[fltsim.0]
title=Rutan Quickie
sim=Quickie
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=
atc_id_color=0x00000000
ui_manufacturer=Rutan
ui_type=Q1 Quickie
ui_variation=N54QK
description=Rutan Q1 Quickie
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
[fltsim.1]
title=Rutan Quickie Navy
sim=Quickie
model=
panel=
sound=
texture=navy
kb_checklists=
kb_reference=
atc_id=
atc_id_color=0x00000000
ui_manufacturer=Rutan
ui_type=Q1 Quickie
ui_variation=Navy
description=Rutan Q1 Quickie Navy
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
[CameraDefinition.0]
Title = "Tail"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description = Looking forward
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 1.2, 0.6, -4.0
InitialPbh = 0, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[General]
atc_type=Experimental
atc_model=J3
editable=0
performance="Maximum Speed\150 mph\n\nEngine\nRotax 503 50-hp air cooled\n\nService Ceiling\n11,500 ft\n\nMaximum Range\n190 mi\n\nFuel Capacity\n8 gal\n\nEmpty Weight\n269 lb \n\nGross Weight\n560 lb \n\n
Category=airplane
[weight_and_balance]
max_gross_weight = 560
empty_weight = 265
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 200
empty_weight_roll_MOI = 200
empty_weight_yaw_MOI = 500
empty_weight_coupled_MOI = 0
max_number_of_stations = 4
station_load.0 = 10, -2.16, 0, -0.96
station_load.1 = 0, 0, 0, 0
station_load.2 = 180, -1.02, 0, -0.51
station_load.3 = 0, -0.19, 0, 0
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar =1.0
min_throttle_limit = 0.0
engine.0 = 4.2, 0, 0
[effects]
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
windshield_rain_effect_available = 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 1
electric_pump=0
engine_driven_pump=1
Center1 = 1.85, 0, -1, 8, 0
//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]
static_pitch = 7
static_cg_height = 1.9
tailwheel_lock = 1
gear_system_type = 0
max_number_of_points = 8
point.0 = 1, -11.2, 0.000, -.30, 1200, 0, 0.21, 45, 0.1, 2.50, 0.9, 0, 0, 0, 0, 0
point.1 = 1, .80, -7.8, -2.2, 1600, 1, 0.6, 0, 0.25, 2.5, 0.8, 0, 0, 2, 0, 0
point.2 = 1, .80, 7.8, -2.2, 1600, 2, 0.6, 0, 0.25, 2.5, 0.8, 0, 0, 3, 0, 0
point.3 = 2, 4.25, 0, 1.7, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 4.25, 0, -1.7, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -3.25, 8.2,1.85, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, -3.25, -8.2, 1.85, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, -10.8, 0, 2.85, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
[keyboard_response]
elevator = 200, 1000
aileron = 200, 1000
rudder = 200, 1000
[forcefeedback]
ground_bumps_magnitude1 = 2600
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.6
ground_bumps_magnitude2 = 1200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.085
ground_bumps_slope2 = 0.65
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 3500000
[airplane_geometry]
wing_area = 54
wing_span = 16.8
wing_root_chord = 2.5
wing_dihedral = 3
wing_incidence = .4
wing_twist = 1.0
oswald_efficiency_factor = 0.7
wing_winglets_flag = 0
wing_sweep = 1
wing_pos_apex_lon = 1.11
wing_pos_apex_vert = -0.01
htail_area = 18.2
htail_span = 7.53
htail_pos_lon = -7.28
htail_pos_vert = 0.47
htail_incidence = 1.7
htail_sweep = 5
vtail_area = 13.0
vtail_span = 3.69
vtail_sweep = 32
vtail_pos_lon = -7.25
vtail_pos_vert = 0.62
elevator_area = 2.7
aileron_area = 2.4
rudder_area = 1
elevator_up_limit = 30.0
elevator_down_limit = 30.0
aileron_up_limit = 20.0
aileron_down_limit = 18.0
rudder_limit = 48.0
elevator_trim_limit = 10.0
spoiler_limit = 0.0
aileron_to_spoileron_gain = 0
spoiler_handle_available = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0
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
[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage =12.0
max_generator_alternator_amps = 60.0
starter1 = 0, 20, 10.0
avionics=0, 5 , 11.0
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=.9
induced_drag_scalar=.9
elevator_effectiveness=0.5
aileron_effectiveness=0.5
rudder_effectiveness=0.8
pitch_stability=1.4
roll_stability=1.0
yaw_stability=2.8
elevator_trim_effectiveness=0.7
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
p_factor_on_yaw = 0.1
torque_on_roll = 0.1
gyro_precession_on_yaw = 0.3
gyro_precession_on_pitch = 1.0
[Flaps.0]
type= 0
[piston_engine]
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=6.500
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=.8
cylinder_displacement= 18.75
two_stroke_cycle = 1
compression_ratio= 12.5
number_of_cylinders= 2
max_rated_rpm= 6500.000
max_rated_hp= 64.0
fuel_metering_type= 1
cooling_type= 1
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
power_scalar=1.000
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=1 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=4 //Propeller Diameter, (feet)
propeller_blades=3 //Number of propeller blades
propeller_moi=.3 //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=12.75 //13.75 //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
[brakes]
parking_brake = 0 //Parking brake available
toe_brakes_scale = 0.8 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint=-1.65, 0.000, 1.65
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=0
Com.1=1, 1
Nav.1=0, 0, 0
Adf.1=0
Transponder.1=1
Marker.1=0
[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=0,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 0
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[Reference Speeds]
flaps_up_stall_speed=50 //Knots True (KTAS)
full_flaps_stall_speed=24.33 //Knots True (KTAS)
cruise_speed=120 //Knots True (KTAS)
max_indicated_speed= 150 //Red line (KIAS)
[autopilot]
autopilot_available=0
flight_director_available=0
[stall_warning]
type=1
stick_shaker=0
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0
