[fltsim.0] title=Bleriot TYpe XI sim=bleriot model= panel= sound= texture= checklists= atc_id=XI ui_manufacturer=Bleriot ui_type=Type XI description=Louis Bleriot made aviation history in flying his Type XI across La Manche (known as the English Channel on the other side) on July 25, 1909. He left Sangatte, France, at 4:35 a.m. and landed on Northfall Meadow near Dover, England, at 5:12 a.m. [forcefeedback] gear_bump_nose_magnitude=6000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=6000 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=6000 gear_bump_right_direction=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [fltsim.1] title= sim= panel= sound= texture= model= [fltsim.2] title= sim= panel= sound= texture= model= [fltsim.3] title= sim= panel= sound= texture= model= [fltsim.4] title= sim= panel= sound= texture= model= [fltsim.5] title= sim= panel= sound= texture= model= [fltsim.6] title= sim= panel= sound= texture= model= [fltsim.7] title= sim= panel= sound= texture= model= [fltsim.8] title= sim= panel= sound= texture= model= [fltsim.9] title= sim= panel= sound= texture= model= [General] performance=Length:8.00m\Span:7.80m\nWeight:210kg\nPower:22/25hp\nSpeed:58kph\nDesigner:Dennis Simanaitis [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 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=463.000000 empty_weight_roll_MOI=2500.000000 empty_weight_pitch_MOI=3200.000000 empty_weight_yaw_MOI=4000.000000 empty_weight_coupled_MOI=0.000000 [fuel] Center1=2.5,0.000000,0.000000,15.8500000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=150.000000 wing_span=25.58333 wing_root_chord=6.58333 wing_dihedral=2.999268 wing_incidence=0.000000 wing_twist=-0.999756 oswald_efficiency_factor=3.225327 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=27.000000 htail_span=9.0 htail_pos_lon=-13.2 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=11.000000 vtail_span=2.92 vtail_sweep=0.000000 vtail_pos_lon=-13.2 vtail_pos_vert=0.000000 elevator_area=12.5 aileron_area=18.300000 rudder_area=7.25 elevator_up_limit=28.000447 elevator_down_limit=20.998903 aileron_up_limit=19.996227 aileron_down_limit=15.000035 rudder_limit=23.995472 elevator_trim_limit=19.497754 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 [contact_points] point.0=1.000000,-7.5,0.000000,-3.4,1574.803150,0.000000,0.507127,36.840000,0.391257,2.00000,0.585862,0.000000,0.000000,0.000000,0.000000,0.000000 point.1=1.000000,4.9,-2.250000,-4.65,1574.803150,1.000000,0.507127,0.000000,0.393055,2.00000,0.585849,0.000000,0.000000,2.000000,0.000000,0.000000 point.2=1.000000,4.9,2.250000,-4.65,1574.803150,2.000000,0.507127,0.000000,0.393055,2.00000,0.585849,0.000000,0.000000,3.000000,0.000000,0.000000 point.3=2.000000,0.000000,-17.916667,2.083333,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,0.000000,17.916667,2.083333,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-13.000000,0.000000,3.333333,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,2.416667,0.000000,-2.166667,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=5.0 static_cg_height=3.8 [GeneralEngineData] engine_type=0 Engine.0=4.8,0.000000,0.000000 fuel_flow_scalar=1.000000 [piston_engine] max_rpm_mechanical_efficiency_scalar=1.000000 idle_rpm_mechanical_efficiency_scalar=3.000000 max_rpm_friction_scalar=1.000000 idle_rpm_friction_scalar=.500000 cylinder_displacement=20.852 compression_ratio=8.000000 number_of_cylinders=3 max_rated_rpm=2400.000000 max_rated_hp=22.000000 fuel_metering_type=1 cooling_type=0 normalized_starter_torque=0.300000 turbocharged=0 max_design_mp=0.000000 min_design_mp=0.000000 critical_altitude=0.000000 emergency_boost_type=0 emergency_boost_mp_offset=0.000000 emergency_boost_gain_offset=0.000000 fuel_air_auto_mixture=0 auto_ignition=0 [propeller] propeller_type=1 propeller_diameter=6.600000 propeller_blades=2 propeller_moi=3.000 beta_max=5.565217 beta_min=15.000000 min_gov_rpm=1400.000000 prop_tc=0.100000 gear_reduction_ratio=1.000000 fixed_pitch_beta=20.000000 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 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [Reference Speeds] flaps_up_stall_speed=25.000000 full_flaps_stall_speed=25.0 cruise_speed=45.0 [keyboard_response] elevator=200.000000,1000.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [Views] eyepoint=0.0,0.0,0.0 [autopilot] autopilot_available=0 flight_director_available=0 [direction_indicators] direction_indicator.0=1,0