//PREMIER AIRCRAFT DESIGN //Mitsubishi MU-2K //Copyright 2008 //Design by J.P.Brisard //Textures and FD by Bob May //Technical assistance by Joe Zerilli //Flight tuning by Danny "Chief" Crance //Saab Technologies paint by Marcel Gisel [fltsim.0] title=mu2k_fix12lipchrome sim=mu2s model= panel=mu2mx sound=0 texture=saabc kb_checklists=MU-2_check kb_reference=MU-2_ref atc_id=SE-GHD ui_manufacturer=Mitsubishi ui_type="MU2 short" ui_variation=Saab Technologies description=The Mitsubishi MU-2 is one of postwar Japan's most successful aircraft. It is a high-wing, pressurized twin-engine turboprop. This MU-2K has a 3 blade propeller and is operated by Saab Technologies ( formerly Saab Nyge Aero) in support of the Swedish armed services. [General] atc_type=MITSU atc_model=MU2 editable=1 performance=Max speed: 330 mph\nRange: 1200 nm\nCeiling: 33,000\nMax weight: 8930\nPassenger: 4 + 2 crew Category=airplane [WEIGHT_AND_BALANCE] max_gross_weight = 8930.00 empty_weight = 5430.00 reference_datum_position = 0.00, 0.00, 0.00 empty_weight_CG_position = 0.00, 0.00, 0.00 station_load.0 = "170, 1.7, -1.75, -3.0, Pilot" //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "170, 1.7, 1.75, -3.0, Front Passenger" //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = "350, -3.3, 0.0, -3.0, Payload" //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) max_number_of_stations =20 ;Moments of Inertia empty_weight_pitch_MOI = 80000.00 empty_weight_roll_MOI = 36000.00 empty_weight_yaw_MOI = 116000.00 empty_weight_coupled_MOI= 0.00 CG_forward_limit= 0.00 CG_aft_limit= 1.00 [flight_tuning] parasite_drag_scalar =1.10 induced_drag_scalar =1.10 elevator_effectiveness =0.85 aileron_effectiveness =0.90 rudder_effectiveness =1.00 pitch_stability =3.50 roll_stability =2.00 yaw_stability =1.50 elevator_trim_effectiveness =1.05 aileron_trim_effectiveness =0.95 rudder_trim_effectiveness =1.20 [GeneralEngineData] engine_type = 5 Engine.0 = 3.50, -9.60, 0.60 Engine.1 = 3.50, 9.60, 0.60 fuel_flow_scalar = 0.50 min_throttle_limit=-0.250 [propeller] thrust_scalar=1.000 propeller_type=0 propeller_diameter=8.6 propeller_blades=3 propeller_moi=24.000 beta_max=90.000 beta_min=6.000 min_gov_rpm=1114.000 prop_tc=0.004 gear_reduction_ratio=17.6 fixed_pitch_beta=0.000 low_speed_theory_limit=150.00//80.00 prop_sync_available=1 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=1 min_rpm_for_feather=1000.000 beta_feather=90.000 power_absorbed_cf=0.900 defeathering_accumulators_available=1 prop_reverse_available=1.000 minimum_on_ground_beta=1.000 minimum_reverse_beta=-14.000 [TurbineEngineData] fuel_flow_gain=0.011 inlet_area=1.000 rated_N2_rpm=41730.000 static_thrust=150.000 afterburner_available=0 [turboprop_engine] power_scalar=1.000 maximum_torque=3200.000 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=0.800 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=0.800 [Reference Speeds] flaps_up_stall_speed = 82.00 full_flaps_stall_speed = 75.00 cruise_speed = 240.00 //knots indicated (IAS) at 20,000 ft. normal_cruise_speed = 240.00 max_indicated_speed =300.00 max_mach=0.579980 [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, 10, 17.0 avionics = 1, 5 , 17.0 pitot_heat = 0, 2 , 17.0 additional_system = 0, 20, 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 [contact_points] //Classes...What type of point 0=Unused or Ignore // 1=Wheel // 2=Scrape point // 4=Float // 5=Float Rudder //0 Class //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=1.000, 8.329, 0.000, -6.20, 1281, 0, 0.75, 39.9, 0.296, 1.5, 0.9516, 10.0, 10.0, 0, 184.0, 184.0 point.1=1.000, -6.41, -7.400, -6.58, 1874, 1, 0.75, 0.0, 0.642, 2.5, 0.8152, 14.0, 12.0, 0, 184.0, 184.0 point.2=1.000, -6.41, 7.400, -6.58, 1874, 2, 0.75, 0.0, 0.642, 2.5, 0.8152, 14.0, 12.0, 0, 184.0, 184.0 point.3=2.000,-2.200,-29.300,3.200,2360.907127,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,5.000,0.000,0.000 point.4=2.000,-2.200,29.300,3.200,2360.907127,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,6.000,0.000,0.000 point.5=2.000,-35.000,0.000,11.000,2360.907127,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,9.000,0.000,0.000 point.6=2.000,23.600,-0.000,-0.500,1574.803150,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,4.000,0.000,0.000 point.7=5.000,23.600,-0.000,-0.500,1574.803150,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,4.000,0.000,0.000 static_pitch =0 static_cg_height = 3.0 //5.9 gear_system_type=1 //Hydraulic [Views] eyepoint=2.122,-0.914,-1.1 // 0.681 [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 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. elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, -4.5 , -19.66, 0.1,fx_navred , light.1 = 3, -4.5, 19.66, 0.1, fx_navgre , light.2 = 3, -23.4, 0.00, 7.30, fx_navwhi , light.3 = 2, -4.9, -19.66, 0.10, fx_strobe , light.4 = 2, -4.9, 19.66, 0.10, fx_strobe , light.5 = 1, -20.92, 0.00, 7.3,fx_beaconh , light.6 = 1,-10.530, 0.00, -4.63,fx_beaconh , light.7 = 4, 3.0, -1.00, -2.10, fx_vclightwhi , light.8 = 4, 3.00, 1.00, -2.10, fx_vclightwhi , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] Center1 = 0.00,0.0, -3.0, 160.00, 6.00 LeftAux = -3.00, -15.00, -1.50, 15.0, 0.00 RightAux = -3.00, 15.00, -1.50, 15.0, 0.00 Lefttip=0.0,-20.0,0.0,93,0.0 Righttip=0.0,20.0,0.0,93,0.0 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=1 [airplane_geometry] wing_area = 178.00 wing_span = 39.2 wing_root_chord = 6.60 wing_dihedral = 3.00 wing_incidence = 2.00 wing_twist = -1.50 oswald_efficiency_factor= 0.70 wing_winglets_flag = 1 wing_sweep = 3.00 wing_pos_apex_lon = 2.00 wing_pos_apex_vert = -1.00 htail_area = 76.00 htail_span = 18.20 htail_pos_lon = -27.50 htail_pos_vert = 11.00 htail_incidence = -1.60 htail_sweep = 20.00 vtail_area = 50.00 vtail_span = 6.50 vtail_sweep = 35.00 vtail_pos_lon = -23.50 vtail_pos_vert = 4.50 elevator_area = 14.00 aileron_area = 5.00//13.0 rudder_area = 17.00 elevator_up_limit = 17.00 elevator_down_limit = 15.50 aileron_up_limit = 10.0//18.00 aileron_down_limit = 10.0//18.00 rudder_limit = 30.00 elevator_trim_limit = 15.00 spoiler_limit = 00.00 spoilerons_available = 0 aileron_to_spoileron_gain = 0.00 min_ailerons_for_spoilerons = 0.00 min_flaps_for_spoilerons = 0.00 auto_spoiler_available=0 spoiler_extension_time=0.000000 positive_g_limit_flaps_up=3.000000 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-2.000000 negative_g_limit_flaps_down=-2.000000 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1800.0 autothrottle_available= 0 pitch_takeoff_ga=8.00 max_pitch=10.00 max_pitch_acceleration=1.00 max_pitch_velocity_lo_alt=2.00 max_pitch_velocity_hi_alt=1.50 max_pitch_velocity_lo_alt_breakpoint=20000.00 max_pitch_velocity_hi_alt_breakpoint=28000.00 max_bank=25.00 max_bank_acceleration=1.80 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.250 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.520 gs_integrator_control=0.260 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain=0.00 [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=08900 ; 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 [Flaps.0] type= 1 span-outboard= 0.30 extending-time= 12.00 system_type= 0 damaging-speed= 250.00 blowout-speed= 300.00 flaps-position.0= 0.00, 0.00 flaps-position.1= 5.00, 0.00 flaps-position.2=20.00, 0.00 flaps-position.3=40.00, 0.00 drag_scalar=1.150 lift_scalar=1.00 pitch_scalar= 0.900 [Flaps.1] type= 1 span-outboard= 0.30 extending-time= 12.00 system_type= 0 damaging-speed= 250.00 blowout-speed= 300.00 flaps-position.0= 0.00, 0.00 flaps-position.1= 5.00, 0.00 flaps-position.2=20.00, 0.00 flaps-position.3=40.00, 0.00 drag_scalar=1.150 lift_scalar=1.00 pitch_scalar= 0.900 [brakes] toe_brakes_scale=1.20 parking_brake= 1.80 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=30.022988 flap_limit_idle=15.011494 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.00 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [exits] number_of_exits=2 exit_rate.0=0.2 ;Percent per second exit_rate.1=0.2 [pitot_static] pitot_heat=1.000000 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=2