[fltsim.0]
title=MAG Basis-15
sim=Glider
model=
panel=
sound=
texture=
panel_alias = schweizr\panel
sound_alias = schweizr\sound
kb_checklists=Basis15
kb_reference=
atc_id=NGLDR
ui_manufacturer=MAG
ui_type=Basis 15
ui_variation=
description=A fictional 15 meter sport glider.
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_type=
atc_model=
performance=Specs:\nWidth:\t15 meters\nLength:\t7 meters\nHeight:\t2 meters\nWeight:\t450lbs.\nCruise Speed:\t50kts\nStall Speed:\t35kts\nMax Speed:\t150kts
[WEIGHT_AND_BALANCE]
max_gross_weight = 900.000
empty_weight = 450.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 1.300, 0.000, -0.500
max_number_of_stations = 1
station_load.0 =170.000000, 2.950000, 0.000000, -0.90000, pilot
;Moments of Inertia
empty_weight_pitch_MOI = 1700.000
empty_weight_roll_MOI = 1700.000
empty_weight_yaw_MOI = 1300.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar =1.090
parasite_drag_scalar =1.000
induced_drag_scalar =1.200
elevator_effectiveness =1.000
aileron_effectiveness =1.000
rudder_effectiveness =1.000
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 2
fuel_flow_scalar = 0 //Scalar for fuel flow efficiency
[pitot_static]
vertical_speed_time_constant = 4 //Increasing this value will cause a more instantaneous reaction in the VSI
//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= 1.000, 2.000, 0.000, -2.750, 1590.000, 2.000, 0.500, 0.000, 0.200, 2.500, 1.000, 0.700, 1.000, 0.000, 0.000, 0.000
point.1= 1.000, -12.200, 0.000, -0.490, 1590.000, 0.000, 0.300, 0.000, 0.20, 2.500, 1.000, 0.700, 1.000, 1.000, 0.000, 0.000
point.2= 2.000, 8.000, 0.000, -1.300, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.3= 2.000, -13.700, 0.000, 0.450, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.4= 2.000, 0.000, 24.500, 2.100, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.5= 2.000, 0.000, -24.500, 2.100, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
static_pitch = 8.600
static_cg_height = 2.200
gear_system_type= 0
[brakes]
parking_brake = 0 //Parking brake available
toe_brakes_scale = 0.51 //Brake scalar
[electrical]
max_battery_voltage = 24.0
gear_motor=0, 0, 0
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint = 2.6, 0.0, 1.3
[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
[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 = 70, 110
aileron = 70, 110
rudder = 70, 110
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
[airplane_geometry]
wing_area = 139.500
wing_span = 54.500
wing_root_chord = 2.85
wing_dihedral = 3.000
wing_incidence = 3.000
wing_twist = -0.996
oswald_efficiency_factor= 0.762
wing_winglets_flag = 1
wing_sweep = 0.000
wing_pos_apex_lon = 0.900
wing_pos_apex_vert = -0.500
htail_area = 28.00
htail_span = 7.100
htail_pos_lon = -11.000
htail_pos_vert = 4.300
htail_incidence = 0.000
htail_sweep = 0.000
vtail_area = 22.000
vtail_span = 4.800
vtail_sweep = 4.000
vtail_pos_lon = -10.500
vtail_pos_vert = 0.300
elevator_area = 14.000
aileron_area = 12.000
rudder_area = 8.000
elevator_up_limit = 20.000
elevator_down_limit = 20.000
aileron_up_limit = 20.000
aileron_down_limit = 20.000
rudder_limit = 20.000
elevator_trim_limit = 5.000
spoiler_limit = 35.000
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 = 40.000
full_flaps_stall_speed = 32.000
cruise_speed = 47.000
max_indicated_speed= 150.086
[autopilot]
autopilot_available= 0
flight_director_available= 0
[forcefeedback]
ground_bumps_magnitude1=2500 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=10.0
ground_bumps_slope1=0.300
ground_bumps_magnitude2=350 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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=2500000 ; in microseconds
[stall_warning]
type=1
[fuel]
fuel_type= 1.000
[gear_warning_system]
gear_warning_available= 0
pct_throttle_limit= 0.000
flap_limit_power= 0.000
flap_limit_idle= 0.000
[Flaps.0]
type= 0
span-outboard= 0.500
extending-time= 0.100
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
[propeller]
thrust_scalar=1.000
[piston_engine]
power_scalar=1.000
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
