[fltsim.0] title=Devastator sim=Devastator Karliten model= panel= sound= texture= ui_manufacturer=Douglas ui_type=TBD-1 Devastator ui_variation=US Navy description= El TBD-1 inició sus vuelos en abril de 1935 y fue el primer monoplano de la US Navy. La producción totalizó 130 ejemplares y el único escuadrón de Devastator presente en la batalla de Midway (junio de 1942) sufrió tal carnicería, que el modelo fue retirado del servicio en primera línea. Carlos José LAGIOIA. Quilmes. Buenos Aires. Argentina. Enero 2006. [General] performance=Envergadura : 15.24 m\nLongitud : 10.67 m\nPeso : 4,624 kg\nPlanta motriz : Pratt & Whitney R-1830-64 Twin Wasp de 900 Hp\nVelocidad máxima : 206 m/h a 8,000 pies\nAlcance operacional : 717 millas\n [WEIGHT_AND_BALANCE] empty_weight = 6182.0 // (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, 1.7, 0.0, 2.3 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.0 = 170, -5.0, 0.0, 2.3 //Gunner Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 8497.03 //slug-ft^2 empty_weight_roll_MOI = 7505.58 //slug-ft^2 empty_weight_yaw_MOI = 13196.87 //slug-ft^2 empty_weight_coupled_MOI=0.000000 max_gross_weight=9528.000000 [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=126.000000 compression_ratio=7.200000 number_of_cylinders=14 max_rated_rpm=2600.000000 max_rated_hp=985.000000 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.035000 turbocharged=1 max_design_mp=39.999999 min_design_mp=1.000000 critical_altitude=10000.000000 emergency_boost_type=0 emergency_boost_mp_offset=0.000000 emergency_boost_gain_offset=0.000000 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 propeller_type=0 propeller_diameter=10.500000 propeller_blades=3 propeller_moi=30.380000 beta_max=49.000000 beta_min=22.000000 min_gov_rpm=1400.000000 prop_tc=0.010000 gear_reduction_ratio=1.710000 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 [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.12,0.11 ;Percent per second [TailHook] tailhook_length=4 ;(feet) tailhook_position = -15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust = 1.0 [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 point.0=1, -20.20, 0.00, -3.66, 3200, 0, 0.30, 90.0, 0.50, 2.5, 0.90, 5.0, 3.0, 0 point.1=1, 2.03, -6.11, -8.69, 2200, 1, 1.30, 0.0, 0.90, 2.5, 0.83, 5.5, 6.5, 2 point.2=1, 2.03, 6.11, -8.69, 2200, 2, 1.30, 0.0, 0.90, 2.5, 0.83, 8.0, 8.0, 3 point.3=2, 0.00, -20.00, -1.25, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5 point.4=2, 0.00, 20.00, -1.25, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6 point.5=2, -20.25, 0.00, -1.66, 2400, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9 point.6=2, 2.41, 0.00, -2.08, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4 static_pitch = 13.9 //degrees (pitch when loaded on ground) static_cg_height = 7.19 //(feet) altitude of CG when at rest (altitude when loaded on ground) gear_system_type=1 [Views] eyepoint = -2.4, 0.0, 2.1 //(feet) longitudinal, lateral, vertical distance from reference datum [General] performance=Need specs here [fuel] LeftMain=-1.000000,-4.600000,-1.000000,145.000000,0.000000 RightMain=-1.000000,4.600000,-1.000000,145.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=415.000000 wing_span=50.916667 wing_root_chord=8.083333 wing_dihedral=6.701660 wing_incidence=0.999756 wing_twist=0.000000 oswald_efficiency_factor=0.700361 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=-0.999756 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=13.000000 aileron_area=20.400000 rudder_area=13.060000 elevator_up_limit=26.000825 elevator_down_limit=26.000825 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 [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 [Flaps.0] type=1 span-outboard=0.500000 extending-time=5.000000 system_type=1 flaps-position.0=0.000000,0.000000 flaps-position.1=10.426415,0.000000 flaps-position.2=15.252831,0.000000 flaps-position.3=20.279246,0.000000 flaps-position.4=25.305662,0.000000 flaps-position.5=30.032077,0.000000 [GeneralEngineData] engine_type=0 Engine.0=8.750000,0.000000,0.000000 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed=67.000000 full_flaps_stall_speed=53.600000 cruise_speed=194.748106 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=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0 [LIGHTS] panel=0.00, 0.75, -0.80, fx_vclight light.0=3, -0.17, -25.0, -0.10, fx_navred light.1=3, -0.17, 25.0, -0.10, fx_navgre light.2=3, -23.31, 0.0, 0.55, fx_navwhi
