[fltsim.0]
title=110 Clipwing Special
sim=110 Clipwing Special
panel=
model=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Monocoupe
ui_type=
ui_variation=110 Special
Description=Monocoupes were the most successful of all the stock plane racers during the Golden Age of Air Racing. They were consistent winners in the ATC classes (for certified aircraft)and often moved up to higher cubic inch classes and beat more powerful airplanes and even specialized racers.By the early 1930s, the Monocoupe was being promoted as an economical, easy to fly flight school trainer, with an average price of $4,750. Three models were produced, differing only in horsepower of engines - 60, 90 and 110.The fastest of all Monocoupes was the 110 Special , or "Clipwing" as it was commonly known.With a 23 foot wing span (compared to the original 32 foot span), new tail section with less area and span, smaller wheels, a new windshield, and a 185 hp Warner. The coupe could reach speeds of 220 mph.
[fltsim.1]
title=110 Clipwing Special Venezuela
sim=110 Clipwing Special
panel=
model=
sound=
texture=venezuela
kb_checklists=
kb_reference=
atc_id=marru
ui_manufacturer=Monocoupe
ui_type=
ui_variation=110 Special Venezuela
Description=Monocoupes were the most successful of all the stock plane racers during the Golden Age of Air Racing. They were consistent winners in the ATC classes (for certified aircraft)and often moved up to higher cubic inch classes and beat more powerful airplanes and even specialized racers.By the early 1930s, the Monocoupe was being promoted as an economical, easy to fly flight school trainer, with an average price of $4,750. Three models were produced, differing only in horsepower of engines - 60, 90 and 110.The fastest of all Monocoupes was the 110 Special , or "Clipwing" as it was commonly known.With a 23 foot wing span (compared to the original 32 foot span), new tail section with less area and span, smaller wheels, a new windshield, and a 185 hp Warner. The coupe could reach speeds of 220 mph. Repaint by Gustavo Zapata Wainberg.
[General]
atc_type=
atc_model=
editable=0
performance=maximum speed, 240 mph cruise speed, 175 mph stall speed, 68 mph range 500 miles
[WEIGHT_AND_BALANCE]
max_gross_weight=1350.000
empty_weight=940.000
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=170.000000,0.000000,0.000000,0.000000
station_load.1=170.000000,0.000000,0.000000,0.000000
;Moments of Inertia
empty_weight_pitch_MOI=2300.000
empty_weight_roll_MOI=1837.000
empty_weight_yaw_MOI=1860.000
empty_weight_coupled_MOI=0.000
CG_forward_limit=0.000
CG_aft_limit=1.000
[exits]
number_of_exits=2
exit_rate.0=0.2
[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=0.500
rudder_effectiveness=1.000
pitch_stability=0.800
roll_stability=0.400
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=7.000, 0.000, 0.500
fuel_flow_scalar=1.000
min_throttle_limit=0.000000
[piston_engine]
power_scalar=1.000
cylinder_displacement=60
compression_ratio=6.800
number_of_cylinders=7
max_rated_rpm=2500.000
max_rated_hp=160.000
fuel_metering_type=2
cooling_type=0
normalized_starter_torque=0.300
turbocharged=0
max_design_mp=0.000
min_design_mp=0.000
critical_altitude=0.000
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=2.000
idle_rpm_mechanical_efficiency_scalar=1.200
max_rpm_friction_scalar=0.700
idle_rpm_friction_scalar=0.800
[propeller]
thrust_scalar = 1.0 //Propeller thrust scalar
propeller_type= 1 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 7.5 //Propeller Diameter, (feet)
propeller_blades= 2 //Number of propeller blades
propeller_moi= 3.8 //Propeller moment of inertia
beta_max= 0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 0 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.0 //Propeller gear reduction ratio
fixed_pitch_beta= 17 //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= 0 //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 in feather
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)
//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]
point.0=1, -9.000, 0.000, -0.60, 1181.100, 0.000, 0.519, 50.000, 0.304, 2.500, 1.000, 0.000, 0.000, 0.000, 0.000, 0.000
point.1=1, 2.000, -2.500, -3.15, 1574.800, 1.000, 0.519, 0.000, 0.304, 2.500, 1.000, 0.000, 0.000, 2.000, 0.000, 0.000
point.2=1, 2.000, 2.500, -3.15, 1574.800, 2.000, 0.519, 0.000, 0.304, 2.500, 1.000, 0.000, 0.000, 3.000, 0.000, 0.000
point.3=2, 0.000, -17.900, -1.5, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4=2, 0.000, 17.900, -1.5, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5=2, -13.000, 0.000, 3.300, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6=2, 2.400, 0.000, -2.200, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = 12.0
static_cg_height = 2.6
[Views]
eyepoint=4.2, -1.0, 3.0
[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1
Nav.1=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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=4, -0.00, 0.00, 0.35, fx_vclightwhi
[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=2,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[SMOKESYSTEM]
smoke.0=0.00, -0.70, 1.40, fx_smoke_w
[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
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
light_panel=0, 5 , 17.0
[fuel]
Center1=0.000, 0.000, 0.000, 25.000, 0.000
fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=129.000
wing_span=21.650
wing_root_chord=4.000
wing_dihedral=1.000
wing_incidence=0.000
wing_twist=-1.000
oswald_efficiency_factor=0.500
wing_winglets_flag=0
wing_sweep=11.000
wing_pos_apex_lon=1.200
wing_pos_apex_vert=0.000
htail_area=22.000
htail_span=8.200
htail_pos_lon=-13.000
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=0.000
vtail_area=12.000
vtail_span=3.800
vtail_sweep=0.000
vtail_pos_lon=-13.000
vtail_pos_vert=0.000
elevator_area=10.000
aileron_area=20.000
rudder_area=10.000
elevator_up_limit=20.000
elevator_down_limit=20.000
aileron_up_limit=30.000
aileron_down_limit=20.000
rudder_limit=17.000
elevator_trim_limit=20.000
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
[Reference Speeds]
flaps_up_stall_speed=68.000
full_flaps_stall_speed=68.000
cruise_speed=175.000
max_indicated_speed=240.0000
[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=0
[brakes]
toe_brakes_scale=0.80000
parking_brake=1
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=0
[attitude_indicators]
attitude_indicator.0=0
[turn_indicators]
turn_indicator.0=0
