[fltsim.0]
title=Coleoptere
sim=Coleoptere
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer=SNECMA
ui_type=Coleoptere
ui_variation=Prototype
description="SNECMA Coléoptère"
atc_type=
atc_model=
editable=0
[General]
performance=SNECMA C-450 Coléoptère\n French VTOL prototype, 1 seat\nLength: 8.02 m, Span: 4.51 m\n Weight: 3000 kg\n1st flight : May 5th, 1959.
[WEIGHT_AND_BALANCE]
reference_datum_position= 1.000, 0.000, 0.000
empty_weight_CG_position= 2.850, 0.000, 0.000 //+ nup******
//empty_weight= 5540.000 //before
empty_weight= 4240.000 //mine
//max_gross_weight= 15450.000 //before
max_gross_weight= 6000.000 //mine
// Moment of Inertia
//empty_weight_roll_MOI=405151 //457051 max
empty_weight_roll_MOI=205151 //457051 max
empty_weight_pitch_MOI=401733 //403733
empty_weight_yaw_MOI=450647 //453747
empty_weight_coupled_MOI=132
max_number_of_stations=50
station_load.0="160, 0.0, -1.17, 0.0, Co-Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1="170, 0.0, 1.17, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2="0, 0.0, 0.00, 0.0, MainCargo" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//0 Class <0=none,1=wheel, 2=scrape, 4=float, 5=?
//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)
CG_forward_limit= 0.100
CG_aft_limit= 1.000
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
[contact_points] //re-do.cb
point.0= 1.000, 26.000, 0.000, -7.342, 2003.698, 1.000, 0.521, 50.000, 0.230, 2.500, 1.899, 5.000, 5.000, 0.000, 0.000, 0.000
point.1= 1.000, -2.900, -5.850, -7.610, 2003.698, 1.000, 0.521, 2.000, 1.003, 2.500, 1.420, 8.000, 8.000, 2.000, 0.000, 0.000
point.2= 1.000, -2.900, 5.850, -7.610, 2003.698, 2.000, 0.521, 2.000, 1.003, 2.500, 1.420, 9.000, 9.000, 3.000, 0.000, 0.000
point.3= 2.000, 4.000, -32.000, 16.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, 4.000, 32.000, 16.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -32.100, 0.000, 0.055, 1802.219, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 27.500, 0.000, -2.683, 787.405, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7= 4.000, -9.000, -4.850, -0.500, 3068.000, 0.000, 0.512, 20.000, 0.800, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000
point.8= 4.000, -9.000, 4.850, -0.500, 3068.000, 0.000, 0.512, 20.000, 0.800, 2.500, 0.700, 0.000, 0.000, 1.000, 0.000, 0.000
point.9= 4.000, 12.350, -4.450, -0.800, 3068.000, 1.000, 0.512, 0.000, 0.800, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000
point.10= 4.000, 12.350, 4.450, -0.800, 3068.000, 2.000, 0.512, 0.000, 0.800, 2.500, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000
static_pitch= 0.000
static_cg_height= 6.900
gear_system_type=0
[GeneralEngineData]
engine_type= 1
Engine.0= -9.540, 00.000, 0.950
fuel_flow_scalar= 1.000
min_throttle_limit=0.000139
[Reference Speeds]
flaps_up_stall_speed= 50.000
full_flaps_stall_speed= -5.0
//cruise_speed= 200.000
cruise_speed= 300.000
//max_indicated_speed=270.000000
max_indicated_speed=370.000000
//max_mach=0.495000
max_mach=0.655000
[CameraDefinition.0]
Title=Train d'atterrissage
Guid={96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description=Vue du train d'atterrissage sous l'aile gauche
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.52
ShowWeather=Yes
InitialXyz=-2.2, -0.0, -7
InitialPbh=0, 0, 13
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.1]
Title=Empennage
Guid={5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description=Vue de l'arrière de l'avion
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.75
ShowWeather=Yes
InitialXyz=0, 2, -25.0
InitialPbh=5, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.2]
Title=Aile droite
Guid={C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description=Vue de droite
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.5
ShowWeather=Yes
InitialXyz=17, 1.6, -3.0
InitialPbh=6, 0, 280
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
[keyboard_response]
elevator=100.000000, 150.000000
aileron=100.000000, 150.000000
rudder=100.000000, 200.000000
[Helicopter]
low_realism_stability_scale=1.1, 0.9, 0.9 //Pitch , Bank, Yaw Scalars on Stability in Low Realism Settings
cyclic_roll_control_scalar=4.0
cyclic_pitch_control_scalar=6.0
pedal_control_scalar=4.0
reference_length=0.000000
reference_frontal_area=0.000000
reference_side_area=0.000000
side_aero_center=0.000000
right_trim_scalar=1.000000
correlator_available=1.000000
governed_pct_rpm_ref=1.000000
rotor_brake_scalar=1.000000
torque_scalar=1.000000
collective_on_rotor_torque_scalar=1.000000
[Views]
//1 Longitudinal - minus rear (feet)
//2 Lateral - minus left (feet)
//3 elevation - minus lower (feet)
eyepoint=9.00,0.00,10.9000
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=800.000000
autothrottle_available=0
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=4.000000
use_no_default_pitch=1
use_no_default_bank=1
default_pitch_mode=0
default_bank_mode=0
max_pitch=8.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=20.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000
[direction_indicators]
direction_indicator.0=3,0
[TurbineEngineData]
fuel_flow_scalar=1.001
fuel_flow_gain= 0.0052
inlet_area= 8.227
rated_N2_rpm= 31500.000 //N2 in reality can have up to 32000 rpm, not N1 !
static_thrust= 8000.000
afterburner_available= 0
reverser_available= 0.000
[propeller]
thrust_scalar=1.2 //Propeller thrust scalar
propeller_type=1 //o=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=38.2 //o=38.1 //Propeller Diameter, (feet)
propeller_blades=3 //Number of propeller blades
propeller_moi=52 //Propeller moment of inertia
beta_max=49 //Max blade pitch angle for constant speed prop, (degrees)
beta_min=14 //Min blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=2750 //Max governed RPM!
prop_tc=0.0200 //Prop time-constant
gear_reduction_ratio=10.0 //Propeller gear reduction ratio/2750 rpm
fixed_pitch_beta=10 //Fixed pitch angle (degrees)
low_speed_theory_limit=9 //Spd at which low spd theory becomes blended in (ft/sec)
prop_sync_available=1 //synchronization 0=FALSE, 1=TRUE
prop_deice_available=1 //0=FALSE, 1=TRUE
prop_feathering_available=1 // 0=FALSE, 1=TRUE
prop_auto_feathering_available=1 // 0=FALSE, 1=TRUE
min_rpm_for_feather=660 //Minimum RPM for prop feathering
beta_feather=70.0 //Feathering pitch angle (degrees)
power_absorbed_cf=0.56 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0 // 0=FALSE, 1=TRUE
prop_reverse_available=0 // 0=FALSE, 1=TRUE
minimum_on_ground_beta=0.2 //Min pitch angle on ground, (degrees)
minimum_reverse_beta=-1.0 //Min pitch angle in reverse, (degrees)
rotation=-1,1 //Engine 1,2,3,... Rotation direction. 1 = CW, -1 = CCW
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
dirtcrash=fx_dirtcrash
[fuel] //changed.cb
Center1= 0.241, 0.000, -0.5, 550.000, 5.000 //+nsdwn ************
LeftMain= 0.0, 0.000, -0.2, 200.000, 4.000
RightMain= 0.0, 0.000, -0.2, 200.000, 4.000
LeftAux= -0.06, -16.575, 0.000, 175.000, 1.000
RightAux= -0.06, 16.575, 0.000, 175.000, 1.000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//1 Longitudinal - minus rear (feet)
//2 Lateral - minus left (feet)
//3 elevation - minus lower (feet)
light.0=3, -0.24, -6.95, 8.66, fx_navred
light.1=3, -0.24, 6.95, 8.66, fx_navgre
light.2=4, 10.40, 0.00, 10.50, fx_vclight
[airplane_geometry]
wing_area= 1420.000
wing_span= 125.000
wing_root_chord= 16.650
wing_dihedral= 1.800
wing_incidence= 0.75 //0.5
wing_twist= -0.25 //2
oswald_efficiency_factor= 0.944
wing_winglets_flag= 1
wing_sweep= -1.001
wing_pos_apex_lon= 7.586 //pos2tail-12mx +++++//
wing_pos_apex_vert= 0.840
htail_area= 1252.000
htail_span= 114.167
htail_pos_lon= -25.832
htail_pos_vert= 2.500
htail_incidence= 0.76
htail_sweep= 0.200
vtail_area= 102.000
vtail_span= 11.502
vtail_sweep= 0.100
vtail_pos_lon= -25.000
vtail_pos_vert= 5.853
elevator_area= 99.800
aileron_area= 98.760
rudder_area= 87.000
elevator_up_limit= 28.000
elevator_down_limit= 26.000
aileron_up_limit= 26.500
aileron_down_limit= 12.500
rudder_limit= 33.000
elevator_trim_limit= 24.000
spoiler_limit= 00.005
spoilerons_available= 1
aileron_to_spoileron_gain= 0.900
min_ailerons_for_spoilerons= 5.000
min_flaps_for_spoilerons= 35.000
[Flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=0.960
induced_drag_scalar=0.740
elevator_effectiveness=1.72
yaw_stability=0.98
elevator_trim_effectiveness=1.02
pitch_stability=1.00
roll_stability=0.99
aileron_effectiveness=2.000
rudder_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
;aileron_trim_effectiveness=1.0
;rudder_trim_effectiveness=1.0
[ground_reaction] //added.cb
main_gear_static_compression=1.5
center_gear_static_compression=0.94
main_gear_damping_ratio=0.99
center_gear_damping_ratio=0.988
[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 1
Com.2=1, 1
Nav.1=1, 1, 1
Nav.2=1, 1, 0
Adf.1=1
Transponder.1=1
Marker.1=1
[brakes]
toe_brakes_scale=0.98
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[hydraulic_system]
normal_pressure=50.000000
engine_map=1,1,0,0
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[jet_engine]
thrust_scalar=1.1185
[Flaps]
type= 1
span-outboard= 0.95
extending-time= 15
system_type= 1
damaging-speed= 170.000
blowout-speed= 185.000
lift_scalar= 7.500
drag_scalar= 4.240
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.600, 0.000 //best below 80 knots
flaps-position.2= 11.100, 0.000 //below 35 knots
flaps-position.3= 36.200, 0.000 //below 18 knots
//flaps-position.4= 83.600, 0.000 //low speed descent-do park brakes
flaps-position.4= 89.000, 0.000 //low speed descent-do park brakes
[smokesystem]
smoke.0=0.00, 3.95, -0.85, afx_A_50Cal.fx
smoke.1=0.00, 3.95, -0.85, afx_50Cal.fx
smoke.2=0.00, 3.95, 0.85, afx_50Cal.fx
smoke.3=0.00, 3.95, 000.00, afx_FireBall500ft.fx
[MainRotor]
number_of_blades=3.000000
weight_per_blade=0.000000
weight_to_moi_factor=0.000000
inflow_vel_reference=0.000000
[SecondaryRotor]
number_of_blades=3.000000
weight_per_blade=0.000000
weight_to_moi_factor=0.000000
inflow_vel_reference=0.000000
[fuselage_aerodynamics]
drag_force_cf=0.000000
side_drag_force_cf=0.000000
pitch_damp_cf=0.000000
roll_damp_cf=0.000000
yaw_damp_cf=0.000000
yaw_stability_cf=0.000000
