//2:04 PM 11/22/2005 [fltsim.0] title=ALPHA Martin-Baker MB.5 sim=MB5 model= panel= sound= texture= kb_checklists=mb5_ck description=© ALPHA Simulations 2005\n\nFirst flown on May 23, 1944, the Martin-Baker M.B.5 was the fifth in a series of experimental prototype fighter aircraft. Powered by the Rolls-Royce Griffon 83 engine, the plane's performance was instantly impressive, with excellent handling qualities and a high top speed of over 460 mph. Pilots who flew it generally raved about the handling, going so far in some cases as to call it the finest-handling fighter ever made. The type used an innovative steel-tube framework which was said to simplify maintenance and add strength. However, in the event, a contract was never awarded and the M.B.5 became another of those great aircraft never to be mass-produced. ui_manufacturer=Martin Baker ui_type=Martin-Baker MB.5 ui_variation=1. Prototype atc_heavy=0 atc_id=R2496 atc_airline= atc_flight_number= atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 [fltsim.1] title=ALPHA Martin-Baker MB.5 RAF sim=MB5 model=RAF panel=2 sound= texture=RAF kb_checklists=mb5_ck description=© ALPHA Simulations 2005\n\nFirst flown on May 23, 1944, the Martin-Baker M.B.5 was the fifth in a series of experimental prototype fighter aircraft. Powered by the Rolls-Royce Griffon 83 engine, the plane's performance was instantly impressive, with excellent handling qualities and a high top speed of over 460 mph. Pilots who flew it generally raved about the handling, going so far in some cases as to call it the finest-handling fighter ever made. The type used an innovative steel-tube framework which was said to simplify maintenance and add strength. However, in the event, a contract was never awarded and the M.B.5 became another of those great aircraft never to be mass-produced. ui_manufacturer=Martin Baker ui_type=Martin-Baker MB.5 ui_variation=2. In-service version atc_heavy=0 atc_id=P6333 atc_airline= atc_flight_number= atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 [fltsim.2] title=ALPHA Martin-Baker MB.5 RAF 2 sim=MB5 model=RAF panel=2 sound= texture=RAF2 kb_checklists=mb5_ck description=© ALPHA Simulations 2005\n\nFirst flown on May 23, 1944, the Martin-Baker M.B.5 was the fifth in a series of experimental prototype fighter aircraft. Powered by the Rolls-Royce Griffon 83 engine, the plane's performance was instantly impressive, with excellent handling qualities and a high top speed of over 460 mph. Pilots who flew it generally raved about the handling, going so far in some cases as to call it the finest-handling fighter ever made. The type used an innovative steel-tube framework which was said to simplify maintenance and add strength. However, in the event, a contract was never awarded and the M.B.5 became another of those great aircraft never to be mass-produced. ui_manufacturer=Martin Baker ui_type=Martin-Baker MB.5 ui_variation=3. In-service version, bare-metal atc_heavy=0 atc_id=SS655 atc_airline= atc_flight_number= atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 [fltsim.3] title=ALPHA Martin-Baker MB.5 racer 1 sim=MB5 model=racer panel= sound= texture=racer kb_checklists=mb5_ck description=© ALPHA Simulations 2005\n\nFirst flown on May 23, 1944, the Martin-Baker M.B.5 was the fifth in a series of experimental prototype fighter aircraft. Powered by the Rolls-Royce Griffon 83 engine, the plane's performance was instantly impressive, with excellent handling qualities and a high top speed of over 460 mph. Pilots who flew it generally raved about the handling, going so far in some cases as to call it the finest-handling fighter ever made. The type used an innovative steel-tube framework which was said to simplify maintenance and add strength. However, in the event, a contract was never awarded and the M.B.5 became another of those great aircraft never to be mass-produced. ui_manufacturer=Martin Baker ui_type=Martin-Baker MB.5 ui_variation=4. Pylon Racer 1 atc_heavy=0 atc_id=G5 atc_airline= atc_flight_number= atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 [fltsim.4] title=ALPHA Martin-Baker MB.5 racer 2 sim=MB5 model=racer panel= sound= texture=racer2 kb_checklists=mb5_ck description=© ALPHA Simulations 2005\n\nFirst flown on May 23, 1944, the Martin-Baker M.B.5 was the fifth in a series of experimental prototype fighter aircraft. Powered by the Rolls-Royce Griffon 83 engine, the plane's performance was instantly impressive, with excellent handling qualities and a high top speed of over 460 mph. Pilots who flew it generally raved about the handling, going so far in some cases as to call it the finest-handling fighter ever made. The type used an innovative steel-tube framework which was said to simplify maintenance and add strength. However, in the event, a contract was never awarded and the M.B.5 became another of those great aircraft never to be mass-produced. ui_manufacturer=Martin Baker ui_type=Martin-Baker MB.5 ui_variation=5. Pylon Racer 2 atc_heavy=0 atc_id=N99SIM atc_airline= atc_flight_number= atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 [General] atc_type= atc_model= performance=Model Designer: C Lampard\nPanel: P Perrott\nGauges: H Pralle\nFlight model: J McDaniel\nTextures: G Flores\nSounds: P Savereux\n\nLength: 37 ft 9 in\nSpan: 35 ft 0 in\nWing area: 264 sq ft\nEmpty weight: 9,000 lbs\nMaximum weight: 11,500 lbs\nPower: Rolls-Royce Griffon 83, 2,340 H.P.\nPropellers: Twin 3-blade DeHavilland, contra-rotating\nRange: 650 miles @ 225 mph\nMax Speed: 460 m.p.h @ 20,000 ft.\nRate of climb: 5,000 fpm\nService Ceiling: 44,000 ft.\nArmament: Four 20mm cannon editable=1 Category=airplane [weight_and_balance] max_gross_weight = 11500.000 empty_weight = 9000.000 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = 0.000, 0.000, 0.000 empty_weight_pitch_MOI = 15472.000 empty_weight_roll_MOI = 9005.000 empty_weight_yaw_MOI = 15418.000 empty_weight_coupled_MOI = 0.000 CG_forward_limit = 0.000 CG_aft_limit = 1.000 max_number_of_stations = 0 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 4, -1.50, 0.00, 1.50, fx_vclight [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 0 fuel_flow_scalar = 1.000 min_throttle_limit = 0.000000 engine.0 = 10.800, 0.000, 0.000 [effects] windshield_rain_effect_available = 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 number_of_tank_selectors = 1 electric_pump = 1 Center1 = 1.000, 0.000, 0.000, 75.000, 0.000 Center2 = -1.000, 0.000, 0.000, 75.000, 0.000 [contact_points] static_pitch = 13.660 static_cg_height = 6.860 tailwheel_lock = 1 gear_system_type = 1 max_number_of_points = 7 point.0 = 1.000, -19.000, 0.000, -3.100, 1800.000, 0.000, 0.549, 39.600, 0.400, 2.500, 0.800, 5.000, 5.000, 0.000, 165.000, 230.000 point.1 = 1.000, 1.350, -7.500, -7.600, 2500.000, 1.000, 1.450, 0.000, 0.422, 2.500, 0.870, 5.000, 5.000, 2.000, 165.000, 230.000 point.2 = 1.000, 1.350, 7.500, -7.600, 2500.000, 2.000, 1.450, 0.000, 0.422, 2.500, 0.870, 5.000, 5.000, 3.000, 165.000, 230.000 point.3 = 2.000, 0.000, -17.500, -0.500, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4 = 2.000, 0.000, 17.500, -0.500, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5 = 2.000, -13.333, 0.000, -2.667, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6 = 2.000, 10.800, 0.000, -6.000, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 [keyboard_response] elevator = 350.000000, 500.000000 aileron = 450.000000, 1000.000000 rudder = 200.000000, 1000.000000 [forcefeedback] gear_bump_nose_magnitude = 1000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2000 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2000 gear_bump_right_direction = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 450 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1 crash_magnitude1 = 2000 crash_direction1 = 1000 crash_magnitude2 = 2000 crash_direction2 = 9000 crash_period2 = 7500 crash_duration2 = 2500000 stick_shaker_magnitude = 2000 stick_shaker_direction = 0 stick_shaker_period = 111111 [airplane_geometry] wing_area = 264.100 wing_span = 35.090 wing_root_chord = 9.520 wing_dihedral = 5.000 wing_incidence = 0.000 wing_twist = 0.000 oswald_efficiency_factor = 0.800 wing_winglets_flag = 0 wing_sweep = 3.000 wing_pos_apex_lon = 2.370 wing_pos_apex_vert = 0.000 htail_area = 32.000 htail_span = 13.520 htail_pos_lon = -14.380 htail_pos_vert = 1.890 htail_incidence = -1.000 htail_sweep = 17.000 vtail_area = 15.000 vtail_span = 5.250 vtail_sweep = 25.000 vtail_pos_lon = -16.620 vtail_pos_vert = 2.290 elevator_area = 18.000 aileron_area = 20.000 rudder_area = 12.000 elevator_up_limit = 28.000 elevator_down_limit = 23.000 aileron_up_limit = 20.000 aileron_down_limit = 15.000 rudder_limit = 28.000 elevator_trim_limit = 18.000 spoiler_limit = 60.000 aileron_to_spoileron_gain = 0.000 spoiler_handle_available = 0 min_ailerons_for_spoilerons = 0.000 min_flaps_for_spoilerons = 0.000 spoilerons_available = 0 auto_spoiler_available=0 spoiler_extension_time=0.000000 positive_g_limit_flaps_up=12.000000 positive_g_limit_flaps_down=10.000000 negative_g_limit_flaps_up=-8.000000 negative_g_limit_flaps_down=-6.000000 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 100 engine_generator_map = 1 electric_always_available = 0 [piston_engine] cylinder_displacement= 186.580 compression_ratio= 6.000 number_of_cylinders= 12 max_rated_rpm= 2750.000 max_rated_hp= 2340.000 fuel_metering_type= 0 cooling_type= 1 normalized_starter_torque= 0.035 turbocharged= 1 max_design_mp= 81.000 min_design_mp= 5.000 critical_altitude= 21000.000 emergency_boost_type= 0 emergency_boost_mp_offset= 0.000 emergency_boost_gain_offset= 0.000 fuel_air_auto_mixture= 1 auto_ignition= 0 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 power_scalar=1.000 [propeller] propeller_type= 0 propeller_diameter= 12.500 propeller_blades= 6 propeller_moi= 88.000 beta_max= 65.000 beta_min= 15.000 min_gov_rpm= 1200.000 prop_tc= 0.010 gear_reduction_ratio= 1.960 fixed_pitch_beta= 0.000 low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 0 prop_feathering_available= 0 prop_auto_feathering_available= 0 min_rpm_for_feather= 0.000 beta_feather= 0.000 power_absorbed_cf= 0.000 defeathering_accumulators_available= 0 prop_reverse_available= 0.000 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 thrust_scalar=1.000 [Reference Speeds] flaps_up_stall_speed= 93.000 full_flaps_stall_speed= 83.000 cruise_speed= 300.000 max_indicated_speed=440 [Views] eyepoint=-2.40, 0.00, 3.30 [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 [direction_indicators] direction_indicator.0=1,0 [brakes] toe_brakes_scale=0.5 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 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 normal_pressure=1000 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [flight_tuning] cruise_lift_scalar=1 parasite_drag_scalar=1 induced_drag_scalar=1 elevator_effectiveness=1 aileron_effectiveness=1 rudder_effectiveness=1 pitch_stability=1 roll_stability=1 yaw_stability=1 elevator_trim_effectiveness=1 aileron_trim_effectiveness=1 rudder_trim_effectiveness=1 p_factor_on_yaw = 0 torque_on_roll = 0 gyro_precession_on_yaw = 1.0 gyro_precession_on_pitch = 1.0 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 10.000 system_type= 2 damaging-speed= 170.000 blowout-speed= 225.000 lift_scalar= 0.000 drag_scalar= 0.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 10.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 30.000, 0.000 flaps-position.4= 40.000, 0.000 flaps-position.5= 50.000, 0.000 [Flaps.1] type= 2 span-outboard= 0.500 extending-time= 10.000 system_type= 2 damaging-speed= 170.000 blowout-speed= 225.000 lift_scalar= 0.000 drag_scalar= 1.000 pitch_scalar= 0.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000 flaps-position.2= 5.000, 0.000 flaps-position.3= 15.000, 0.000 flaps-position.4= 30.000, 0.000 flaps-position.5= 50.000, 0.000 [Flaps.2] type= 2 span-outboard= 0.500 extending-time= 10.000 system_type= 2 damaging-speed= 170.000 blowout-speed= 225.000 lift_scalar= 1.000 drag_scalar= 0.000 pitch_scalar= 0.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 15.000, 0.000 flaps-position.2= 25.000, 0.000 flaps-position.3= 40.000, 0.000 flaps-position.4= 45.000, 0.000 flaps-position.5= 50.000, 0.000 [Radios] Audio.1=1 Com.1=1,0 Com.2=0,0 Nav.1=1,0,1 Nav.2=0,0,0 Adf.1=1,0 Transponder.1=1 Marker.1=1 [pitot_static] pitot_heat=1.000000 [vacuum_system] max_pressure=5.150000 vacuum_type=1 electric_backup_pressure=0.000000 engine_map=1,1,0,0 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=0.000000 [deice_system] structural_deice_type=0