[fltsim.0] title=B10b NL sim=B10b model= panel= sound= texture=NL ui_manufacturer=martin KB_checklists= description=The Martin B-10 was the first all-metal monoplane bomber to go into regular use by the United States Army Air Corps, \nentering service in June 1934.It was also the first mass-produced bomber whose performance was superior to that \nof the Army's pursuit aircraft of the time.\nThe B-10 served as the airframe for the B-12, B-13, B-14, A-15 and O-45 designations.\nThe B-10 included several revolutionary features, and won Martin the Collier Trophy in 1932 for its design.\n [fltsim.1] title=B10b US sim=B10b model= panel= sound= texture=US ui_manufacturer=martin KB_checklists= description=The Martin B-10 was the first all-metal monoplane bomber to go into regular use by the United States Army Air Corps, \nentering service in June 1934.It was also the first mass-produced bomber whose performance was superior to that \nof the Army's pursuit aircraft of the time.\nThe B-10 served as the airframe for the B-12, B-13, B-14, A-15 and O-45 designations.\nThe B-10 included several revolutionary features, and won Martin the Collier Trophy in 1932 for its design.\n [fltsim.2] title=B10b USAAC sim=B10b model= panel= sound= texture=USaac2 ui_manufacturer=martin KB_checklists= description=The Martin B-10 was the first all-metal monoplane bomber to go into regular use by the United States Army Air Corps, \nentering service in June 1934.It was also the first mass-produced bomber whose performance was superior to that \nof the Army's pursuit aircraft of the time.\nThe B-10 served as the airframe for the B-12, B-13, B-14, A-15 and O-45 designations.\nThe B-10 included several revolutionary features, and won Martin the Collier Trophy in 1932 for its design.\n [WEIGHT_AND_BALANCE] empty_weight=15140 reference_datum_position=-0.01, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) ; 25% MAC distance from specified datum empty_weight_CG_position=0.05, 0, 0 // (feet) longitudinal, lateral, vertical max_number_of_stations=50 station_load.0=200, -3.0, +2.0, 3.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.0=200, -3.0, -2.0, 3.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=20265 empty_weight_roll_MOI=25806 empty_weight_yaw_MOI=45439 empty_weight_coupled_MOI=0.000000 [forcefeedback] gear_bump_nose_magnitude=6000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=6000 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=6000 gear_bump_right_direction=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [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=137.333333 compression_ratio=6.000000 number_of_cylinders=12 max_rated_rpm=3000.000000 max_rated_hp=1130.000000 fuel_metering_type=2 cooling_type=1 normalized_starter_torque=0.035000 turbocharged=1 max_design_mp=47.999999 min_design_mp=12.000000 critical_altitude=17000.000000 emergency_boost_type=3 emergency_boost_mp_offset=8.400000 emergency_boost_gain_offset=0.540000 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 //rotation=-1,1 //Engine 1,2,3,... Rotation direction. 1 = CW, -1 = CCW propeller_type=0 propeller_diameter=12.704000 propeller_blades=2 propeller_moi=37.947956 beta_max=65.000000 beta_min=15.000000 min_gov_rpm=1200.000000 prop_tc=0.010000 gear_reduction_ratio=2.380000 fixed_pitch_beta=20.000000 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 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,-25.750000, 0.000000,-2.4000, 6153.305, 0, 0.626,48.540, 0.305390, 2.500,0.726,5,5,0,0,0 point.1=1, 3.083333, -8.833333,-8.3000, 6153.305, 1, 0.626, 0.000, 0.407181, 2.500,0.726,5,5,2,0,0 point.2=1, 3.083333, 8.833333,-8.3000, 6153.305, 2, 0.626, 0.000, 0.407181, 2.500,0.726,5,5,3,0,0 point.3=2, 2.083333,-27.083333, 2.0833, 2475.912, 0, 0.000, 0.000, 0.000000, 0.000,0.000,0,0,0,5,0,0 point.4=2, 2.083333, 27.083333, 2.0833, 2475.912, 0, 0.000, 0.000, 0.000000, 0.000,0.000,0,0,0,6,0,0 point.5=2,-25.750000, 0.000000,-1.3333, 2475.912, 0, 0.000, 0.000, 0.000000, 0.000,0.000,0,0,0,9,0,0 point.6=2, 11.250000, 0.000000, 0.0000, 2475.912, 0, 0.000, 0.000, 0.000000, 0.000,0.000,0,0,0,4,0,0 static_pitch=12.5 static_cg_height=7.1 [Views] ;f/a - l/r - u/d eyepoint=2.717,-0.607,2.197 [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=10 // degrees, KIAS flaps-position.2=25 // degrees, KIAS flaps-position.3=35 // degrees, KIAS damaging-speed=201 // KIAS blowout-speed=305 // KIAS [LIGHTS] panel=0.00, 0.10, 0.35, fx_vclight [General] performance= Wingspan: 70 ft. 6 in.\nLength: 44 ft. 9 in.\nHeight: 15 ft. 5 in.\nEmpty Weight: 9,681 lbs\nGross Weight: 13,212 lbs\nTop Speed: 215 mph\nService Ceiling: 24,200 ft.\nRange: 1240 miles\nEngine\/Horsepower: Two Wright R-1820s\/700 each\nArmament: Three .30-in. machine guns, one each \nnose, rear cockpit, and fuselage bottom\s \n226 lbs of bombs [fuel] Center1=-4.157000,0.000000,0.000000,60.000000,0.000000 LeftMain=-1.120000,-4.000000,0.200000,171.700000,0.000000 LeftAux=-0.690000,-10.750000,0.580000,69.700000,0.000000 RightMain=-1.120000,4.000000,0.200000,171.700000,0.000000 RightAux=-0.690000,10.750000,0.580000,69.700000,0.000000 External1=-0.590000,-1.200000,-2.400000,120.100000,0.000000 External2=-0.590000,1.200000,-2.400000,120.100000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=454.000000 wing_span=54.166667 wing_root_chord=8.416667 wing_dihedral=0.000000 wing_incidence=1.499634 wing_twist=0.000000 oswald_efficiency_factor=0.888253 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.010000 wing_pos_apex_vert=0.000000 htail_area=34.000000 htail_span=10.500000 htail_pos_lon=-17.656667 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=-19.573333 vtail_pos_vert=3.250000 elevator_area=13.260000 aileron_area=18.900000 rudder_area=8.230000 elevator_up_limit=25.000000 elevator_down_limit=25.000000 aileron_up_limit=26.500000 aileron_down_limit=11.500000 rudder_limit=25.000000 elevator_trim_limit=18.000000 spoiler_limit=45.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [GeneralEngineData] engine_type=0 Engine.0=7.510000,-8.083333,0.000000 Engine.1=7.510000,8.083333,0.000000 fuel_flow_scalar=1.000000 [Reference Speeds] flaps_up_stall_speed=119.000000 full_flaps_stall_speed=95.200000 cruise_speed=285.359049 [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 [direction_indicators] direction_indicator.0=1,0
