[fltsim.0] title=Otto C.I sim=Otto_CI model= panel= sound= texture= checklists= ui_manufacturer=Aerowerke Gustav Otto ui_type=Otto C.I ui_variation=Aufklärer kb_reference=Otto_CI_ref description=Notes: Wooden twin-boom pusher biplane, preceding the AGO C.I-III Series, built by Gustav Otto in 1915, with tail-booms and fuselage-gondola in box-shaped cross-section. The specification 150 hp Benz Bz.III engine produced 165 hp at 1420 rpm at sea level. [General] performance=One 172 hp 6-cyl Mercedes D.III pusher\nCruise climb at full throttle\nTrim with throttle\nReduce rpm to obtain level flight\n [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 [General] performance=Length: 29.5 ft\nSpan: 49.15 ft Area: 447 sq ft\nMTOW: 2094lbs\nNet weight: 1760 lb\nPower: 1 x 165 hp Benz III\nRange: 340 mi . Cieling: 16000 ft\nDate: Sept 2008\nDetails:\nDesigner: Stephan Scholz [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=2160.000000 empty_weight_roll_MOI=36000.000000 empty_weight_pitch_MOI=45000.000000 empty_weight_yaw_MOI=60000.000000 empty_weight_coupled_MOI=0.000000 [fuel] LeftMain=0.000000,-10.000000,0.000000,50.000000,0.000000 RightMain=0.000000,10.000000,0.000000,50.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=447.000000 wing_span=49.1500000 wing_root_chord=12.00000 wing_dihedral=2.801514 wing_incidence=4.498901 wing_twist=0.000000 oswald_efficiency_factor=0.6 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=160.000000 htail_span=22.500000 htail_pos_lon=-35.583333 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=102.000000 vtail_span=11.515207 vtail_sweep=0.000000 vtail_pos_lon=-35.666667 vtail_pos_vert=4.000000 elevator_area=71.810000 aileron_area=102.900000 rudder_area=33.950000 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 [contact_points] point.0=1.000000,9.500000,0.000000,-6.333333,1574.803150,0.000000,0.519133,0.000000,0.093508,2.500000,2.044803,5.000000,5.000000,0.000000,0.000000,0.000000 point.1=1.000000,-0.666667,-3.833333,-6.916667,1574.803150,1.000000,0.519133,0.000000,0.423067,2.500000,0.915666,5.000000,5.000000,2.000000,0.000000,0.000000 point.2=1.000000,-0.666667,3.833333,-6.916667,1574.803150,2.000000,0.519133,0.000000,0.423067,2.500000,0.915666,5.000000,5.000000,3.000000,0.000000,0.000000 point.3=2.000000,-1.666667,-36.000000,-0.416667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,-1.666667,36.000000,-0.416667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-20.833333,0.000000,0.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,6.750000,0.000000,-0.416667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 point.7=2.000000,-19.250000,0.000000,-2.250000,3003.698634,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,7.000000,0.000000,0.000000 static_pitch=0.000000 static_cg_height=6.642034 [GeneralEngineData] engine_type=0 Engine.0=0.0,-0.0,0.500000 fuel_flow_scalar=1.1 ;including oil consumption [piston_engine] ;1 x 150Hp Benz Bz.III class 3 engines combat rated at 165hp at 1420 rpm ; cylinder_displacement=145.7 ;huge cylinders compression_ratio=4.5 number_of_cylinders=6 max_rated_rpm=1420 max_rated_hp=165 ;combat rating fuel_metering_type=1 cooling_type=0 normalized_starter_torque=0.300000 turbocharged=0 max_design_mp=0.0 min_design_mp=0.0 critical_altitude=0.0 emergency_boost_type=0 emergency_boost_mp_offset=0.0 emergency_boost_gain_offset=0.0 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.0 idle_rpm_mechanical_efficiency_scalar=1.0 max_rpm_friction_scalar=1.0 idle_rpm_friction_scalar=1.0 [propeller] propeller_type=1 propeller_diameter=8.25 propeller_blades=2 propeller_moi=8.7 beta_max=25 beta_min=25 min_gov_rpm=1400.0 prop_tc=0.100000 gear_reduction_ratio=1.0 fixed_pitch_beta=25.0 low_speed_theory_limit=80.0 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.0 beta_feather=0.0 power_absorbed_cf=0.0 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.0 minimum_reverse_beta=0.0 [Reference Speeds] flaps_up_stall_speed=30.000000 full_flaps_stall_speed=24.000000 cruise_speed=72.273380 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=3.498708,0.000000,1.076526 [autopilot] autopilot_available=0 flight_director_available=0 [direction_indicators] direction_indicator.0=1,0