[fltsim.0] title=Gee Bee R-1 sim=SingleEnginePropHP model= panel= sound= texture= panel_alias = mooney_bravo\panel sound_alias = mooney_bravo\sound kb_checklists= kb_reference= atc_id=NSEHP ui_manufacturer=Granville Brothers ui_type=GeeBee ui_variation= description=Built by the Granville Brothers Aircraft Company 1932. Used as a fast racer & being notoriously difficult to fly - this aircraft claimed many lives. visual_damage=1 [General] atc_type= atc_model= editable=0 performance=Enter your performance information here. [WEIGHT_AND_BALANCE] max_gross_weight = 2350 // (pounds) empty_weight = 1800 // (pounds) reference_datum_position = 0.7, 0, 0.7 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 0.2, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 20 station_load.0 = 170, -4.4, 0.0, 1.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = 400, 2.5, 0.0, 0.0 ;Moments of Inertia empty_weight_pitch_MOI = 570 empty_weight_roll_MOI = 513 empty_weight_yaw_MOI = 593 empty_weight_coupled_MOI = 0.0 [pitot_static] vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI [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 = 0.3 pitch_stability = 1.0 roll_stability = 0.5 yaw_stability = 0.01 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [flaps.0] //Trailing Edge Flaps type = 0 // 1 - tail, 2 - lead system_type = 4 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [GeneralEngineData] engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 2.1, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar= 1.0 //Fuel flow scalar [piston_engine] power_scalar = 1.0 //Piston power scalar cylinder_displacement=130.3 //Cubic inches per cylinder compression_ratio= 6.0 //Compression ratio number_of_cylinders=9 //Number of cylinders max_rated_rpm= 3575 //Max rated RPM max_rated_hp= 775 //Max rated HP fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter 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= 38 //Max design manifold pressure, (inHg) min_design_mp= 1 //Min design manifold pressure, (inHg) critical_altitude= 18000 //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= 5 //Propeller Diameter, (feet) propeller_blades= 2 //Number of propeller blades propeller_moi= 6.0 //Propeller moment of inertia beta_max= 43 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 15 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm= 800 //Miminum governed RPM prop_tc= 0.1 //Prop time-constant gear_reduction_ratio= 1.0 //Propeller gear reduction ratio fixed_pitch_beta= 0 //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= 1 //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 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) [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus = 0, 10, 17.0 additional_system = 0, 20, 17.0 fuel_pump = 0, 5 , 17.0 starter1 = 0, 20, 17.0 //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 [contact_points] // FORE LEFT UP ROD BRAKE WH RA STANG SCOM C/R DR EXT RET ST AL D/AS point.0= 3, -8.0, 0.0, -2.9, 1180.0, 0, 0.115, 31.0, 0.388, 2.5, 0.835, 0.0, 0.0, 0.0, 0.0, 0.0 //TAIL point.1= 1, 1.0, -2.5, -4.4, 1574.0, 0, 0.765, 0.0, 0.428, 2.5, 0.750, 0.0, 0.0, 2.0, 0.0, 0.0 //LEFT point.2= 1, 1.0, 2.5, -4.4, 1574.0, 0, 0.765, 0.0, 0.428, 2.5, 0.750, 0.0, 0.0, 3.0, 0.0, 0.0 //RIGHT point.3= 2, -1.5, -14.4, -1.0, 787.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0 //LWS point.4= 2, -1.5, 14.4, -1.0, 787.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0 //RWS point.5= 2, 6.0, 0.0, -2.5, 787.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9.0, 0.0, 0.0 //TS max_number_of_points = 21 static_pitch =13.84 static_cg_height = 2.5 [Views] eyepoint = -4.2, 0.0, 1.6 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator = 140, 240 aileron = 200, 1000 rudder = 200, 1000 [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain = -4.1, -7.9, -0.8, 47.5, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -4.1, 7.9, -0.8, 47.5, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 [airplane_geometry] wing_area = 80.0 //Square feet wing_span = 25.0 //Feet wing_root_chord = 3.1 //Feet wing_dihedral = 0.0 //Degrees wing_incidence = 0.0 //Degrees wing_twist = 0.0 //Degrees oswald_efficiency_factor= 0.6 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 0.0 //Degrees, wing leading edge wing_pos_apex_lon = -0.6 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up htail_area = 9.0 //Square feet htail_span = 11.8 //Feet htail_pos_lon = -6.6 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 0.8 //Feet, vertical distance from reference point, positive going up htail_incidence = 0.0 //Degrees htail_sweep = 5.0 //Degrees, horizontal tail leading edge vtail_area = 5.0 //Square feet vtail_span = 3.6 //Feet, tip to body vtail_sweep = 15.0 //Degrees, vertical tail leading edge vtail_pos_lon = -6.5 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 1.5 //Feet, vertical distance from reference point, positive going up elevator_area = 7.6 //Square feet aileron_area = 18.3 //Square feet rudder_area = 1.7 //Square feet elevator_up_limit = 28.0 //Degrees elevator_down_limit = 21.0 //Degrees aileron_up_limit = 20.0 //Degrees aileron_down_limit = 15.0 //Degrees rudder_limit = 24.0 //Degrees elevator_trim_limit = 19.5 //Degrees spoiler_limit = 0.0 //Degrees spoilerons_available = 0 //Spoilerons Available? aileron_to_spoileron_gain = 0 //Aileron to spoileron gain min_ailerons_for_spoilerons = 0 //Degrees min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed = 100.0 //Knots True (KTAS) cruise_speed = 270.0 //Knots True (KTAS) full_flaps_stall_speed = 100.0 [autopilot] autopilot_available=0 flight_director_available= 0 default_vertical_speed= 1000.0 autothrottle_available= 0 pitch_takeoff_ga=8.000000 [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 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 [Flaps.0] type=1 span-outboard=0.500000 extending-time=7.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=16.501184,0.000000 flaps-position.2=33.002369,0.000000