[fltsim.0]
title=Vans RV3
sim=RV3
model=
panel=
panel_alias = c172\panel
sound=
sound_alias = c172\sound
texture=
kb_checklists=
kb_reference=
atc_id=NZMAN
ui_manufacturer=Vans
ui_type=RV3
ui_variation=Blue and White
description=The Vans Rv3 is a single place high performance homebuilt sports plane.\nModel designed by Gilles Arlove \nContact gillesa@onfinals.net www.onfinals.net
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_type=VANS
atc_model=
performance=With 125 HP Top Speed 170 kts Cruise @ 75% power 160 kts Stall 44 Kts
[WEIGHT_AND_BALANCE]
max_gross_weight = 2550.000
empty_weight = 1650.000
reference_datum_position = 3.600, 0.000, 0.000
empty_weight_CG_position = -3.500, 0.000, 0.000
max_number_of_stations = 50
station_load.0 = 170.000, -3.000, -1.500, 0.000
station_load.1 = 170.000, -3.000, 1.500, 0.000
station_load.2 = 0, -6.2, -1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 0, -6.2, 1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 0, -8.0, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 1400.000
empty_weight_roll_MOI = 1137.000
empty_weight_yaw_MOI = 2360.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 0.5
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness = 1.6
rudder_effectiveness = 1.0
pitch_stability = 1.0
roll_stability = 0.5
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[GeneralEngineData]
engine_type = 0
Engine.0 = 2.400, 0.000, 0.000
fuel_flow_scalar= 0.880
min_throttle_limit=0.000000
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 98.000
compression_ratio= 8.500
number_of_cylinders= 6
max_rated_rpm= 2700.000
max_rated_hp= 160.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.300
turbocharged= 0
max_design_mp= 0.000
min_design_mp= 0.000
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= 1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar = 1.0 //Propeller thrust scalar
propeller_type= 1
propeller_diameter= 6.400
propeller_blades= 2
propeller_moi= 6.900
beta_max= 45.000
beta_min= 17.200
min_gov_rpm= 1100.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 28.5.000
low_speed_theory_limit= 80.000
prop_sync_available= 1
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 0
min_rpm_for_feather= 700.000
beta_feather= 82.500
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
prop_reverse_available= 0
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
[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
//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, -15.5, 0, -0.4, 1181.1, 0, 0.523, 33.66, 0.296, 2.0, 0.5, 3.5, 3.5, 0, 0.0, 0.0
point.1=1, -1.5, -2.8, -2.8, 1574.8, 1, 0.523, 0.00, 0.2, 1.7, 0.7, 4.7, 4.7, 2, 0.0, 0.0
point.2=1, -1.5, 2.8, -2.8, 1574.8, 2, 0.523, 0.00, 0.2, 1.7, 0.7, 5.2, 5.2, 3, 0.0, 0.0
point.3=2, -3.90, -18.0, -0.67, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -3.90 18.0, -0.67, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -20.23, 0.0, 0.83, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, -1.48, 0.0, -2.17, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 4, 0.0, 0.0
point.7=2, -20.23, 0.0, 6.83, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 7, 0.0, 0.0
point.8=2, -4.90, 0.0, -1.83, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 8, 0.0, 0.0
max_number_of_points = 21
static_pitch = 9.0
static_cg_height = 3.0
gear_system_type=0
[Views]
eyepoint= -5.1, 0, 2.5
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
[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 = 100, 180
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=1,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = -3.900, -2.100, 2.500, 26.500, 0.000
RightMain = -3.900, 2.100, 2.500, 26.500, 0.000
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 174.000
wing_span = 36.100
wing_root_chord = 4.900
wing_dihedral = 0.2
wing_incidence = 1.500
wing_twist = -3.000
oswald_efficiency_factor= 0.680
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = -3.7
wing_pos_apex_vert = 0.000
htail_area = 39.000
htail_span = 11.700
htail_pos_lon = -18.300
htail_pos_vert = 0.000
htail_incidence = 3.200
htail_sweep = 10.000
vtail_area = 18.000
vtail_span = 4.800
vtail_sweep = 40.000
vtail_pos_lon = -16.200
vtail_pos_vert = 1.500
elevator_area = 16.600
aileron_area = 18.300
rudder_area = 6.700
elevator_up_limit = 32
elevator_down_limit = 34
aileron_up_limit = 25.000
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 = 54.000
full_flaps_stall_speed = 43.200
cruise_speed = 155.000
max_indicated_speed=190.000000
[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 700.0
autothrottle_available= 0
pitch_takeoff_ga= 8.000
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]
gear_bump_nose_magnitude=6000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=6000 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=6000 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
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
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 7.000
system_type= 0
damaging-speed= 120.000
blowout-speed= 150.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 12.700, 0.000
flaps-position.2= 25.300, 0.000
flaps-position.3= 40.000, 0.000
[brakes]
toe_brakes_scale=0.671407
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=0.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[exits]
number_of_exits = 1
exit_rate.0 = 1.1 ;Percent per second
