[fltsim.0]
title=Rotodyne Fairey Test Plane
sim=Rotodyne
model=
panel=
sound=
texture=Fairey
kb_checklists=
//ui_manufacturer=–ЇЉФ—pѓwѓЉѓRѓvѓ^Ѓ[
//ui_type=Fairey Rotodyne
ui_manufacturer=Fairey
ui_type=Rotodyne
ui_variation=Fairey Test Plane (XE521)
description=This was a compound autogyro or gyrodyne. \nIt took off and landed as a helicopter, and cruised as an autogyro with supplemental fixed wings. \nThis would then cruise at speeds of about 150 knots to another city (say, London to Paris) where the rotor tip-jet system would be restarted for landing vertically in the city centre.\n\nby Kazunori Ito\n  [email protected]\n

[fltsim.1]
title=Rotodyne QANTAS AirLine
sim=Rotodyne
model=
panel=
sound=
texture=QANTAS
kb_checklists=
//ui_manufacturer=–ЇЉФ—pѓwѓЉѓRѓvѓ^Ѓ[
//ui_type=Fairey Rotodyne
ui_manufacturer=Fairey
ui_type=Rotodyne
ui_variation=QANTAS Airline (VH-EAF)
description=This was a compound autogyro or gyrodyne. \nIt took off and landed as a helicopter, and cruised as an autogyro with supplemental fixed wings. \nThis would then cruise at speeds of about 150 knots to another city (say, London to Paris) where the rotor tip-jet system would be restarted for landing vertically in the city centre.\n\nby Kazunori Ito\n  [email protected]\n

[General]
performance=Length: 58 ft 8 in (17.9 m) \nRotor diameter: 90 ft 0 in (27.4 m) \nHeight: 22 ft 2 in (6.76 m) \nDisc area: 6,360 ft2 (591 m2) \n\nLoaded weight: 33,000 lb (15,000 kg) \nMax takeoff weight: 38,000 lb (17,000 kg) \n\nPowerplant: 2Ѓ~ Napier Eland turboprops, 2,800 hp (2,100 kW) each \n\nMaximum speed: 213 mph (343 km/h) \nRange: 520 mi (830 km) \nDisc loading: 5.2 lb/ft2 (25 kg/m2) \nPower/mass: 0.17 hp/lb (280 W/kg) \n\nCrew: 3 \nCapacity: 40 passengers \n 
atc_type=
atc_model=

[WEIGHT_AND_BALANCE]
reference_datum_position= 1.000, 0.000, 0.000
empty_weight_CG_position= 2.850, 0.000, 0.000
empty_weight= 5540.000
max_gross_weight= 15450.000
empty_weight_roll_MOI=405151
empty_weight_pitch_MOI=401733
empty_weight_yaw_MOI=450647
empty_weight_coupled_MOI=132
max_number_of_stations=50
station_load.0="160,  0.0, -1.17, 0.0, "
station_load.1="170,  0.0,  1.17, 0.0, "
station_load.2="0,  0.0,  0.00, 0.0,"
CG_forward_limit= 0.100
CG_aft_limit= 1.000

[airplane_geometry]
wing_area= 1420.000
wing_span= 125.000
wing_root_chord= 16.650
wing_dihedral= 1.800
wing_incidence= 0.75
wing_twist= -0.25
oswald_efficiency_factor= 0.944
wing_winglets_flag= 1
wing_sweep= -1.001
wing_pos_apex_lon= 7.586
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

[fuel]
Center1= 0.241, 0.000, -0.5, 550.000, 5.000
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

[contact_points] 
point.0= 1.000, 26.000, 0.000, -6.142, 2003.698, 1.000, 0.521, 50.000, 0.230, 2.500, 1.899, 8.000, 8.000, 0.000, 0.000, 0.000
point.1= 1.000, -2.900, -5.850, -7.010, 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, -7.010, 2003.698, 2.000, 0.521, 2.000, 1.003, 2.500, 1.420, 8.000, 8.000, 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= 6.500
gear_system_type=0

[Flaps.0]
type= 1
span-outboard= 0.95
extending-time= 3 //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
flaps-position.2= 11.100, 0.000
flaps-position.3= 36.200, 0.000
flaps-position.4= 83.600, 0.000

[Flaps.1]
type= 2
span-outboard= 0.75
extending-time= 3 //6
system_type= 1
damaging-speed= 170.000
blowout-speed= 185.000
lift_scalar= 0.750
drag_scalar= 0.050
pitch_scalar= 0.005
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 0.200, 0.000
flaps-position.3= 1.000, 0.000
flaps-position.4= 2.200, 0.000

[GeneralEngineData]
engine_type= 1
Engine.0= -9.540, -18.830, 0.950
Engine.1= -9.540, 18.830, 0.950
Engine.2= 0.000, 0.000, 3.550
fuel_flow_scalar= 1.000
min_throttle_limit=0.000139

[TurbineEngineData]
fuel_flow_scalar=1.001
fuel_flow_gain= 0.0052
inlet_area= 8.227
rated_N2_rpm= 31500.000
static_thrust= 5700.000
afterburner_available= 0
reverser_available= 0.000

//[jet_engine]
//thrust_scalar=1.1185

[Helicopter]
low_realism_stability_scale=1.1, 0.9, 0.9
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

[propeller]
thrust_scalar=1.2
propeller_type=1
propeller_diameter=38.2
propeller_blades=3
propeller_moi=52
beta_max=49
beta_min=14
min_gov_rpm=2750
prop_tc=0.0200
gear_reduction_ratio=10.0
fixed_pitch_beta=10
low_speed_theory_limit=9
prop_sync_available=1
prop_deice_available=1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather=660
beta_feather=70.0
power_absorbed_cf=0.56
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.2
minimum_reverse_beta=-1.0
rotation=-1,1

[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

[hydraulic_system] //Џd—v
normal_pressure=50.000000
engine_map=1,1,0,0

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
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

[Views]
eyepoint=22.307,-1.841,1.673

[Reference Speeds]
flaps_up_stall_speed= 50.000
full_flaps_stall_speed= -5.0
cruise_speed= 200.000
max_indicated_speed=270.000000
max_mach=0.495000

[direction_indicators]
direction_indicator.0=3,0

[keyboard_response]
elevator=100.000000, 150.000000
aileron=100.000000, 150.000000
rudder=100.000000, 200.000000

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
dirtcrash=fx_dirtcrash

[Lights]
light.0=3,  -1.59, 0.00,  12.53, fx_navredm ,
light.1=2,  -1.59, 0.00,  12.53, fx_strobeh ,
light.2=3,  -3.00, 0.00,  -3.90, fx_navredm ,
light.3=2,  -3.00, 0.00,  -3.90, fx_strobeh ,

light.4=3,  4.35, 22.87,  3.05, fx_navgrem ,
light.5=3,  4.35, -22.87,  3.05, fx_navredm ,

light.6=3,  -29.35, 0.00,  2.17, fx_navwhih ,

[brakes]
toe_brakes_scale=0.887783
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
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0