[fltsim.0]
title=Martin B-10 Silver
sim=B-10
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
prop_anim_ratio=1.76
atc_id=
ui_manufacturer=Martin
ui_type="B-10"
ui_variation="Silver"
description=This model of the Martin B-10 is painted for both the 2nd and 19th Bomber Group
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
performance=
[fltsim.1]
title=Martin B-10 Yellow Blue
sim=B-10
model=
panel=
sound=
texture=1
kb_checklists=
kb_reference=
prop_anim_ratio=1.76
atc_id=
ui_manufacturer=Martin
ui_type="B-10"
ui_variation="Yellow Blue"
description=This model of the Martin B-10 is painted for both the 2nd and 19th Bomber Group
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
performance=
[weight_and_balance]
// ACM V2.5
max_gross_weight = 14700
empty_weight = 9681
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 69699.03
empty_weight_roll_MOI = 61179.1
empty_weight_yaw_MOI = 131797.97
empty_weight_coupled_MOI = 0
max_number_of_stations = 2
station_load.0 = 170, 3.34, 0, 2.06
station_load.1 = 170, -9.46, 0, 2.22
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4, 3.143, 0.0, 3.143, fx_vclight,
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.0
min_throttle_limit = 0.0
master_ignition_switch = 1
engine.0 = 6.23, -8.32, -0.02,
engine.1 = 6.23, 8.32, -0.02,
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
startup = fx_engstrt_jenny
windshield_rain_effect_available = 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 2
electric_pump = 1
Center1 = 0, 0, -20, 200, 0
LeftMain = -2.25, -5, 0, 202, 0
RightMain = -2.25, 5, 0, 202, 0
[contact_points]
static_pitch = 11.4
static_cg_height = 6.5
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 7
point.0 = 1, -29.0099, 0, -0.9873, 1200, 0, 0.6, 22, 0.2, 2.5, 0.695, 0, 0, 0, 0, 0
point.1 = 1, 0.884, -8.25, -7.3593, 1600, 1, 1.7, 0, 0.704, 2.5, 0.686, 5, 5, 7, 166, 166
point.2 = 1, 0.776, 8.25, -7.3593, 1600, 2, 1.7, 0, 0.704, 2.5, 0.682, 5, 5, 7, 166, 166
point.3 = 2, -1.7962, -34.7481, 0.674, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.685, 34.3034, 0.8963, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -31.6892, 0, 0.829, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 10.8122, -0.1106, -3.3706, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
[keyboard_response]
elevator = 200, 1000
aileron = 200, 1000
rudder = 200, 1000
[forcefeedback]
ground_bumps_magnitude1 = 2600
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.6
ground_bumps_magnitude2 = 1200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.085
ground_bumps_slope2 = 0.65
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 3500000
[airplane_geometry]
wing_area = 678
wing_span = 70.5
wing_root_chord = 12.85
wing_dihedral = 3
wing_incidence = 2.0
wing_twist = -1.0
oswald_efficiency_factor = 0.65
wing_winglets_flag = 0
wing_sweep = 5
wing_pos_apex_lon = 4.30
wing_pos_apex_vert = -0.13
htail_area = 95.8
htail_span = 20
htail_pos_lon = -23.17
htail_pos_vert = 1.66
htail_incidence = -1.0
htail_sweep = 15
vtail_area = 37.9
vtail_span = 7.88
vtail_sweep = 25
vtail_pos_lon = -21.87
vtail_pos_vert = 1.02
elevator_area = 83.4
aileron_area = 102.8
rudder_area = 46.7
elevator_up_limit = 22.0
elevator_down_limit = 22.0
aileron_up_limit = 22.0
aileron_down_limit = 22.0
rudder_limit = 25.0
elevator_trim_limit = 12.0
spoiler_limit = 60.0
aileron_to_spoileron_gain = 0
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 25
max_generator_alternator_amps = 100
engine_generator_map = 1,1
electric_always_available = 0
[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
p_factor_on_yaw = 0.5
torque_on_roll = 1.0
gyro_precession_on_yaw = 1.0
gyro_precession_on_pitch = 1.0
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 35 // degrees
damaging-speed = 140 // KIAS
blowout-speed = 175 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[piston_engine]
power_scalar=1.0 //Piston power scalar
cylinder_displacement=130.71 //Cubic inches per cylinder
compression_ratio=6.7 //Compression ratio
number_of_cylinders=14 //Number of cylinders
max_rated_rpm=2700 //Max rated RPM
max_rated_hp=775 //Max rated HP
fuel_metering_type=1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3 //Starter torque factor
turbocharged=1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=47 //Max design manifold pressure, (inHg)
min_design_mp=10 //Min design manifold pressure, (inHg)
critical_altitude=7000 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset=0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar=1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=12 //Propeller Diameter, (feet)
propeller_blades=3 //Number of propeller blades
propeller_moi=40.2 //Propeller moment of inertia
beta_max=30.0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=18.0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=1400 //Miminum governed RPM
prop_tc=0.1 //Prop time-constant
gear_reduction_ratio=1.778 //Propeller gear reduction ratio
fixed_pitch_beta=0.0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80.0 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=1 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=700.0 //Minimum RPM for prop feathering
beta_feather=89.5 //Feathering pitch angle (degrees)
power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller in feather
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=0.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0.0 //Minimum pitch angle in reverse, (degrees)
feathering_switches=1 //Switches which invoke feathering
//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
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 0.0 //Flap angle that activates warning at idle
flap_limit_power = 16.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.7 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure = 732.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint=3.143, 0.0, 3.143
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Adf.2 = 1
Transponder.1=0
Marker.1=1
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=1,0
direction_indicator.1=2,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
attitude_indicator.1 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=2,0
[Reference Speeds]
flaps_up_stall_speed=67.5 //Knots True (KTAS)
full_flaps_stall_speed=61.5 //Knots True (KTAS)
cruise_speed=95.0 //Knots True (KTAS)
max_indicated_speed = 224 //Red line (KIAS)
[autopilot]
autopilot_available=0
flight_director_available=0
pitch_takeoff_ga=0.0
default_vertical_speed=700.000000
autothrottle_available=0
direction_indicator=1
attitude_indicator =1
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 = 0.0
default_bank_mode=2 //Default to Heading Hold
[stall_warning]
type=1
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
[General]
performance=Span: 70' 6"\nLength: 44' 9"\nWeight: 9681 empty, 14700 gross\nRange: 1370 miles\nSpeed: 183 mph cruise, 215 mph top\nCeiling:24,000 ft.\nPower: 2 Wright R-1820's at 775hp.\nDesigner: P. Clawson 1\/2006\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n
