//Breguet 1150 Atlantic I FD Files Ver 1.1, 18 Dec 04 [fltsim.0] title=Breguet 1150 Atlantic I, Flottille 23F sim=Atlantic I model= panel= sound= texture=23F kb_checklists= kb_reference= atc_heavy=0 atc_airline="Navy" atc_flight_number=44 atc_id=44 atc_id_color=0x00000000 atc_parking_types=MIL_COMBAT ui_manufacturer=M.Dassault Breguet ui_type=1150 ui_variation=Atlantic I, French Navy, 23F of Lann-Bihoué Navy Base Description=Breguet (later Dassault-Breguet) designed the 1150 Atlantic maritime patrol aircraft to meet a 1958 NATO specification. The prototype first flew on 21 October 1961. Initial orders were for 40 aircraft for France and 20 for Germany. The last of these was completed in 1968. Later, The Netherlands ordered nine aircraft and Italy 18. Three French aircraft were sold to Pakistan in 1975.\nModel by Massimo Taccoli. Panel By Jean-Pierre Langer. Flight Dynamics by Dennis Seeley. atc_id_font=Verdana,-11,1,600,0 visual_damage=0 [fltsim.1] title=Breguet 1150 Atlantic I,Flottille 24F sim=Atlantic I model= panel= sound= texture=24F kb_checklists= kb_reference= atc_heavy=0 atc_airline="Navy" atc_flight_number=48 atc_id=48 atc_id_color=0x00000000 atc_parking_types=MIL_COMBAT ui_manufacturer=M.Dassault Breguet ui_type=1150 ui_variation=Atlantic I French Navy, 24F of Lann-Bihoué Navy Base Description=Breguet (later Dassault-Breguet) designed the 1150 Atlantic maritime patrol aircraft to meet a 1958 NATO specification. The prototype first flew on 21 October 1961. Initial orders were for 40 aircraft for France and 20 for Germany. The last of these was completed in 1968. Later, The Netherlands ordered nine aircraft and Italy 18. Three French aircraft were sold to Pakistan in 1975.\nModel by Massimo Taccoli. Panel By Jean-Pierre Langer. Flight Dynamics by Dennis Seeley. atc_id_font=Verdana,-11,1,600,0 visual_damage=0 [General] atc_type=Breguet atc_model=1150 editable=0 Performance=Length: 104 ft 1.5 in.\nHeight: 37 ft 1.75 in.\nWing Span: 119 ft 1.25 in.\nWing Area: 1295.33 sq ft.\nWgts: Empty 55,115 lb, MTO 98,104 lb.\nEngines: Two RR Tyne R.Ty.20 Mk 21.\nPower: 6,105 ehp each.\nMax Level Speed: 409 mph at high altitude.\nMax Cruise Speed: 363 mph TAS at 19,685 ft.\nStall Speed (76,500 lb): Clean: 119 mph IAS. Full flaps: 100 mph IAS.\nInitial Climb: 2,450 fpm\nService Ceiling: 32,800 ft.\nRange: 5,590 mi.\nEndurance: 18 hrs at 195 mph patrol speed. Category=airplane [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 elevator_trim_effectiveness =1.0 aileron_trim_effectiveness =1.0 rudder_trim_effectiveness =1.0 pitch_stability =1.0 roll_stability =1.0 yaw_stability =1.0 hi_alpha_on_roll = 1.0 [weight_and_balance] // ACM V2.5 max_gross_weight = 98104 empty_weight = 55115 reference_datum_position = 0.3, 0, -0.43 empty_weight_CG_position = -2, 0, 0.25 empty_weight_pitch_MOI = 609848.9 empty_weight_roll_MOI = 334635.4 empty_weight_yaw_MOI = 920616.3 empty_weight_coupled_MOI = 0 CG_forward_limit = 1.0 CG_aft_limit = -1.0 max_number_of_stations = 2 station_load.0 = 170.0, 22.4, -2.5, 3.6, Pilot station_load.1 = 170.0, 22.4, 2.5, 3.6, Co-pilot [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -2.024, 59.80, 3.46, fx_navgre light.1 = 3, -2.024, -59.80, 3.46, fx_navred light.2 = 3, -58.290, 0.00, 6.79, fx_navwhi light.3 = 1, -3.390, 0.00, 9.33, fx_beacon light.4 = 2, -3.050, 60.20, 3.46, fx_strobeh light.5 = 2, -3.050, -60.20, 3.46, fx_strobeh light.6 = 8, 0.328, 27.65, 0.203, fx_navwhih light.7 = 8, 0.328, -27.65, 0.203, fx_navwhih [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 5 fuel_flow_scalar = 0.85 min_throttle_limit = -0.25 engine.0 = 15.46, 14.75, 0.25 engine.1 = 15.46, -14.75, 0.25 [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 1 windshield_rain_effect_available = 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 1 electric_pump = 1 LeftMain = -1.5, -20, 0.25, 1545, 0 LeftAux = -1.5, -30, 0.25, 1545, 0 RightMain = -1.5, 20, 0.25, 1545, 0 RightAux = -1.5, 30, 0.25, 1545, 0 [contact_points] static_pitch = -0.5 static_cg_height = 10 tailwheel_lock = 0 gear_system_type = 1 max_number_of_points = 7 point.0 = 1, 26.5, 0, -9.5, 1574, 0, 1.18, 45, 0.275, 2.5, 0.675, 9, 9, 0, 200, 200 point.1 = 1, -4.75, -14.75, -10, 1574, 1, 1.9, 0, 0.657, 1.25, 0.433, 8, 8, 2, 200, 200 point.2 = 1, -4.75, 14.75, -10, 1574, 2, 1.9, 0, 0.657, 1.25, 0.433, 8, 8, 3, 200, 200 point.3 = 2, -4.50, -60.17, 3.90, 1574, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5, 0.0, 0.0 point.4 = 2, -4.50, 60.17, 3.90, 1574, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6, 0.0, 0.0 point.5 = 2, -73.40, 0.00, 4.40, 1574, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9, 0.0, 0.0 point.6 = 2, 31.80, 0.00, 0.36, 1574, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 4, 0.0, 0.0 [keyboard_response] elevator = 100.0, 180.0 aileron = 200.0, 1000.0 rudder = 200.0, 1000.0 [airplane_geometry] wing_area = 1295.370 wing_span = 119.100 wing_root_chord = 15.333 wing_dihedral = 3.600 wing_incidence = 1.500 wing_twist = -2.500 oswald_efficiency_factor = 0.750 wing_winglets_flag = 0 wing_sweep = 5.600 wing_pos_apex_lon = 3.833 wing_pos_apex_vert = 0.000 htail_area = 349.700 htail_span = 40.354 htail_pos_lon = -39.292 htail_pos_vert = 6.750 htail_incidence = 0.000 htail_sweep = 16.500 vtail_area = 179.100 vtail_span = 16.083 vtail_sweep = 19.500 vtail_pos_lon = -41.958 vtail_pos_vert = 8.167 elevator_area = 89.100 aileron_area = 58.000 rudder_area = 64.100 elevator_up_limit = 27.000 elevator_down_limit = 27.000 aileron_up_limit = 21.000 aileron_down_limit = 15.000 rudder_limit = 21.000 elevator_trim_limit = 30.000 spoiler_limit = 90.000 aileron_to_spoileron_gain = 0.000 spoiler_handle_available = 1 min_ailerons_for_spoilerons = 0.000 min_flaps_for_spoilerons = 0.000 spoilerons_available = 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 200 engine_generator_map = 1,1 electric_always_available = 0 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 5, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 2, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 [Brakes] parking_brake = 1 toe_brakes_scale = 0.75 [Views] eyepoint =10.5, -1.0, 3.0 [Flaps.0] type = 1 system_type = 0 lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar = 1.0 span-outboard = 0.75 extending-time= 4.0 damaging-speed= 230.0 blowout-speed = 300.0 flaps-position.0= 0.0, 0.0 flaps-position.1= 15.0, 230.0 flaps-position.2= 25.0, 200.0 flaps-position.3= 40.0, 150.0 [TurbineEngineData] afterburner_available =0 fuel_flow_gain =0.011 inlet_area =0.825 rated_N2_rpm =14500.000 static_thrust =1065.000 [Turboprop_engine] power_scalar=1.0 max_rpm_mechanical_efficiency_scalar = 1.0 idle_rpm_mechanical_efficiency_scalar= 1.0 max_rpm_friction_scalar = 1.0 idle_rpm_friction_scalar = 1.0 maximum_torque =29373.0 [Propeller] thrust_scalar =1.0 propeller_type =0 prop_sync_available =1 prop_deice_available =1 prop_feathering_available =1 prop_auto_feathering_available =1 defeathering_accumulators_available =0 propeller_blades =4 propeller_diameter =16 propeller_moi =40.000 beta_max =55.000 beta_min =20.000 min_gov_rpm =700.000 prop_tc =0.001 gear_reduction_ratio =15.625 fixed_pitch_beta =0.000 low_speed_theory_limit =80.000 min_rpm_for_feather =700.000 beta_feather =88.000 power_absorbed_cf =0.900 minimum_on_ground_beta =10.000 prop_reverse_available =0.250 minimum_reverse_beta =-14.000 [Radios] Audio.1 =1 Com.1 =1, 0 Com.2 =1, 0 Nav.1 =1, 0, 1 Nav.2 =1, 0, 1 Adf.1 =1 Transponder.1=1 Marker.1 =1 [Hydraulic_system] electric_pumps = 1 engine_map = 1,1,0,0 normal_pressure = 3000.0 [Exits] number_of_exits = 2 exit_rate.0 = 0.4 exit_rate.1 = 0.6 [TailHook] //used for Radar radome up and down movement tailhook_length = 1 ;(feet) cable_force_adjust = 1.0 tailhook_position = 5.183, 0.0, -5.62 [Gear_warning_system] gear_warning_available= 1 pct_throttle_limit = 0.0 flap_limit_idle = 10.0 flap_limit_power = 30.0 [Stall_warning] type =2 stick_shaker =1 [Pitot_static] vertical_speed_time_constant = 1.0 pitot_heat =1.000000 [Direction_indicators] direction_indicator.0 =3,0 [Attitude_indicators] attitude_indicator.0 = 1 [Turn_indicators] turn_indicator.0 = 1,0 [Airspeed_indicators] airspeed_indicator.0 = 1, 0 [Autopilot] autopilot_available=1 flight_director_available=1 default_pitch_mode = 0 default_bank_mode = 0 autothrottle_available=1 autothrottle_arming_required = 0 autothrottle_takeoff_ga = 1.00 autothrottle_max_rpm = 110.00 max_throttle_rate = 0.001 default_vertical_speed=1000.00 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 yaw_damper_gain = 1.00 nav_proportional_control = 11.00 nav_integrator_control = 0.20 nav_derivative_control = 0.00 nav_integrator_boundary = 2.50 nav_derivative_boundary = 0.00 gs_proportional_control = 9.52 gs_integrator_control = 0.26 gs_derivative_control = 0.00 gs_integrator_boundary = 0.70 gs_derivative_boundary = 0.00 [Reference Speeds] flaps_up_stall_speed =86.0 full_flaps_stall_speed =76.0 cruise_speed =300.0 max_indicated_speed = 355.0 max_mach = 0.7 [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 =0.150000 [deice_system] structural_deice_type =0 [forcefeedback] gear_bump_nose_magnitude = 3000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2700 gear_bump_left_direction = 9000 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2700 gear_bump_right_direction = 27000 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1300 ground_bumps_angle1 = 08900 ground_bumps_intercept1 = 3.0 ground_bumps_slope1 = 0.2 ground_bumps_magnitude2 = 200 ground_bumps_angle2 = 09100 ground_bumps_intercept2 = 1.075 ground_bumps_slope2 = 0.035 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 stick_shaker_magnitude = 5000 stick_shaker_direction = 0 stick_shaker_period = 111111
