[fltsim.0] title = De Havilland Mosquito NFII sim = Mosquito NFII model = panel = sound = texture = panel_alias = sound_alias = kb_checklists = kb_reference = visual_damage=1 atc_id = GNFII atc_id_color = atc_parking_types =MIL_COMBAT atc_parking_codes =DH98 Mosquito ui_manufacturer = De Havilland ui_type = Mosquito NFII ui_variation = 23 Sqdn, 1942 description = RR Merlin 23 - 1390hp @ + 12lbs Boost, 3000 rpm @ Take Off, 1480hp @ 16 lbs Boost, 3000rpm @ 12250ft (Climbing Boost + 9lbs @ 2850rpm [General] atc_type = DeHavilland atc_model = Mosquito editable = 1 performance = + Empty Weight: 14480 lbs + Max Power: 1480 Hp + Maneuver speed: 292 mph @ 7.5 g + Max speed: 370 mph @ 22000 ft + Max speed at sea-level: 317 mph + Climb rate: 3000 ft/min @ 170 mph Flight Dynamics By: Paul Bradford BRADBURGER FD Build 2 - 4/28/04 09:20 PM Flight Dynamics Workbook V2.84.63 [pitot_static] vertical_speed_time_constant = 0.49 [WEIGHT_AND_BALANCE] max_gross_weight = 19200 empty_weight = 14120 reference_datum_position = 0, 0, 0 empty_weight_CG_position = -0.077122, 0, 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 2 station_load.0 = 180, 3.58, -0.81, -0.16, Pilot station_load.1 = 180, 2.47, 0.89, -0.27, Navigator empty_weight_pitch_MOI = 22994 empty_weight_roll_MOI = 24299 empty_weight_yaw_MOI = 44259 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1 parasite_drag_scalar = 1 induced_drag_scalar = 1 elevator_effectiveness = 1 aileron_effectiveness = 1 rudder_effectiveness = 1 pitch_stability = 1 roll_stability = 1 yaw_stability = 1 elevator_trim_effectiveness = 1 aileron_trim_effectiveness = 1 rudder_trim_effectiveness = 1 hi_alpha_on_roll = 1 hi_alpha_on_yaw = 1 p_factor_on_yaw = 1 torque_on_roll = 1 gyro_precession_on_roll = 1 gyro_precession_on_yaw = 1 [GeneralEngineData] engine_type = 0 Engine.0 = 7.87, -8.27, -0.46 Engine.1 = 7.87, 8.27, -0.46 fuel_flow_scalar = 1 min_throttle_limit = 0 max_contrail_temperature=-28 [piston_engine] power_scalar = 1 cylinder_displacement = 137.416666666667 compression_ratio = 6 number_of_cylinders = 12 max_rated_rpm = 3000 max_rated_hp = 1390 fuel_metering_type = 2 cooling_type = 1 normalized_starter_torque = 0.035 turbocharged = 1 max_design_mp = 54.34 min_design_mp = 11 critical_altitude = 22000 emergency_boost_type = 3 emergency_boost_mp_offset = 2.17 emergency_boost_gain_offset = 0.174490600022515 fuel_air_auto_mixture = 1 auto_ignition = 0 emergency_boost_duration = 300 max_rpm_mechanical_efficiency_scalar = 1 idle_rpm_mechanical_efficiency_scalar = 1 max_rpm_friction_scalar = 1 idle_rpm_friction_scalar = 1 [propeller] thrust_scalar = 1 propeller_type = 0 propeller_diameter = 12 propeller_blades = 3 propeller_moi = 56.6 beta_max = 65 beta_min = 15 min_gov_rpm = 450 prop_tc = 0.01 gear_reduction_ratio = 2.096 fixed_pitch_beta = 20 low_speed_theory_limit = 80 prop_sync_available = 0 prop_deice_available = 0 prop_feathering_available = 1 prop_auto_feathering_available = 0 feathering_switches = 1 min_rpm_for_feather = 700 beta_feather = 88.5 power_absorbed_cf = 0.9 defeathering_accumulators_available = 0 prop_reverse_available = 0 minimum_on_ground_beta = 1 minimum_reverse_beta = -14 rotation = 1, 1 [contact_points] max_number_of_points = 12 point.0 = 1, -26.0511, 0, -2.83, 6153.30513, 0, 0.75, 30, 0.25, 2.5, 0.72631, 3, 3.9, 0, 157.52, 184.8 point.1 = 1, 2.3176, -8.4, -9.67, 6153.30513, 1, 2, 0, 1.15, 2.5, 0.72651, 8.9, 6.8, 2, 157.52, 184.8 point.2 = 1, 2.3176, 8.4, -9.67, 6153.30513, 2, 2, 0, 1.15, 2.5, 0.72651, 9.6, 8.2, 3, 157.52, 184.8 point.3 = 2, -25.2894, 0, 8.89, 3500, 0, 0, 0, 0, 0, 0, 0, 0, 9 point.4 = 2, 10.6331, 0, -0.8543, 5000, 0, 0, 0, 0, 0, 0, 0, 0, 4 point.5 = 2, 0.1091, -27.121, 1.1497, 4000, 0, 0, 0, 0, 0, 0, 0, 0, 5 point.6 = 2, 0.1091, 27.121, 1.1497, 4000, 0, 0, 0, 0, 0, 0, 0, 0, 6 point.7 = 2, -30.4069, 0, 0.9484, 2500, 0, 0, 0, 0, 0, 0, 0, 0, 9 point.8 = 2, -27.8842, 0, 0.1496, 2650, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 point.9 = 2, 2.4845, 0, -3.8415, 2850, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 point.10 = 2, 8.1429, -8.27, -4.15, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0 point.11 = 2, 8.1431, 8.4, -4.13, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 7 point.12 = 2, -7.3435, 0, -3.301, 2800, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0 static_pitch= 12.5 static_cg_height= 7.9 gear_system_type = 1 tailwheel_lock = 0 [Views] eyepoint= 3.24, -0.85, 2.15 [folding_wings] wing_fold_system_type = 4 fold_rates = 0.12, 0.13 [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 4 flaps-position.0 = 0 flaps-position.1 = 10, 182 flaps-position.2 = 15, 173 flaps-position.3 = 25, 143 flaps-position.4 = 45, 133 damaging-speed = 186 blowout-speed = 208 system_type = 1 lift_scalar = 1 drag_scalar = 1 pitch_scalar = 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 30 max_generator_alternator_amps = 60 engine_generator_map= 0,1 electric_always_available = 0 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 pitot_heat = 2, 2, 17 additional_system = 3, 20, 17 marker_beacon = 2, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 4, 5, 17 starter1 = 0, 20, 17 starter2 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 standby_vacuum = 2, 15, 17 fuel_transfer_pump = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 [SMOKESYSTEM] //(feet) vertical, longitudinal, lateral, SMOKE.0=0.00, -3.00, -27.00, FX_HB_CONTRAIL_S, SMOKE.1=0.00, -3.00, 27.00, FX_HB_CONTRAIL_S, [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi, 7=recog, 8=wing, 9=logo, // class long lat vert effect light.0=3, 0.900, -26.650, 1.100, fx_HB_NAVREDSTROBE, light.1=3, 0.900, 26.650, 1.100, fx_HB_NAVGRESTROBE, light.2=3, -25.000, 0.000, 8.850, fx_beaconh, light.3=3, -30.440, 0.000, 1.000, fx_navwhi, light.4=4, 4.500, -0.800, 0.900, fx_vclight //pilot light.5=4, 3.000, -0.800, 0.900, fx_vclight //co-pilot light.6=6, 3.825, -10.132, -1.100, FX_HB_FS2002_HE111_EXH, //port outer light.7=6, 3.825, -6.400, -1.100, FX_HB_FS2002_HE111_EXH, //port inner light.8=6, 3.825, 10.132, -1.100, FX_HB_FS2002_HE111_EXH, //starb outer light.9=6, 3.825, 6.400, -1.100, FX_HB_FS2002_HE111_EXH, //starb inner light.10=5, -0.200, -14.355, -0.850, fx_landing, //port landing light light.11=5, -0.200, 14.355, -0.850, fx_landing, //starb landing light [Radios] // availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 1 Transponder.1 = 1 [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [direction_indicators] direction_indicator.0 = 1, 0 [exits] number_of_exits = 1 exit_rate.0 = 0.5 [EFFECTS] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 [autopilot] autopilot_available = 1 flight_director_available = 0 default_vertical_speed = 1000 autothrottle_available = 0 autothrottle_arming_required = 0 autothrottle_max_rpm = 90 autothrottle_takeoff_ga = 1 pitch_takeoff_ga = 8 max_pitch_velocity_hi_alt = 1.5 max_pitch_velocity_lo_alt_breakpoint = 20000 max_pitch_velocity_hi_alt_breakpoint = 28000 max_pitch = 10 max_pitch_acceleration = 1 max_pitch_velocity_lo_alt = 2 max_bank= 25 max_bank_acceleration = 1.8 max_bank_velocity = 3 max_throttle_rate = 0.1 nav_proportional_control = 9 nav_integrator_control = 0.25 nav_derivative_control = 0 nav_integrator_boundary = 2.5 nav_derivative_boundary = 0 gs_proportional_control = 9.52 gs_integrator_control = 0.26 gs_derivative_control = 0 gs_integrator_boundary = 0.7 gs_derivative_boundary = 0 yaw_damper_gain = 0 [fuel] Center2 = -3.077122, -0.8, 0.3, 30, 0 Center3 = -3.077122, 0.8, 0.3, 30, 0 LeftMain = -0.577122, -4, 0, 171.7, 0 RightMain = -0.577122, 4, 0, 171.7, 0 LeftAux = -1.077122, -16.5, 0.55, 69.7, 0 RightAux = -1.077122, 16.5, 0.55, 69.7, 0 fuel_type = 1 number_of_tank_selectors = 1 electric_pump=0 [airplane_geometry] wing_area = 454 wing_span = 54.1666666666667 wing_root_chord = 8.38153846153846 wing_dihedral = 1.24 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.88419837495823 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 2.01826261538462 wing_pos_apex_vert = 0 htail_area = 44.98 htail_span = 20.9 htail_pos_lon = -27.12 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 13.3 vtail_span = 5.75 vtail_sweep = 0 vtail_pos_lon = -24.9 vtail_pos_vert = 0 elevator_area = 34.08 aileron_area = 34.4 rudder_area = 16 elevator_up_limit = 25 elevator_down_limit = 25 aileron_up_limit = 26.5 aileron_down_limit = 11.5 rudder_limit = 25 elevator_trim_limit = 18 spoiler_limit = 0.6555 spoilerons_available = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 [Reference Speeds] flaps_up_stall_speed = 93 full_flaps_stall_speed = 74.7 cruise_speed = 169 max_indicated_speed = 435 max_mach = 0.5585 [forcefeedback] gear_bump_nose_magnitude = 2000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 6050 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 6850 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 stick_shaker_magnitude = 2860 stick_shaker_direction = 0 stick_shaker_period = 111111 [gear_warning_system] gear_warning_available = 0 pct_throttle_limit = 0.1 flap_limit_idle = 33.75 flap_limit_power = 16.875 [brakes] toe_brakes_scale = 0.569170201727348 parking_brake = 1 differential_braking_scale = 15 [stall_warning] // 0 = None, 1 = Suction, 2 = Electric. type = 1 [hydraulic_system] electric_pumps = 0 engine_map = 1, 1, 0, 0 normal_pressure = 1225 [attitude_indicators] // 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] // 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0 = 1, 0 [direction_indicators] // 0=None, 1=Vac Gyro, 2=Elec Gyro, 3=EM Slave Compass, 4=Slave to other ind direction_indicator.0 = 1, 0 [airspeed_indicators] airspeed_indicator.0 = 1, 0