[fltsim.0]
title=Mini-Max
sim=Mini_Max
model=
panel=
sound=
texture=
kb_checklists=MiniMax_check
kb_reference=MiniMax_ref
atc_id=
atc_id_color=0x00000000
ui_manufacturer=Flight Replicas
ui_type=Mini-Max
ui_variation=C-ILFR
description=\n
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\n100 mph\n\nEngine\nRotax 447 40-hp air cooled\n\nService Ceiling\n11,500 ft 3,505 m\n\nMaximum Range\n190 mi 306 km\n\nFuel Capacity\n10 gal 45.4 L\n\nEmpty Weight\n269 lb \n\nGross Weight\n560 lb \n\n
Category=airplane
[weight_and_balance]
max_gross_weight = 560
empty_weight = 269
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 89
empty_weight_roll_MOI = 89
empty_weight_yaw_MOI = 149
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 = 220, -1.02, 0, -0.51
station_load.3 = 0, -0.19, 0, 0
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 0.8
min_throttle_limit = 0.0
engine.0 = 4.46, 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=1
engine_driven_pump=0
Center1 = 1.85, 0, 0, 10, 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 = 11.7
static_cg_height = 3.02
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 8
point.0 = 1, -11.2, 0.000, -1.40, 1200, 0, 0.21, 180, 0.1, 2.50, 0.9, 0, 0, 0, 0, 0
point.1 = 1, 0.6571, -2.1435, -3.8, 1600, 1, 0.6, 0, 0.25, 2.5, 0.8, 0, 0, 2, 0, 0
point.2 = 1, 0.665, 2.1535, -3.8, 1600, 2, 0.6, 0, 0.25, 2.5, 0.8, 0, 0, 3, 0, 0
point.3 = 2, 0.9779, -12.4764, 0.4792, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 0, 0.459, 0, 0.2214, 0, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.5 = 2, 0.9925, 12.4764, 0.5026, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.6 = 2, -11.4391, 0, 0.4514, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.7 = 2, 4.0942, 0, -1.2851, 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 = 112.5
wing_span = 25
wing_root_chord = 4.57
wing_dihedral = 3
wing_incidence = 1.0
wing_twist = 1.0
oswald_efficiency_factor = 0.9
wing_winglets_flag = 0
wing_sweep = 0
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 = -0.8
htail_sweep = 34
vtail_area = 13.0
vtail_span = 3.69
vtail_sweep = 32
vtail_pos_lon = -7.25
vtail_pos_vert = 0.62
elevator_area = 10.64
aileron_area = 5.6
rudder_area = 6.55
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]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
additional_system = 0, 2 , 17.0
starter1 = 0, 20, 17.0
fuel_pump = 0, 5 , 17.0
[flight_tuning]
cruise_lift_scalar=1.2
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=0.8
aileron_effectiveness=0.6
rudder_effectiveness=0.8
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
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 = 0.3
[Flaps.0]
type= 0
[piston_engine]
power_scalar=1.0 //Piston power scalar
cylinder_displacement=26.625 //Cubic inches per cylinder
compression_ratio=6.3 //Compression ratio
number_of_cylinders=2 //Number of cylinders
max_rated_rpm=2350 //Max rated RPM
max_rated_hp=44 //Max rated HP
fuel_metering_type=1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=1.5 //Starter torque factor
turbocharged=0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=0 //Max design manifold pressure, (inHg)
min_design_mp=0 //Min design manifold pressure, (inHg)
critical_altitude=0 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset=0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar=0.2 //Scalar on idle RPM friction
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=1 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=5 //Propeller Diameter, (feet)
propeller_blades=2 //Number of propeller blades
propeller_moi=0.26 //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=20 //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 = 1 //Parking brake available
toe_brakes_scale = 0.5 //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=-1.73, 0.000, 1.35
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=0
Com.1=1, 0
Nav.1=0, 0, 0
Adf.1=0
Transponder.1=0
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=26.93 //Knots True (KTAS)
full_flaps_stall_speed=24.33 //Knots True (KTAS)
cruise_speed=56.48 //Knots True (KTAS)
max_indicated_speed= 86.89 //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
