//alphasim FS2002 Bristol Bulldog Mk IIA, Version 1.0 [fltsim.0] title=ALPHA Bristol Bulldog IIA sim=Bulldog IIA model= panel= sound= texture= checklists= atc_id=BDOG ui_manufacturer=ALPHA ui_type=Bristol Bulldog IIA ui_variation=32 Sqn. RAF description=© ALPHA Simulations 2002\n\nBristol Bulldog IIA\n\nFirst flown in 1928, the Bulldog II beat all the competitors and became the new standard RAF fighter of the 1930's. 312 were supplied to the RAF and 131 were exported, mainly to Scandinavia and the Baltic Republics. The Bulldog was tremendously manouverable but suffered from a low top speed and tricky landing characteristics. Bulldogs remained in squadron service until 1938, when it was replaced by the Gladiator and Hurricane.\n\n \n [General] atc_type=BIPLANE performance=Model Designer : Chris Lampard\nPanel : Phil Perrott\nFlight model : Larry Vrooman\n\nLength: 25 feet\nWing span: 33 feet 10 ins.\nEmpty Weight: 2,412 lbs.\nLoaded Weight: 3,530 lbs.\nPower: 440 h.p. (T\/O) Bristol Jupiter VIIF\nMax level Speed: 178 m.p.h. at 10,000 ft.\nTime to Climb: 14.5 mins. to 20,000 feet\nCeiling: 26, 994 ft.\nRange: 350 miles\nArmament: 2 x Vickers 0.303 ins. MG\n\n [WEIGHT_AND_BALANCE] reference_datum_position = 0.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0.000000,0.000000,0.000000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=2412.000000 empty_weight_roll_MOI=8000.000000 empty_weight_pitch_MOI=12000.000000 empty_weight_yaw_MOI=18000.000000 empty_weight_coupled_MOI=0.000000 max_gross_weight=3618.000000 [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 [fuel] Center1= 0.30, 0.00, 1.18, 22.8, 0.0 fuel_type=1 number_of_tank_selectors=1 electric_pump=1 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 startup=fx_engstrt [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=4, -2.30, 0.00, 1.70, fx_vclight [SMOKESYSTEM] smoke.0=-1.55, -3.00, 10.00, fx_smoke_w smoke.1=-1.55, -3.00, -10.00, fx_smoke_w [contact_points] point.0=1, -15.08, 0.00, -2.00, 1600,0,0.507,20.0,0.300,2.50,1.613,0.0,0.0,0 point.1=1, 1.25, -3.00, -5.40, 1600,1,0.507, 0.0,0.300,2.50,0.987,0.0,0.0,2 point.2=1, 1.25, 3.00, -5.40, 1600,2,0.507, 0.0,0.300,2.50,0.987,0.0,0.0,3 point.6=2, 5.70, 0.00, -4.20, 1600,0,0.000, 0.0,0.000,0.00,0.000,0.0,0.0,4 point.3=2, -0.92,-13.83, -0.83, 1600,0,0.000, 0.0,0.000,0.00,0.000,0.0,0.0,5 point.4=2, -0.92, 13.83, -0.83, 1600,0,0.000, 0.0,0.000,0.00,0.000,0.0,0.0,6 point.7=2, 0.00,-17.00, 4.40, 1600,0,0.000, 0.0,0.000,0.00,0.000,0.0,0.0,7 point.8=2, 0.00, 17.00, 4.40, 1600,0,0.000, 0.0,0.000,0.00,0.000,0.0,0.0,8 point.5=2, -15.10, 0.00, -1.20, 1600,0,0.000, 0.0,0.000,0.00,0.000,0.0,0.0,9 static_pitch = 14.00 //degrees (pitch when loaded on ground) static_cg_height=4.900 //feet, altitude of CG when at rest on the ground gear_system_type=0 [Views] eyepoint= -3.00, 0.00, 2.75 //(feet) longitudinal, lateral, vertical distance from reference datum [airplane_geometry] wing_area=306.000000 wing_span=33.833333 wing_root_chord=9.083333 wing_dihedral=2.999268 wing_incidence=0.999756 wing_twist=0.000000 oswald_efficiency_factor=0.534660 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=51.000000 htail_span=11.000000 htail_pos_lon=-14.166667 htail_pos_vert=0.000000 htail_incidence=0.499878 htail_sweep=0.000000 vtail_area=31.000000 vtail_span=6.348228 vtail_sweep=0.000000 vtail_pos_lon=-15.000000 vtail_pos_vert=0.583333 elevator_area=8.600000 aileron_area=8.700000 rudder_area=10.250000 elevator_up_limit=27.501974 elevator_down_limit=20.626481 aileron_up_limit=19.480565 aileron_down_limit=14.896903 rudder_limit=23.491270 elevator_trim_limit=19.480565 spoiler_limit=59.988681 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [Flaps.0] type=1 span-outboard=0.500000 extending-time=0.000000 system_type=0 flaps-position.0=0.000000,0.000000 [GeneralEngineData] engine_type=0 Engine.0= 5.583, 0.000, 0.000 fuel_flow_scalar=1.0 min_throttle_limit=0.0 [piston_engine] power_scalar = 1.0 //Piston power scalar cylinder_displacement= 184.4 //Cubic inches per cylinder compression_ratio= 5.0 //Compression ratio number_of_cylinders=9 //Number of cylinders max_rated_rpm= 2000 //Max rated RPM max_rated_hp= 520 //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= 0 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp= 0 //Max design manifold pressure, (inHg) min_design_mp= 0 //Min design manifold pressure, (inHg) critical_altitude= 0 //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= 1 //0=Constant Speed, 1=Fixed Pitch propeller_diameter= 8.6 //Propeller Diameter, (feet) propeller_blades= 2 //Number of propeller blades propeller_moi= 12.3 //Propeller moment of inertia beta_max= 0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm= 1400 //Miminum governed RPM prop_tc= 0.0 //Prop time-constant gear_reduction_ratio= 1.0 //Propeller gear reduction ratio fixed_pitch_beta= 25 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit= 80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available= 0 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available= 0 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available= 0 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather= 0 //Minimum RPM for prop feathering beta_feather= 0 //Feathering pitch angle (degrees) power_absorbed_cf= 0 //Coefficient of friction for power absorbed by propeller by feathered prop 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 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta= 0 //Minimum pitch angle in reverse, (degrees) [Reference Speeds] flaps_up_stall_speed=50.0 full_flaps_stall_speed=40.0 cruise_speed=118.0 max_indicated_speed=163.0 [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [autopilot] autopilot_available=0 [direction_indicators] direction_indicator.0=1,0 [brakes] toe_brakes_scale=1.0 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] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
