[fltsim.0] title=Curtiss P-40M Noela sim=P-40 model=M panel= sound= texture=Noela checklists=P-40ncf_CHECK ui_manufacturer=Curtiss description=Curtiss P-40 M CURTISS P-40M SV-G "Noela". This aircraft served with 76 Squadron and was flown by Bob Hunter. Nicknamed "Noela", it featured nose art showing a kangaroo lobbing bombs, and the phrase "Semper In Excreta - Section 40 Special". [fltsim.1] title=Curtiss P-40N Cleopatra III sim=P-40 model=N panel= sound= texture=CLEO checklists=P-40_CHECK ui_manufacturer=Curtiss description=A29-629 was nicknamed "Cleopatra III" and flown by Wg Cdr Geoff Atherton of 80 Squadron. Atherton had previously served with distinction in the Port Moresby and Milne Bay campaigns while part of 75 Squadron - this was his third Kittyhawk. The aircraft survived the war and was struck off charge at Oakey, Queensland in January 1946. [General] performance=Model: Curtiss P-40M-N \nEngine: Allison V-1710-19 F4R\nMIL Power: 1,325 horsepower\nWEP Power: 1,550 horsepower\nTop speed @ 15,000 ft: 362 mph TAS (MIL)\nTop speed @ 15,000 ft: 374 mph TAS (WEP)\nTop speed @ sea level: 320 mph TAS (MIL)\nTop speed @ sea level: 332 mph TAS (WEP)\nInitial climb: 2700 fpm (MIL)\nArmament: (6) .50 caliber machine guns\nRange: 1,343 miles with maximum fuel at optimal cruise\nEmpty weight: 6,977 lbs.\nCombat weight: 8,093 lbs\nGMAX mdl by AF Scrub Aug 2012 Category=airplane [WEIGHT_AND_BALANCE] empty_weight=6400 // (pounds) reference_datum_position=0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=170, -3.8, 0.0, 4.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 6181.10 empty_weight_roll_MOI = 4396.69 empty_weight_yaw_MOI = 8475.84 empty_weight_coupled_MOI=0.000000 max_gross_weight=9855.000000 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 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=1.0 [piston_engine] power_scalar=1.0 cylinder_displacement=142.500000 compression_ratio=6.650000 number_of_cylinders=12 max_rated_rpm=3000.000000 max_rated_hp=1240.000000 fuel_metering_type=0 cooling_type=1 normalized_starter_torque=0.035000 turbocharged=1 max_design_mp=53.999999 min_design_mp=1.000000 critical_altitude=26000.000000 emergency_boost_type=1 emergency_boost_mp_offset=4.100000 emergency_boost_gain_offset=0.500000 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 ;Percent per second propeller_type=0 propeller_diameter=11.200000 propeller_blades=4 propeller_moi=58.100000 beta_max=65.000000 beta_min=13.000000 min_gov_rpm=1800.000000 prop_tc=0.010000 gear_reduction_ratio=2.000000 fixed_pitch_beta=0.000000 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=0.000000 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [exits] number_of_exits=1 exit_rate.0=0.4 ;Percent per second [electrical] max_battery_voltage=24.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=60.0 [contact_points] //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 (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) point.0=1.000, -15.710, 0.000, -3.030, 3200.000, 0.000, 0.380, 45.000, 0.450, 2.500, 0.900, 1.000, 4.000, 0.000, 200.000, 398.935 point.1=1.000, 2.290, -4.420, -7.800, 2200.000, 1.000, 1.350, 0.000, 0.640, 2.500, 0.860, 5.500, 6.500, 2.000, 200.000, 427.429 point.2=1.000, 2.290, 4.420, -7.800, 2200.000, 2.000, 1.350, 0.000, 0.640, 2.500, 0.860, 5.500, 5.000, 3.000, 200.000, 427.429 point.3=2.000, 1.079, -19.300, 0.000, 1200.000, 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, 1.079, 19.300, 0.000, 1200.000, 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, -18.250, 0.000, -0.910, 2400.000, 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, 5.410, 0.000, -6.200, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_cg_height=6.750 static_pitch=14.300 gear_system_type=1 [Views] eyepoint=-2.750,0.0,1.60 [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.125 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees, KIAS flaps-position.1=16, // degrees, KIAS flaps-position.2=32, // degrees, KIAS flaps-position.3=64, // degrees, KIAS flaps-position.4=80, damaging-speed=190 // KIAS blowout-speed=250 // KIAS [LIGHTS] panel=0.00, 0.45, -2.00, fx_vclight [fuel] Center1=-3.900000,0.000000,-1.600000,55.600000,0.000000 LeftMain=-0.350000,-1.200000,-1.200000,45.600000,0.000000 RightMain=-0.350000,1.200000,-1.200000,45.600000,0.000000 External1=2.300000,0.000000,-4.400000,150.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=236.000000 wing_span=37.333333 wing_root_chord=6.333333 wing_dihedral=4.400024 wing_incidence=0.999756 wing_twist=0.000000 oswald_efficiency_factor=0.595553 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=24.000000 htail_span=11.000000 htail_pos_lon=-18.833333 htail_pos_vert=0.000000 htail_incidence=-1.801001 htail_sweep=0.000000 vtail_area=15.000000 vtail_span=4.415880 vtail_sweep=0.000000 vtail_pos_lon=-18.833333 vtail_pos_vert=0.583333 elevator_area=14.000000 aileron_area=17.400000 rudder_area=13.060000 elevator_up_limit=25.427867 elevator_down_limit=23.708994 aileron_up_limit=21.497376 aileron_down_limit=20.345731 rudder_limit=28.997394 elevator_trim_limit=19.996227 spoiler_limit=0.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 auto_spoiler_available=0 positive_g_limit_flaps_up=10.000000 positive_g_limit_flaps_down=10.000000 negative_g_limit_flaps_up=-10.000000 negative_g_limit_flaps_down=-10.000000 [brakes] toe_brakes_scale=1.000000 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 [GeneralEngineData] engine_type=0 Engine.0=8.000000,0.000000,0.000000 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed=70.000000 full_flaps_stall_speed=56.000000 cruise_speed=250.000000 max_indicated_speed=760.500000 [keyboard_response] elevator=350.000000,500.000000 aileron=450.000000,1000.000000 rudder=200.000000,1000.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 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 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 normal_pressure=6.930556 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0 [General] Category=airplane [pitot_static] pitot_heat=1.000000 [vacuum_system] max_pressure=5.000000 vacuum_type=1 electric_backup_pressure=0.000000 engine_map=1,1,1,1 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=0.000000 [deice_system] structural_deice_type=0
