[fltsim.0] title=Robinson R22 Helijet sim=Robinson_R22 model= panel= sound= texture=helijet kb_checklists=Robinson_R22_check kb_reference=Robinson_R22_ref prop_anim_ratio=-1.76 atc_id_color=0xc6eff7ff atc_id=C-GKWX ui_manufacturer=Robinson ui_type="R22 Beta II" ui_variation=Helijet description="Performance, price, and low operating cost have made the two-seat Robinson R22 Beta II among the most popular helicopters in the world. It's also a popular training helicopter for the same reasons. A fun aircraft to fly, the R22 has one of the best overall records of reliability for all helicopters. " atc_parking_types=RAMP atc_parking_codes=HCP [General] atc_type=Robinson atc_model=R22 performance="Maximum Speed\n102 kts 189 km/hr\n\nCruise Speed\n96 kts 178 km/hr\n\nEngine\nLycoming O-360 or o-360, 150 BHP\n\nMaximum Range\n200 nm 371 km\n\nService Ceiling\n14,000 ft 4,267 m\n\nHovering Ceiling\n9,450 ft 2,880 m\n\nFuel Capacity\n29.7 gal 112 L\n\nEmpty Weight\n830 lb 376 kg\n\nMax Gross Weight\n1,370 lb 621 kg\n\nLength\n28.75 ft 8.75 m\n\nRotor Span\n25.2 ft 7.68 m\n\nHeight\n9 ft 2.74 m\n\nSeating\n2" editable=0 [WEIGHT_AND_BALANCE] max_gross_weight=1370 // (pounds) empty_weight=862.4 // (pounds) reference_datum_position=8.33, 0.0, 0.0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-8.73, 0.0, 0.0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0="160, -6.6, 0.89, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1="160, -6.6, -0.78, 0.0, Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=6000 empty_weight_roll_MOI=4000 empty_weight_yaw_MOI=10000 empty_weight_coupled_MOI=0 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 5 , 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 2 , 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 //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=3, -3.74, -3.13, -4.00, 1600, 0, 0, 0.0, 0.39, 2.5, 0.82, 0.0, 0.0, 7, 0.0, 0.0 point.1=3, -3.74, 3.13, -4.00, 1600, 0, 0, 0.0, 0.39, 2.5, 0.82, 0.0, 0.0, 7, 0.0, 0.0 point.2=3, -10.00, -3.13, -3.70, 1600, 0, 0, 0.0, 0.28, 2.5, 0.82, 0.0, 0.0, 7, 0.0, 0.0 point.3=3, -10.00, 3.13, -3.70, 1600, 0, 0, 0.0, 0.28, 2.5, 0.82, 0.0, 0.0, 7, 0.0, 0.0 point.4=2, -8.50, -11.80, 5.30, 100, 0, 0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5, 0.0, 0.0 point.5=2, -8.50, 11.80, 5.30, 100, 0, 0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6, 0.0, 0.0 point.6=2, 3.00, 0.00, 5.30, 100, 0, 0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4, 0.0, 0.0 point.7=2, -23.00, 0.00, -0.60, 300, 0, 0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9, 0.0, 0.0 static_pitch=0.2 static_cg_height=3.58 [brakes] parking_brake=0 //Parking brake available toe_brakes_scale=0.0 //Brake scalar [hydraulic_system] normal_pressure=0.0 //PSI [Views] eyepoint=-7.453, .718, 1.358 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 8, -8.5, 0.0, -8.4, fx_nickspropdust_dirt_h light.1 = 9, -8.5, 0.0, -8.4, fx_nickspropdust_gravsnd_h light.2 = 6, -8.5, 0.0, -8.4, fx_nickspropdust_watrsno_h light.3 = 3, -5.60, -1.88, -1.60, fx_navred , light.4 = 3, -5.60, 1.88, -1.60, fx_navgre , light.5 = 3, -23.39, 0.40, 1.95, fx_navwhi , light.6 = 1, -18.90, 0.04, 2.58, fx_beacon , light.7 = 5, -2.85, 0.20, -1.65, fx_landing , light.8 = 5, -2.85, -0.20, -1.65, fx_landing , light.9 = 4, -7.75, 0.30, 1.50, fx_vclighth , [SMOKESYSTEM] smoke.0 = 0.00, -8.5, 0.00, fx_nicks_watrsnoland_h [EFFECTS] wake=fx_wake water=fx_nicks_tchwater_h dirt=fx_nicks_tchdirt concrete=fx_sparks landrotorwash=fx_nicks_rtr_dirt_h waterrotorwash=fx_nicks_rtr_wtr_h startup=fx_engstrt [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. //NOTE: These map to cyclic (fore/aft), cyclic (left/right), and anti-torque elevator=100, 180 aileron=200, 1000 rudder=200, 1000 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type=4 direction_indicator.0=3,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0=1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [fuel] LeftMain=-8.85, -0.5, 0.0, 19.2, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-8.85, 0.5, 0.0, 10.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [GeneralEngineData] engine_type=0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-8.5, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.0 //Fuel flow scalar min_throttle_limit=0.0; //Minimum percent throttle. Generally negative for turbine reverser [piston_engine] power_scalar=1.0 //Piston power scalar cylinder_displacement=90.0 //Cubic inches per cylinder compression_ratio=8.5 //Compression ratio number_of_cylinders=4 //Number of cylinders max_rated_rpm=2700 //Max rated RPM max_rated_hp=180 //Max rated HP fuel_metering_type=1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque=0.3 //Starter torque factor turbocharged=0 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp=0 //Max design manifold pressure, (inHg) min_design_mp=0 //Min design manifold pressure, (inHg) critical_altitude=0 //Altitude to which the turbocharger will provide max design manifold pressure (feet) emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power emergency_boost_mp_offset=0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset=0 //Multiplier on manifold pressure due to emergency boost fuel_air_auto_mixture=0 //Automixture available? 0=FALSE, 1=TRUE auto_ignition=0 //Auto-Ignition available? 0=FALSE, 1=TRUE max_rpm_mechanical_efficiency_scalar=1.0 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction idle_rpm_friction_scalar=1.0 //Scalar on idle RPM friction [Reference Speeds] cruise_speed=90.0 //Knots True (KTAS) max_indicated_speed=102 //Red line (KIAS) [autopilot] autopilot_available=0 flight_director_available=0 [yaw_string] yaw_string_available=1 [Helicopter] reference_length=21.58 reference_frontal_area=17.7 reference_side_area=44.5 side_aero_center=-12.5 right_trim_scalar=1.0 correlator_available=1 governed_pct_rpm_ref=1.04 governor_pid=0.4, 0, 0.1, 0, 0.2 rotor_brake_scalar=1.0 torque_scalar=1.0 cyclic_roll_control_scalar=1.0 cyclic_pitch_control_scalar=1.0 pedal_control_scalar=1.0 collective_on_rotor_torque_scalar=1.0 [fuselage_aerodynamics] drag_force_cf=0.55 side_drag_force_cf=10.0 pitch_damp_cf=-2.0 roll_damp_cf=-2.0 yaw_damp_cf=-0.1 yaw_stability_cf=0.27 [MainRotor] Position=-8.5, 0, 4.91 //Longitudinal, Lateral, Vertical feet from datum Radius=12.583 //feet max_disc_angle=5.0 RatedRpm=510 Number_of_blades=2 Weight_per_blade=26.0 Weight_to_moi_factor=0.58 inflow_vel_reference=34.0 [SecondaryRotor] Position=-22.8, -0.74, 1.8 //Longitudinal, Lateral, Vertical feet from datum TailRotor=1 Radius=1.75 //feet
