[fltsim.0]
title=Stampe SV4 
sim=stampe_sv4
model=
panel=
sound=
texture=classique
kb_checklists=
kb_reference=
atc_id=f-bagk
ui_manufacturer=Stampe et Vertongen
ui_type=Stampe SV4
ui_variation=
description=Établie en 1922 en Belgique, la firme Stampe et Vertongen, dont le bureau d'études fut dirigé par Alfred Renard, se spécialisa dans la mise au point d'appareils de tourisme et d'entraînement de base ou avancé qui reçurent la dénomination de RSV (pour Renault Stampe Vertongen).                                                   Auteur : Eric Dantès 

[General]
atc_type=SV4
atc_model=SV4
editable=0
performance=vitesse maximale, 200 km/h  / plafond pratique, 5 500 m  / Poids à vide, 480 kg  / maximal au décollage, 780 kg  / envergure, 8,40 m  / longueur, 6,50 m  / hauteur, 2,60 m  / surface alaire, 19 m2  / moteur , Renault 140 ch


[WEIGHT_AND_BALANCE]
max_gross_weight=1720.000
empty_weight=1170.000

reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000

max_number_of_stations=50

station_load.0=170.000000,0.000000,0.000000,0.000000
station_load.1=170.000000,0.000000,0.000000,0.000000

;Moments of Inertia
empty_weight_pitch_MOI=1346.000
empty_weight_roll_MOI=1148.000
empty_weight_yaw_MOI=2967.000
empty_weight_coupled_MOI=0.000
CG_forward_limit=0.000
CG_aft_limit=1.000

[exits]
number_of_exits=3
exit_rate.0=0.2

[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
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=0
Engine.0=8.300, 0.000, 0.500
fuel_flow_scalar=1.000
min_throttle_limit=0.000000

[piston_engine]
power_scalar=1.000
cylinder_displacement=80
compression_ratio=6.800
number_of_cylinders=4
max_rated_rpm=2400.000
max_rated_hp=140.000
fuel_metering_type=3
cooling_type=0
normalized_starter_torque=0.300
turbocharged=0
max_design_mp=0.000
min_design_mp=5.000
critical_altitude=0.000
emergency_boost_type=0
emergency_boost_mp_offset=0.000
emergency_boost_gain_offset=0.000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=0.750

[propeller]
thrust_scalar=1.000
propeller_type=1
propeller_diameter=6.800
propeller_blades=2
propeller_moi=5.000
beta_max=0.000
beta_min=0.000
min_gov_rpm=0.000
prop_tc=0.100
gear_reduction_ratio=1.000
fixed_pitch_beta=18.000
low_speed_theory_limit=80.000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000
beta_feather=0.000
power_absorbed_cf=0.000
defeathering_accumulators_available=0
minimum_on_ground_beta=0.000
minimum_reverse_beta=0.000


//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
prop_reverse_available=0

[contact_points]
point.0=1.000, -9.000, 0.000, -2.950, 1181.100, 0.000, 0.519, 50.000, 0.304, 2.500, 0.695, 0.000, 0.000, 0.000, 0.000, 0.000
point.1=1.000, 2.000, -2.500, -5.100, 1574.800, 1.000, 0.519, 0.000, 0.304, 2.500, 0.686, 0.000, 0.000, 2.000, 0.000, 0.000
point.2=1.000, 2.000, 2.500, -5.100, 1574.800, 2.000, 0.519, 0.000, 0.304, 2.500, 0.682, 0.000, 0.000, 3.000, 0.000, 0.000
point.3=2.000, 0.000, -17.900, -2.100, 787.400, 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, 0.000, 17.900, -2.100, 787.400, 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, -13.000, 0.000, 3.300, 787.400, 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, 2.400, 0.000, -2.200, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch=11.700
static_cg_height=4.300

[Views]
eyepoint=-3.85, 0.0, 1.3

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 1
Nav.1=1, 1, 0
Adf.1=1
Transponder.1=0
Marker.1=1

[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=200, 1000
aileron=200, 1000
rudder=200, 1000

[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
touchdown=fx_tchdwn_s, 1

[SMOKESYSTEM]
smoke.0=0.00, -0.70, 1.40, fx_smoke_w

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
light_nav=0, 5 , 17.0
light_beacon=0, 5 , 17.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 17.0
light_panel=0, 5 , 17.0

[fuel]
RightMain=0.000, 0.000, 0.000, 20.000, 0.000
fuel_type=1                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area=174.000
wing_span=35.800
wing_root_chord=4.900
wing_dihedral=3.000
wing_incidence=0.000
wing_twist=-1.000
oswald_efficiency_factor=0.500
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=1.200
wing_pos_apex_vert=0.000
htail_area=40.000
htail_span=11.700
htail_pos_lon=-14.700
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=0.000
vtail_area=18.000
vtail_span=4.800
vtail_sweep=0.000
vtail_pos_lon=-12.600
vtail_pos_vert=0.000
elevator_area=17.600
aileron_area=18.300
rudder_area=6.700
elevator_up_limit=30.000
elevator_down_limit=21.000
aileron_up_limit=30.000
aileron_down_limit=20.000
rudder_limit=24.000
elevator_trim_limit=19.500
spoiler_limit=0.000
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=50.000
full_flaps_stall_speed=50.000
cruise_speed=90.000
max_indicated_speed=180.000000

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
max_pitch=10.000000
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=25.000000
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

[forcefeedback]
ground_bumps_magnitude1=2600            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200            ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
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=3500000                 ; in microseconds

[Flaps.0]
type=0
span-outboard=0.500
extending-time=0.100
system_type=0
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=0.000, 0.000

[brakes]
toe_brakes_scale=0.610370
parking_brake=1

[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=0

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0