[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