.50, RD_BATBURNER , light.3 = 6, -0.53, 0.00, -1.18, RD_BATBURNER , light.4 = 3, -4.20, 2.42, -1.33, fx_navgre , light.5 = 3, -4.20, -2.42, -1.33, fx_navred , light.6 = 3, 2.20, 0.00, 1.17, fx_navwhi , light.7 = 3, 0.22, 0.00, 1.44, fx_vclight_whi light.8 = 3, -3.71, 0.00, 0.20, fx_beacon , light.9 = 3, -3.69, 0.00, 0.20, fx_navred , light.10 = 3, 0.56, 0.70, 0.18, NAV_Blue3 , light.11 = 3, 0.56, -0.71, 0.18, NAV_Blue3 , [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 0.03 engine.0 = 0, 0, 0, engine.1 = 0, 0, 0, engine.3 = 0, 0, 0, min_throttle_limit=-0. [jet_engine] thrust_scalar =1.2 [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks [contact_points] //0 Class 0-none 1-wheel 2-scrape point 3-skid 4-float 5-water rudder //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 / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal //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=1.0 ,6.8, -1.6, -4.39, 19950.8, 0.0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 2.0, 0.0, 0.0 point.1=1.0 ,6.8, 1.6, -4.39, 19950.8, 1.0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 2.0, 0.0, 0.0 point.2=1.0 ,-4.5, -3.2, -4.21, 19950.8, 2.0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 3.0, 0.0, 0.0 point.3=1.0 ,-4.5, 3.2, -4.21, 19950.8, 0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 3.0, 0.0, 0.0 point.4=1.0 ,7.99, -1.6, -4.39, 19950.8, 0.0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 2.0, 0.0, 0.0 point.5=1.0 ,7.99, 1.6, -4.39, 19950.8, 1.0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 2.0, 0.0, 0.0 point.6 = 2, 6.21, 0.00, -1.25, 19950.8, 0.0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 2.0, 0.0, 0.0 point.7 = 2, -1.45, 1.84, -1.53, 19950.8, 0.0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 2.0, 0.0, 0.0 point.8 = 2, -1.45, -1.84, -1.53, 19950.8, 0.0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 2.0, 0.0, 0.0 point.9 = 2, -5.34, 3.50, -2.75, 19950.8, 0.0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 2.0, 0.0, 0.0 point.10 = 2, -5.34, -3.50, -2.75, 19950.8, 0.0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 2.0, 0.0, 0.0 point.11 = 2, 2.77, 0.00, 0.36, 19950.8, 0.0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 2.0, 0.0, 0.0 point.12 = 2, -0.75, 0.00, 2.40, 19950.8, 0.0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 2.0, 0.0, 0.0 point.13 = 2, 5.71, 0.00, -1.70, 19950.8, 0.0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 2.0, 0.0, 0.0 point.14 = 2, -6.41, 1.81, -1.50, 19950.8, 0.0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 2.0, 0.0, 0.0 point.15 = 2, -6.41, -1.81, -1.50, 19950.8, 0.0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 2.0, 0.0, 0.0 point.16 = 2, 6.19, 0.00, -0.66, 19950.8, 0.0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 2.0, 0.0, 0.0 //point.17 = 2, -3.0, 0.0, -2.85, 19950.8, 0.0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 2.0, 0.0, 0.0 //point.18 = 2, 6.8, 0.0, 2.95, 19950.8, 0.0, 0.6475, 43.1, 0.55, 0.8, 0.8, 3.75, 3.75, 2.0, 0.0, 0.0 static_pitch=0.000000 static_cg_height=2.75 gear_system_type=0 [exits] number_of_exits=2 exit_rate.0=0.2 ;Percent per second exit_rate.1=0.5 [TailHook] tailhook_length=4.6 //feet) tailhook_position=-9.21, 0.0, 2.84 //(feet) longitudinal, lateral, vertical positions from datum (-2.84) cable_force_adjust=1.0 [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.12,0.11 ;Percent per second [keyboard_response] elevator = 150.000000, 250.000000 aileron = 150.000000, 250.000000 rudder = 150.000000, 250.000000 [forcefeedback] gear_bump_nose_magnitude = 6000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 6000 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 6000 gear_bump_right_direction = 00500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 3250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5.0 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 750 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1.0 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 [airplane_geometry] //ACM_AREAW1// 0,0,0,10.0825,0.7293,0.7293,0.1155,9.6941,1.4586,1.4586 //ACM_AREAW2// 0.2310,9.3055,2.1884,2.1884,0.3465,8.9167,2.9179,2.9179,0.4620,8.5283 //ACM_AREAW3// 3.6473,3.6473,0.5776,8.1393,4.3769,4.3769,0.6930,7.7511,5.1064,5.1064 //ACM_AREAW4// 0.8087,7.3625,5.8358,5.8358,0.9243,6.9738,6.5651,6.5651,1.0398,6.5851 //ACM_AREAH1// 0,0,0,2.1914,0.3652,0.3652,0,2.0817,0.7304,0.7304 //ACM_AREAH2// 0,1.9723,1.0957,1.0957,0,1.8624,1.4608,1.4608,0,1.7532 //ACM_AREAH3// 1.8262,1.8262,0,1.6433,2.1914,2.1914,0,1.5340,2.5566,2.5566 //ACM_AREAH4// 0,1.4242,2.9219,2.9219,0,1.3149,3.2871,3.2871,0,1.2051 //ACM_AREAV1// 0,0,0,1.4234,0.1580,0.1580,0.1580,1.4677,0.3163,0.3163 //ACM_AREAV2// 0.3163,1.5118,0.4744,0.4744,0.4744,1.5562,0.6326,0.6326,0.6326,1.6002 //ACM_AREAV3// 0.7907,0.7907,0.7907,1.6447,0.9488,0.9488,0.9488,1.6891,1.1071,1.1071 //ACM_AREAV4// 1.1071,1.7331,1.2652,1.2652,1.2652,1.7776,1.4234,1.4234,1.4234,1.8219 //ACM_CAREAW1// 3.2825,3.2825,5.5612,7.5777,3.6473,3.6473,5.6188,7.5348,4.0121,4.0121 //ACM_CAREAW2// 5.6767,7.4917,4.3769,4.3769,5.7346,7.4485,4.7416,4.7416,5.7923,7.4056 //ACM_CAREAW3// 5.1064,5.1064,5.8501,7.3625,5.4710,5.4710,5.9078,7.3193,5.8358,5.8358 //ACM_CAREAW4// 5.9657,7.2764,6.2006,6.2006,6.0233,7.2333,6.5651,6.5651,6.0812,7.1901 //ACM_CAREAH1// 0,0,1.0957,2.1914,0.3652,0.3652,1.0957,2.1366,0.7304,0.7304 //ACM_CAREAH2// 1.0957,2.0817,1.0957,1.0957,1.0957,2.0271,1.4608,1.4608,1.0957,1.9723 //ACM_CAREAH3// 1.8262,1.8262,1.0957,1.9175,2.1914,2.1914,1.0957,1.8624,2.5566,2.5566 //ACM_CAREAH4// 1.0957,1.8078,2.9219,2.9219,1.0957,1.7532,3.2871,3.2871,1.0957,1.6984 //ACM_CAREAV1// 0,0,0.3558,1.0671,0.1580,0.1580,0.5138,1.1684,0.3163,0.3163 //ACM_CAREAV2// 0.6721,1.2697,0.4744,0.4744,0.8302,1.3710,0.6326,0.6326,0.9883,1.4723 //ACM_CAREAV3// 0.7907,0.7907,1.1466,1.5736,0.9488,0.9488,1.3047,1.6748,1.1071,1.1071 //ACM_CAREAV4// 1.4629,1.7761,1.2652,1.2652,1.6210,1.8773,1.4234,1.4234,1.7790,1.9785 wing_area = 995.000000 wing_span = 43.08 wing_root_chord = 33.08 wing_dihedral = 1 wing_incidence = -0.5 wing_twist = -0.99 oswald_efficiency_factor = 0.9 wing_winglets_flag = 0 wing_sweep = 9 wing_pos_apex_lon = 5.02 wing_pos_apex_vert = 0 htail_area = 200.000000 htail_span = 21.57 htail_pos_lon = -20.82 htail_pos_vert = 0 htail_incidence = 0.000000 htail_sweep = 0 vtail_area = 150.000000 vtail_span = 4.67 vtail_sweep = 45 vtail_pos_lon = -8.92 vtail_pos_vert = 0.65 elevator_area = 70.000000 aileron_area = 143.800000 rudder_area = 42.500000 elevator_up_limit = 15.501974 elevator_down_limit = 20.626481 aileron_up_limit = 15.480565 aileron_down_limit = 15.896903 rudder_limit = 45 elevator_trim_limit = 19.480565 spoiler_limit = 90.1 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 spoilerons_available = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 electric_always_available = 1 [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=1 Marker.1=1 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=0.6 induced_drag_scalar=0.3 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=3.0 // Bring this down to 1.0 if the radical rudder response bugs you... pitch_stability=1.5 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [TurbineEngineData] fuel_flow_gain=1 inlet_area=20.861 rated_N2_rpm=27920.000 //22920.00 static_thrust=7775.999 //Was 16775.999 afterburner_available=1 reverser_available=1 [Views] eyepoint=12.912, 0.0, 2.512 //(feet) longitudinal, lateral, vertical distance from reference datum [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=2500.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=100.000000 pitch_takeoff_ga=8.000000 use_no_default_bank=1 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=35.000000 max_bank_acceleration=2.800000 max_bank_velocity=5.000000 max_throttle_rate=0.100000 nav_proportional_control=20 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=25 gs_integrator_control=0.53 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=1.000000 [direction_indicators] direction_indicator.0=3,0 [flaps.0] type = 1 // 1 - trail, 2 - lead span-outboard = 0.5 // 0.0 .. 1.0 extending-time = 4.5 // seconds flaps-position.0 = 0 // degrees //flaps-position.1 = 2.4,0.000000 // degrees //flaps-position.2 = 7.7,0.000000 // degrees //flaps-position.3 = 11.9,0.000000 // degrees //flaps-position.4 = 11.9,0.000000 // degrees flaps-position.1 = 17.4,0.000000 // degrees flaps-position.2 = 26.7,0.000000 // degrees flaps-position.3 = 39.9,0.000000 // degrees flaps-position.4 = 74.9,0.000000 // degrees damaging-speed = 300 // KIAS blowout-speed = 250 // KIAS lift_scalar = 0.01 drag_scalar = 0.01 pitch_scalar= 0.01 system_type = 0 //Hydraulic [flaps.1] type = 2 // 1 - trail, 2 - lead span-outboard = 0.5 // 0.0 .. 1.0 extending-time = 4.5 // seconds flaps-position.0 = 0.0 // degrees //flaps-position.1 = 0.05 //degrees //flaps-position.2 = 0.15 // degrees //flaps-position.3 = 0.3 // degrees //Flaps-position.4 = 0.45 // degrees flaps-position.1 = 3.25 // degrees flaps-position.2 = 12.0 // degrees flaps-position.3 = 40.0 // degrees flaps-position.4 = 30.0 // degrees damaging-speed = 300 // KIAS blowout-speed = 250 // KIAS lift_scalar = 1.0 drag_scalar = 2 pitch_scalar= 1 system_type = 0 //Hydraulic [flaps.2] type = 2 // 1 - trail, 2 - lead span-outboard = 0.5 // 0.0 .. 1.0 extending-time = 4.5 // seconds flaps-position.0 = 0 // degrees //flaps-position.1 = 0 // degrees //flaps-position.2 = 0 // degrees //flaps-position.3 = 0 // degrees //flaps-position.4 = 30.000000 // degrees flaps-position.1 = 45.000000 // degrees flaps-position.2 = 60.000000 // degrees flaps-position.3 = 90.000000 // degrees flaps-position.4 = 40.0 // degrees damaging-speed = 300 // KIAS blowout-speed = 250 // KIAS lift_scalar = 0.0 drag_scalar = 0.0 pitch_scalar= 0.0 system_type = 0 //Hydraulic [flaps.3] type = 1 // 1 - trail, 2 - lead span-outboard = 0.5 // 0.0 .. 1.0 extending-time = 4.5 // seconds flaps-position.0 = 0 // degrees //flaps-position.1 = 0 //degrees //flaps-position.2 = 0 // degrees //flaps-position.3 = 0 // degrees// //Flaps-position.4 = 0 // degrees flaps-position.1 = 0 // degrees flaps-position.2 = 0 // degrees flaps-position.3 = 0 // degrees flaps-position.4 = 0.0 // degrees damaging-speed = 300 // KIAS blowout-speed = 250 // KIAS lift_scalar = 0.0 drag_scalar = 0.0 pitch_scalar= 0.0 system_type = 0 //Hydraulic [Reference Speeds] flaps_up_stall_speed=180.000000 full_flaps_stall_speed=1.000000 cruise_speed=.1600 max_indicated_speed=31000 max_mach=5.0 [brakes] toe_brakes_scale=1.000061 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
