[fltsim.0] title=p39 sim=mz-p39 model= panel= sound= texture= kb_checklists=P39D_check kb_reference=P39D_ref atc_id= ui_manufacturer=Bell ui_type='P-39D ui_variation=P-39 Bell Aircobra description=Bell P39 Aircobra [fltsim.1] title=P39N sim=mz-p39 model= panel= sound= texture=n kb_checklists=P39D_check kb_reference=P39D_ref atc_id= ui_manufacturer=Bell ui_type='P-39D ui_variation=P-39N Russian Aircobra description=P-39N flown by Russian fighter ace Grigori A. Rechkolov, 16 GIAP, June 1944. [WEIGHT_AND_BALANCE] empty_weight = 5645.0 // (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, 1.3, 0.0, 1.5 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 5760.89 //slug-ft^2 empty_weight_roll_MOI = 3167.42 //slug-ft^2 empty_weight_yaw_MOI = 6863.67 //slug-ft^2 empty_weight_coupled_MOI=0.000000 max_gross_weight=8722.500000 [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 = 1.500 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.12,0.11 ;Percent per second [piston_engine] power_scalar = 1.0 cylinder_displacement=142.500000 compression_ratio=6.650000 number_of_cylinders=12 max_rated_rpm=3000.000000 max_rated_hp=1150.000000 fuel_metering_type=0 cooling_type=1 normalized_starter_torque=0.035000 turbocharged=1 max_design_mp=53.999999 min_design_mp=1.000000 critical_altitude=21000.000000 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=11.580000 propeller_blades=3 propeller_moi=40.800000 beta_max=65.000000 beta_min=23.000000 min_gov_rpm=1800.000000 prop_tc=0.010000 gear_reduction_ratio=2.230000 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 [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, 7.67, 0.00, -5.10, 1600, 0, 0.75, 43.0, 0.40, 2.5, 0.90, 4.0, 3.0, 0 point.1=1, -1.92, -6.00, -4.45, 2200, 1, 1.05, 0.0, 0.45, 2.5, 0.83, 7.5, 7.5, 2 point.2=1, -1.92, 6.00, -4.45, 2200, 2, 1.05, 0.0, 0.45, 2.5, 0.83, 5.5, 8.0, 3 point.3=2, 0.00, -20.00, 0.25, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5 point.4=2, 0.00, 20.00, 0.25, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6 point.5=2, -20.25, 0.00, -0.16, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9 point.6=2, 2.41, 0.00, -0.58, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4 static_pitch = 5.4 //degrees (pitch when loaded on ground) static_cg_height = 5.60 //(feet) altitude of CG when at rest (altitude when loaded on ground) gear_system_type=1 [Views] eyepoint = 0.17, 0.0, 4.05 //(feet) longitudinal, lateral, vertical distance from reference datum [forcefeedback] gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [General] performance=ÅåoÍF1150\nÅå¬xF312\/i3600j\nSF10.36\nS·F9.19 [fuel] LeftMain=-2.000000,-9.000000,-1.700000,60.000000,0.000000 RightMain=-2.000000,9.000000,-1.700000,60.000000,0.000000 External1=-0.500000,0.000000,-4.500000,75.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=213.000000 wing_span=34.000000 wing_root_chord=6.083333 wing_dihedral=5.998535 wing_incidence=0.999756 wing_twist=0.000000 oswald_efficiency_factor=0.733955 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=11.000000 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=19.996227,0.000000 flaps-position.2=39.992454,0.000000 flaps-position.3=59.988681,0.000000 flaps-position.4=79.984908,0.000000 [GeneralEngineData] engine_type=0 Engine.0=-3.250000,0.000000,0.000000 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed=86.000000 full_flaps_stall_speed=68.800000 cruise_speed=250.000000 max_indicated_speed=760.500000 [keyboard_response] elevator=350.000000,500.000000 aileron=450.000000,1000.000000 rudder=200.000000,1000.000000 [Radios] Audio.1=1 Com.1=1,0 Com.2=1,0 Nav.1=1,0,1 Nav.2=1,0,0 Adf.1=1,0 Transponder.1=1 Marker.1=1 [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 default_pitch_mode=0 default_bank_mode=0 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 normal_pressure=6.930556 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0
