[fltsim.0] title=Fokker DR1 "Red Baron" sim=Trip2 model= panel= sound= texture= kb_checklists= description=On the 21st April 1918 at 10:45am Manfred Von Richthofen (The Red Baron) met his death in the triplane depicted here, killed by a single .303 calibre bullet through the heart. ui_manufacturer=Fokker ui_type=DR1 Triplane ui_variation=The Red Baron atc_heavy=0 atc_id= atc_airline= atc_flight_number= [General] atc_type=FOKKER atc_model= editable=1 performance=Maximum speed:- 120mph.\nEndurance:- 1 hour 30 mins\nCeiling:- 20,000 ft\nInitial climb:- 800ft per minute.\nArmament:- 2 Spandau 7.92mm Machine guns.\n Category=airplane [WEIGHT_AND_BALANCE] max_gross_weight= 2766.000 empty_weight= 2500.000 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 ;Moments of Inertia empty_weight_pitch_MOI= 1346.000 empty_weight_roll_MOI= 948.000 empty_weight_yaw_MOI= 1967.000 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.750 aileron_effectiveness=2.002 rudder_effectiveness=1.750 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [GeneralEngineData] engine_type= 0 Engine.0= 6.300, 0.000, 0.500 fuel_flow_scalar= 0.900 min_throttle_limit=0.000000 [piston_engine] power_scalar=1.000 cylinder_displacement= 66.000 compression_ratio= 2.700 number_of_cylinders= 9 max_rated_rpm= 3000.000 max_rated_hp= 120.000 fuel_metering_type= 1 cooling_type= 0 normalized_starter_torque= 0.300 turbocharged= 1 max_design_mp= 42.000 min_design_mp= 1.000 critical_altitude= 10000.000 emergency_boost_type= 0 emergency_boost_mp_offset= 0.000 emergency_boost_gain_offset= 0.000 fuel_air_auto_mixture= 0 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 [propeller] thrust_scalar=1.000 propeller_type= 1 propeller_diameter= 10.000 propeller_blades= 2 propeller_moi= 20.000 beta_max= 31.800 beta_min= 17.000 min_gov_rpm= 1800.000 prop_tc= 0.100 gear_reduction_ratio= 2.000 fixed_pitch_beta= 30.000 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 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 //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 prop_reverse_available= 0 [contact_points] point.0= 1.000, -14.220, 0.000, -0.620, 1181.100, 0.000, 0.519, 30.000, 0.304, 2.500, 0.695, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, 0.810, -2.900, -5.950, 1574.800, 0.000, 0.519, 0.000, 0.304, 2.500, 0.686, 0.000, 0.000, 2.000, 0.000, 0.000 point.2= 1.000, 0.810, 2.890, -5.950, 1574.800, 0.000, 0.519, 0.000, 0.304, 2.500, 0.682, 0.000, 0.000, 3.000, 0.000, 0.000 point.3 = 2.000, -14.216, 0.003, -0.620, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000 point.4 = 2.000, 4.045, 0.003, -0.511, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000 point.5 = 2.000, -0.756, 10.043, -1.885, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000 point.6 = 2.000, -0.756, -9.803, -1.885, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000 point.7 = 0.81, 2.89, -5.95, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.8 = 0.81, -2.90, -5.95, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.9 = -14.22, 0.00, -0.62, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 static_pitch = 19.523 static_cg_height= 3.284 [Views] eyepoint= -4.08, 0.00, 2.81 //(feet) longitudinal, lateral, vertical distance from reference datum [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=0 Com.1=0, 0 Nav.1=0, 0, 0 Adf.1=0 Transponder.1=0 Marker.1=0 [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=200, 1000 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=3,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [electrical] max_battery_voltage=0 generator_alternator_voltage=0 [fuel] LeftMain= 0.000, 0.000, 0.000, 20.000, 0.000 RightMain= 0.000, 0.000, 0.000, 20.000, 0.000 fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area= 220.000 wing_span= 28.000 wing_root_chord= 6.000 wing_dihedral= 1.000 wing_incidence= 1.000 wing_twist= -1.000 oswald_efficiency_factor= 0.800 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 1.200 wing_pos_apex_vert= 0.000 htail_area= 50.000 htail_span= 11.700 htail_pos_lon= -14.700 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 18.000 vtail_span= 4.800 vtail_sweep= 0.000 vtail_pos_lon= -12.600 vtail_pos_vert= 0.000 elevator_area= 16.600 aileron_area= 18.300 rudder_area= 6.700 elevator_up_limit= 28.000 elevator_down_limit= 21.000 aileron_up_limit= 20.000 aileron_down_limit= 15.000 rudder_limit= 24.000 elevator_trim_limit= 19.500 spoiler_limit= 0.000 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 auto_spoiler_available=0 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-1.500000 negative_g_limit_flaps_down=-1.500000 [Reference Speeds] flaps_up_stall_speed= 40.000 full_flaps_stall_speed= 38.000 cruise_speed= 99.000 max_indicated_speed=180.000000 [autopilot] autopilot_available=0 flight_director_available=0 [forcefeedback] ground_bumps_magnitude1=2600 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.6 ground_bumps_magnitude2=1200 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.085 ground_bumps_slope2=0.65 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=3500000 ; in microseconds [Flaps.0] type= 1 span-outboard= 0.750 extending-time= 2.000 system_type= 4 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 2.000 drag_scalar= 3.000 pitch_scalar= 0.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 20.000, 0.000 [brakes] toe_brakes_scale=0.000000 parking_brake=0 [pitot_static] pitot_heat=0.000000 [hydraulic_system] normal_pressure=0.000000 [vacuum_system] max_pressure=5.150000 vacuum_type=0 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=1.000000 [stall_warning] type=0 stick_shaker=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [deice_system] structural_deice_type=0
