[General] atc_type=MERLIN editable=1 performance=Country Of Origin: UK/Italy \nDesignation: ASW helicopter \nAircraft Crew: One or two pilots, Observer and Aircrewman \nWeapon Capacity: Mix of 4 Stingray Torpedoes or Depth Charges \n\nAircraft Dimensions: \n Length: 74 ft 10 in (12.8 m) \n Rotor Size: 61 ft (12.8 m) \n Height: 21 ft 9 in (3.5 m) \n\nAircraft Weights: \n Empty: 20,388 lb \n Max T\/O: 32,188 lb \n\nAircraft Performance: \n Cruising Speed: 150knots \n Range: 610 nm/5h45min \n Powerplant: Three RTM322 turboshafts \n Power: 2,312 shp \n\n\n atc_model=Merlin [fltsim.0] title=CH149 Cormorant sim=Merlin model= panel= sound= texture=CH149 kb_checklists= kb_reference= prop_anim_ratio=-1.76 atc_id_color=0xc6eff7ff atc_id=904 atc_model= ui_manufacturer=Westland ui_type=CH149 ui_variation=Cormorant description=CH-149 Cormorant 904, 442 Squadron Comox BC. Model by Philip Chandler; Textures by Vern Opperman atc_heavy=0 atc_airline=Air Force atc_flight_number=904 [turboprop_engine] power_scalar=50.0 [propeller] thrust_scalar=9.0 propeller_type=1 propeller_diameter=6.883000 propeller_blades=2 propeller_moi=5.706520 beta_max=0.000000 beta_min=15.000000 min_gov_rpm=0.000000 prop_tc=0.100000 gear_reduction_ratio=1.000000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 //Dampers are set to our mormal standards of flight [ground_reaction] //main_gear_static_compression=5.2 // (feet), The distance the main gear strut is compressed when at rest on the ground center_gear_static_compression=5.2 // (feet), The distance the center gear strut is compressed when at rest on the ground //main_gear_damping_ratio=0.7 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped center_gear_damping_ratio=1.0 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped [WEIGHT_AND_BALANCE] reference_datum_position=0.000, 0.000, 0.000 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=1000.000 empty_weight_roll_MOI=4000.000 empty_weight_pitch_MOI=6000.000 empty_weight_yaw_MOI=10000.000 empty_weight_coupled_MOI=1200.000 max_gross_weight=8000.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [fuel] Center1=0.000, 0.000, -7.000, 91.000, 10.000 LeftMain=5.000, 0.000, -7.000, 91.000, 10.000 RightMain=-5.000, 0.000, -7.000, 91.000, 10.000 fuel_type=2.000 number_of_tank_selectors=1 electric_pump=0 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 gear_motor=0, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=1, 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 //1 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, 14.500, 0.000, -11.100, 2200.000, 0.000, 0.400, 45.000, 0.750, 0.750, 0.850, 2.000, 2.000, 0.000, 0.000, 0.000 point.1=1.000, -6.500, -7.110, -11.100, 2200.000, 1.000, 0.500, 0.000, 0.750, 0.750, 0.850, 2.000, 2.000, 0.000, 0.000, 0.000 point.2=1.000, -6.500, 7.110, -11.100, 2200.000, 2.000, 0.500, 0.000, 0.750, 0.750, 0.850, 2.000, 2.000, 0.000, 0.000, 0.000 point.3=2.000, 19.5, 0.000, -7.5, 2200, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.4=2.000, -12, 0.000, -8.5, 2200, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.5=2.000, -37, 0.000, -2, 2200, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.6=2.000, -10, -8.000, -7.5, 2200, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.7=2.000, -10, 8.000, -7.5, 2200, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 static_cg_height=10.5 static_pitch=0.000 gear_system_type=0 [Views] eyepoint=14, 1.5, -1 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=0, 0 Nav.1=1, 1, 1 Nav.2=0, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [keyboard_response] elevator=100.000, 180.000 aileron=200.000, 1000.000 rudder=200.000, 1000.000 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -5.5, -8, -7.0, fx_navred , light.1=3, -5.5, 8, -7.0, fx_navgre , //light.2=3, -29, 0.4, 1.5, fx_navwhi , light.3=1, 2.35, 0.0, -8.5, fx_beacon , light.4=2, -36.5, -2.0, 7.75, fx_beacon , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks [GeneralEngineData] engine_type=3 Engine.0=5.000, 0.000, 5.300 Engine.1=5.000, 0.000, 5.300 // added to make tailrotor turn fuel_flow_scalar=1.69 min_throttle_limit=0.000000 [exits] number_of_exits=1 exit_rate.0=0.2 [autopilot] autopilot_available=0 flight_director_available=0 [direction_indicators] direction_indicator.0=3,0 [brakes] toe_brakes_scale=1.000031 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 [Reference Speeds] cruise_speed=0.000000 max_indicated_speed=190.000000 [hydraulic_system] normal_pressure=0.000000 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
