[fltsim.0]
title=Garbers and Beckert GB-I Parachute (House colors)
sim=Chute_test
model=
panel=
sound=
texture=mg
kb_checklists=GB-I_check
kb_reference=GB-I_ref
atc_id=D-0815
ui_manufacturer=Garbers and Beckert
ui_type=GB-I Parachute
ui_variation=House colors
visual_damage=1
description=Visual model by Michael Garbers,\t flight dynamics by Wolfram Beckert
[fltsim.1]
title=Garbers and Beckert GB-I Parachute (C.S.A colors)
sim=Chute_test
model=
panel=
sound=
texture=wb
kb_checklists=GB-I_check
kb_reference=GB-I_ref
atc_id=D-0815
ui_manufacturer=Garbers and Beckert
ui_type=GB-I Parachute
ui_variation=C.S.A colors
visual_damage=1
description=Visual model by Michael Garbers,\t flight dynamics by Wolfram Beckert www.simflight.de/classic
[fltsim.2]
title=Garbers and Beckert GB-I Parachute (FlightXtreme colors)
sim=Chute_test
model=
panel=
sound=
texture=fxt
kb_checklists=GB-I_check
kb_reference=GB-I_ref
atc_id=D-0815
ui_manufacturer=Garbers and Beckert
ui_type=GB-I Parachute
ui_variation=FlightXtreme colors
visual_damage=1
description=Visual model by Michael Garbers,\t flight dynamics by Wolfram Beckert www.flightxtreme.com
[fltsim.3]
title=Garbers and Beckert GB-I Parachute (Whale colors)
sim=Chute_test
model=
panel=
sound=
texture=wal
kb_checklists=GB-I_check
kb_reference=GB-I_ref
atc_id=D-0815
ui_manufacturer=Garbers and Beckert
ui_type=GB-I Parachute
ui_variation=Whale colors
visual_damage=1
description=Visual model by Michael Garbers,\t flight dynamics by Wolfram Beckert www.dornier-wal.info
[fltsim.4]
title=Garbers and Beckert GB-I Parachute (FlightSim colors)
sim=Chute_test
model=
panel=
sound=
texture=fs
kb_checklists=GB-I_check
kb_reference=GB-I_ref
atc_id=D-0815
ui_manufacturer=Garbers and Beckert
ui_type=GB-I Parachute
ui_variation=FlightSim colors
visual_damage=1
description=Visual model by Michael Garbers,\t flight dynamics by Wolfram Beckert www.FlightSim.com
[General]
atc_type=Experimental
atc_model=
editable=1
performance=Maximum Speed\t37 kts\nGlide Ratio\t12 to 1\nEmpty Weight\t25 lb\nSeating\t\t1\nUseful Load\t195 lb\n
[WEIGHT_AND_BALANCE]
max_gross_weight = 195 // (pounds)
empty_weight = 25 // (pounds)
reference_datum_position = 1.25, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -1.00, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 1
station_load.0 = 170, -0.8, 0.0, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 800
empty_weight_roll_MOI = 400
empty_weight_yaw_MOI = 800
empty_weight_coupled_MOI = 0.0
[flight_tuning]
cruise_lift_scalar = 0.8
parasite_drag_scalar = 2.98
induced_drag_scalar = 2.8
elevator_effectiveness = 1.4
aileron_effectiveness = 1.0
rudder_effectiveness = 1.8
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
[GeneralEngineData]
engine_type = 2 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
fuel_flow_scalar = 0 //Fuel flow scalar
[pitot_static]
vertical_speed_time_constant = 1 //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=3, -2.0, 0.0, -2.5, 1574.8, 2, 0.509, 0.0, 0.40, 2.5, 1.22, 0.0, 0.0, 3, 0.0, 0.0// Schuhe als Kufe
point.1=2, -1.25, -16.5, 0.5, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5, 0.0, 0.0
point.2=2, -1.25, 16.5, 0.5, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6, 0.0, 0.0
point.3=2, -15.42, 0.0, -0.7, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9, 0.0, 0.0
point.4=2, 6.25, 0.0, -2.2, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4, 0.0, 0.0
static_pitch = -4.65
static_cg_height = 2.17
[Views]
eyepoint = 2.0, 0.0, 1.6
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 2.000
system_type= 3
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.400
drag_scalar= 1.200
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 45.000, 0.000
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 0
Com.1 = 0, 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 = 160, 360
aileron = 160, 360
rudder = 160, 360
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
[airplane_geometry]
wing_area = 107.0 //Square feet
wing_span = 26.2 //Feet
wing_root_chord = 4.1 //Feet
wing_dihedral = 3.5 //Degrees
wing_incidence = 3.0 //Degrees
wing_twist = -2.0 //Degrees
oswald_efficiency_factor= 0.6 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 0.0 //Degrees, wing leading edge
wing_pos_apex_lon = -0.5 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 21.0 //Square feet
htail_span = 7.9 //Feet
htail_pos_lon = -17.3 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 0.0 //Degrees, horizontal tail leading edge
vtail_area = 17.0 //Square feet
vtail_span = 4.7 //Feet, tip to body
vtail_sweep = 0.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -16.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 3.9 //Feet, vertical distance from reference point, positive going up
elevator_area = 16.0 //Square feet
aileron_area = 14.7 //Square feet
rudder_area = 8.0 //Square feet
elevator_up_limit = 36.0 //Degrees
elevator_down_limit = 26.0 //Degrees
aileron_up_limit = 30.0 //Degrees
aileron_down_limit = 30.0 //Degrees
rudder_limit = 40.0 //Degrees
elevator_trim_limit = 15.0 //Degrees
spoiler_limit = 70.0 //Degrees
spoilerons_available = 0 //Spoilerons Available?
aileron_to_spoileron_gain = 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed = 15.0 //Knots True (KTAS)
full_flaps_stall_speed = 10.0 //Knots True (KTAS)
cruise_speed = 37.0 //Knots True (KTAS)
[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
