// AI Helicopter configuration files // by Holger Sandmann (hsandman@sfu.ca) // and Doug Callihan // // Version 1, May 2003 // // for FS2002 default Bell 206B JetRanger // // based on Stemme motor glider aircraft.cfg // by Al Kaiser, kaiser@va-works.com or http://www.va-works.com/ // // !!!Copyright remains with the original authors!!! [fltsim.0] title=AI Bell 206B JetRanger RAFO-Royal Air Force Oman sim=stemme_as_helicopter_1 model= panel= sound= texture=NwBll206_4 atc_id= atc_heavy=0 prop_anim_ratio=1.71 ui_manufacturer=Bell ui_type=206B JetRanger ui_variation=Royal Air Force Oman description=The Bell 206 series has accumulated an astounding array of impressive statistics. More than 6,000 JetRangers are flying worldwide in roles as diverse as corporate transportation, police surveillance, and United States Army aviation training. The series has flown over 26 million flight hours, and a few JetRangers are flying with more than 30,000 hours on their airframes. atc_parking_types=RAMP atc_parking_codes=H19,M004 atc_flight_number= atc_airline=MAJAN visual_damage=0 [General] atc_type=BELL atc_model=B06 performance=Engine: Allison 250-C20J 420 shp\nCruise Speed: 115kts\/132mph\/213kmh\nMaximum Range: 435nm\/500m\/805km\nService Ceiling: 20,000ft\/6,096m\nHovering Ceiling: 19,600ft\/5974m\nFuel Capacity: 91 U.S. gal\/344ltr\nEmpty Weight: 1,640lbs\/744kg\nMax Gross Weight: 3,200lb\/1,451kg\nHook Load Limit: 1,500lb\/680kg\nLength: 31.2ft\/9.51m\nRotor Span: 33.3ft\/10.15m\nHeight: 11.7ft\/3.57m\nSeating: Up to 5\n //---- misc tweaked parameters [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position= 0.000,0.000,-2.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 max_gross_weight=2300 // (pounds) empty_weight=1300 ;Moments of Inertia empty_weight_pitch_MOI=3000 empty_weight_roll_MOI=4000 empty_weight_yaw_MOI=9000 empty_weight_coupled_MOI=-1000 CG_forward_limit=0.000 CG_aft_limit=1.000 [Reference Speeds] flaps_up_stall_speed=30 full_flaps_stall_speed=27 cruise_speed=80 max_indicated_speed=180.000000 [flight_tuning] cruise_lift_scalar=1.15 // was 1.15 parasite_drag_scalar=0.8 // was 0.8 induced_drag_scalar=0.8 // was 0.8 elevator_effectiveness=1.5 // was 1.0 aileron_effectiveness=1.0 rudder_effectiveness=2.0 // was 1.5 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=1.9 // was 1.0 [flaps.0] //Trailing Edge Flaps type=1 // 1 - tail, 2 - lead span-outboard=0.600 // 0.0 .. 1.0 extending-time=4.000 // seconds flaps-position.0=0 // degrees flaps-position.1=0 // degrees flaps-position.2=20 // degrees flaps-position.3=30 // degrees damaging-speed=200 // KIAS blowout-speed=250 // KIAS lift_scalar=1.3 drag_scalar=0.8 pitch_scalar=1.2 system_type=0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None //---- parameters from B206b, tweaked //0 Class <0=none,1=wheel, 2=scrape, 3=skid> //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) [contact_points] point.0= 1.000, -2.930, -4.188, -4.691, 3000.000, 1.000, 0.519, 90.000, 0.500, 0.750, 0.850, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, -2.930, 4.188, -4.691, 3000.000, 2.000, 0.519, 90.000, 0.500, 0.750, 0.850, 0.000, 0.000, 0.000, 0.000, 0.000 point.2= 1.000, 5.320, -4.188, -4.892, 3000.000, 1.000, 0.519, 90.000, 0.500, 0.750, 0.850, 0.000, 0.000, 0.000, 0.000, 0.000 point.3= 1.000, 5.320, 4.188, -4.892, 3000.000, 2.000, 0.519, 90.000, 0.500, 0.750, 0.850, 0.000, 0.000, 0.000, 0.000, 0.000 //point.0=3, 4.83, 3.33, -4.50, 1574.8, 0, 0.5187, 0.0, 0.286975, 2.5, 0.605067, 0.0, 0.0, 0.0, 0.0, 0.0 //point.1=3, -3.50, -3.33, -4.58, 1574.8, 0, 0.5187, 0.0, 0.396299, 2.5, 0.728164, 0.0, 0.0, 2.0, 0.0, 0.0 //point.2=3, -3.50, 3.33, -4.58, 1574.8, 0, 0.5187, 0.0, 0.396299, 2.5, 0.728164, 0.0, 0.0, 3.0, 0.0, 0.0 //point.3=3, 4.83, -3.33, -4.50, 1574.8, 0, 0.5187, 0.0, 0.286975, 2.5, 0.605067, 0.0, 0.0, 1.0, 0.0, 0.0 //point.4=2, 0.00, -16.67, 9.00, 0.0, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 5.0, 0.0, 0.0 //point.5=2, 0.00, 16.67, 9.00, 0.0, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 6.0, 0.0, 0.0 //point.6=2, -20.50, 0.00, 1.67, 787.4, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 9.0, 0.0, 0.0 //point.7=2, 0.00, 9.08, 2.58, 787.4, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 4.0, 0.0, 0.0 static_pitch = 0.0 // was 0.198 static_cg_height = 4.7 // was 4.600 [Views] eyepoint = 1.69, 1.23, 1.95 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -15.00, -2.80, 2.27, fx_navred , light.1=3, -15.00, 2.80, 2.27, fx_navgre , light.2=3, -23.05, 0.00, 2.95, fx_navwhi , light.3=1, -22.45, 0.44, 6.54, fx_beacon , light.4=2, -5.78, 0.00, 4.58, fx_strobe , light.5=4, 2.00, 0.00, 1.50, fx_vclight , [effects] water=fx_spray dirt = fx_tchdrt concrete = fx_tchdrt, 1 touchdown = fx_dustcloud_m, 1 startup=fx_engstrt //touchdown = fx_tchdwn, 1 //landrotorwash = fx_rtr_lnd //waterrotorwash = fx_rtr_wtr wake=fx_wake [SMOKESYSTEM] smoke.0=0.00,-5.00,0.00, fx_engsmoke //---- parameters from Stemme motor glider, tweaked [fuel] LeftMain=-0.250000,-2.100000,2.500000,6.000000,0.000000 RightMain=-0.250000,2.100000,2.500000,6.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=400 // was 201.0 wing_span=60 // was 57.0 wing_root_chord=4.916670 wing_dihedral=3.499146 wing_incidence=4.999268 // was 2.999268 wing_twist=-1.994019 oswald_efficiency_factor=.448140 // was 1.064814 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=1.229000 wing_pos_apex_vert=0.000000 htail_area=16.000000 htail_span=7.916667 htail_pos_lon=-16.083333 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=16.000000 vtail_span=4.560702 vtail_sweep=0.000000 vtail_pos_lon=-14.750000 vtail_pos_vert=4.166667 elevator_area=15.000000 aileron_area=11.740000 rudder_area=6.000000 elevator_up_limit=30.0 // was 25.000447 elevator_down_limit=18.998903 aileron_up_limit=17.996227 aileron_down_limit=13.000035 rudder_limit=20.995472 elevator_trim_limit=10.0 // was 19.497754 spoiler_limit=70 spoilerons_available=1 // was 0 aileron_to_spoileron_gain=0.0005 // was 0 min_ailerons_for_spoilerons=0.005 // was 0 min_flaps_for_spoilerons=0.005 // was 0 [GeneralEngineData] engine_type=0 Engine.0=6.000000,0.000000,0.000000 fuel_flow_scalar=1.00 min_throttle_limit=0.000000 [piston_engine] power_scalar=1.0 //Piston power scalar cylinder_displacement=100.300000 compression_ratio=6.0 number_of_cylinders=6 // was 2 max_rated_rpm=3500 // was 2700 max_rated_hp=200 // was 115 fuel_metering_type=1 cooling_type=0 // was 1 normalized_starter_torque=0.3 turbocharged=0 max_design_mp=0.0 min_design_mp=0.0 critical_altitude=0.0 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] thrust_scalar=1.0 // Propeller thrust scalar propeller_type=2 // was 0 propeller_diameter=8.000 // was 5.433000 propeller_blades=2 propeller_moi=20.50000 // was 3.350000 beta_max=29.800000 beta_min=4.000000 // was 17.000000 min_gov_rpm=50.000000 // was 700.000000 prop_tc=0.4 // was 0.004000 gear_reduction_ratio=1.10 // was 1.0 fixed_pitch_beta=0 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=1 prop_auto_feathering_available=0 min_rpm_for_feather=0 beta_feather=90.0 power_absorbed_cf=0.0 defeathering_accumulators_available=0 // was 1 prop_reverse_available=1 // was 0 minimum_on_ground_beta=2.0 // was 0 minimum_reverse_beta=0.000000 [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [autopilot] default_bank_mode=0 default_pitch_mode=0 autopilot_available=1 flight_director_available=0 default_vertical_speed=500.000000 // was 700 autothrottle_available=0 pitch_takeoff_ga=-5.00 // was 8.0 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=1,0 [brakes] toe_brakes_scale=1.000000 parking_brake=1 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [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 = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 3250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5# ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 750 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1# crash_magnitude1 = 10000 crash_direction1 = 1000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 // //Default FF Code installed by FFUtil 18:32:18 04-23-2004
