[fltsim.0]
title=Nimbus 3/24.5 F-CFTO v.3
sim=Nimbus3v3
model=
panel=
sound=
texture=
checklists=
kb_reference=Nimbus3v3_ref
atc_id=TO
ui_manufacturer=Schempp-Hirth
ui_type=Nimbus 3/24.5
ui_variation=F-CFTO
visual_damage=1
description=Open class- High performance single seat glider.\nDesigned by Klaus Holighaus and manufactured in carbon fiber by Schempp-Hirth ( Germany).\nWinner of multiple World Championships and Record Flights.
[General]
atc_heavy=0
atc_type=Nimbus
atc_airline=
atc_flight_number=
editable=0
performance=Wing span: 22.9 m - 24.5 m with wing tips\n ( 75.1- 80.4 ft )\nLength: 7.63 m ( 25.3 ft )\nWeight: 404 Kg - 750 Kg with water ballasts\n ( 1656 lb )\nMaximum L/D:60 to 1\nDetails:\nDesigner: Thierry OGERAU\nDate: Jan 99,Apr 02 & Jan 03. To better copy my real Nimbus 3\/24.5 F-CFTO, this Version 3 for FS2002 includes GPS, ballasts and an upgraded panel.
[electrical]
max_battery_voltage=24
avionics_bus=0, 0 , 0
avionics=0, 0 , 0
additional_system=0, 0 , 0
flap_motor=0, 0 , 0
gear_motor=0, 0 , 0
[SMOKESYSTEM]
smoke.0=0.0,0.0,16.50, fx_contrail_s.fx
smoke.1=0.0,-2.0,2.00, fx_contrail_s.fx
smoke.2=0.0,0.0,-16.50, fx_contrail_s.fx
smoke.3=0.0,-2.0,-2.00, fx_contrail_s.fx
[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=1102.000000
empty_weight_roll_MOI=735.000000
empty_weight_pitch_MOI=369.000000
empty_weight_yaw_MOI=971.000000
empty_weight_coupled_MOI=0.000000
[fuel]
LeftMain=0.000000,0.000000,0.000000,29.000000,0.000000
RightMain=0.000000,0.000000,0.000000,29.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
//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, -16.0, 0.0, -1.166667,1574.8, 0, 0.506572, 0.0, 0.401632, 2.5, 0.622963,0.5,0.5,0.0,0.0,0.0
point.1=1,1.166667,-0.083333,-2.666667,1574.8,1,0.506572,0.0,0.267552,2.5,0.882012,0.5,0.5,2.0,0.0,0.0
point.2=1,1.166667, 0.083333,-2.666667,1574.8,2,0.506572,0.0,0.267552,2.5,0.882012,0.5,0.5,3.0,0.0,0.0
point.3=2,-1.333333,-41.8, 1.5,1574.8,0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,5.0,0.0,0.0
point.4=2,-1.333333,41.8, 1.5,1574.8,0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,6.0,0.0,0.0
point.5=2,-16.0, 0.0, -1.333333,1574.8,0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,9.0,0.0,0.0
point.6=2,5.666667, 0.0, -1.833333,1574.8,0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,4.0,0.0,0.0
point.7=2,-1.333333,41.8, 1.5,1574.8,0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,7.0,0.0,0.0
static_pitch=5.998535
static_cg_height=2.333910
[Views]
eyepoint= 1.332841, 0.0, 0.589526
[Flaps.0]
type=1 // 1 - tail, 2 - lead
span-outboard=0.5 // 0.0 .. 1.0
extending-time=0.3 // seconds
system_type=0
flaps-position.0=0.0,0 // degrees, KIAS
flaps-position.1=9.9,0
flaps-position.2=19.9,0
flaps-position.3=29.9,0
flaps-position.4=39.9,0
[GeneralEngineData]
engine_type=2
fuel_flow_scalar=1.000000
[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 = 150, 250
aileron = 150, 250
rudder = 150, 250
[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
[airplane_geometry]
wing_area=118.000000
wing_span=54.500000
wing_root_chord=2.166667
wing_dihedral=3.499146
wing_incidence=0.000000
wing_twist=-0.999756
oswald_efficiency_factor=1.249987
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=22.000000
htail_span=7.916667
htail_pos_lon=-13.750000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=22.000000
vtail_span=5.347897
vtail_sweep=0.000000
vtail_pos_lon=-13.750000
vtail_pos_vert=3.916667
elevator_area=13.760000
aileron_area=21.500000
rudder_area=11.200000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
[Reference Speeds]
flaps_up_stall_speed=41.0
full_flaps_stall_speed=32.8
cruise_speed=71.087706
[autopilot]
autopilot_available=0
flight_director_available=0
[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750 ; 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
