[fltsim.0]
title=Red Disco Vollante'
sim=Disco
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Seruphum Aerospace Research
ui_type=
ui_variation=Red
description=Born from the most imaginative concepts in lifting body technologies comes a flying body shaped like a saucer with enclosed dual ducted fans, a turbo charged 4 rotor fuel injected Wankel rotary engine with a carbon fibre block, a large gyro that enduces yaw and roll control which enables flying sideways like a helicopter without flight control surfaces. This is a STOL vehicle designed to take-off as well as land in sectored streets that allow flying vehicle flight interfacing. The dynamic body which produces lift also sports pop-out wings when added control surfaces are required. The most latest and compact state of the art avionics are installed on this 'craft'. If you find yourself being followed by an F16 or guys dressed in black are waiting for you in the driveway, tell them its just a sim model.
[fltsim.1]
title=Yellow Disco Vollante'
sim=Disco
model=
panel=
sound=
texture=1
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Seruphum Aerospace Research
ui_type=
ui_variation=Yellow
description=Born from the most imaginative concepts in lifting body technologies comes a flying body shaped like a saucer with enclosed dual ducted fans, a turbo charged 4 rotor fuel injected Wankel rotary engine with a carbon fibre block, a large gyro that enduces yaw and roll control which enables flying sideways like a helicopter without flight control surfaces. This is a STOL vehicle designed to take-off as well as land in sectored streets that allow flying vehicle flight interfacing. The dynamic body which produces lift also sports pop-out wings when added control surfaces are required. The most latest and compact state of the art avionics are installed on this 'craft'. If you find yourself being followed by an F16 or guys dressed in black are waiting for you in the driveway, tell them its just a sim model.
[fltsim.2]
title=Blue Disco Vollante'
sim=Disco
model=
panel=
sound=
texture=2
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Seruphum Aerospace Research
ui_type=
ui_variation=Blue
description=Born from the most imaginative concepts in lifting body technologies comes a flying body shaped like a saucer with enclosed dual ducted fans, a turbo charged 4 rotor fuel injected Wankel rotary engine with a carbon fibre block, a large gyro that enduces yaw and roll control which enables flying sideways like a helicopter without flight control surfaces. This is a STOL vehicle designed to take-off as well as land in sectored streets that allow flying vehicle flight interfacing. The dynamic body which produces lift also sports pop-out wings when added control surfaces are required. The most latest and compact state of the art avionics are installed on this 'craft'. If you find yourself being followed by an F16 or guys dressed in black are waiting for you in the driveway, tell them its just a sim model.
[fltsim.3]
title=Black Disco Vollante'
sim=Disco
model=
panel=
sound=
texture=3
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Seruphum Aerospace Research
ui_type=
ui_variation=Black
description=Born from the most imaginative concepts in lifting body technologies comes a flying body shaped like a saucer with enclosed dual ducted fans, a turbo charged 4 rotor fuel injected Wankel rotary engine with a carbon fibre block, a large gyro that enduces yaw and roll control which enables flying sideways like a helicopter without flight control surfaces. This is a STOL vehicle designed to take-off as well as land in sectored streets that allow flying vehicle flight interfacing. The dynamic body which produces lift also sports pop-out wings when added control surfaces are required. The most latest and compact state of the art avionics are installed on this 'craft'. If you find yourself being followed by an F16 or guys dressed in black are waiting for you in the driveway, tell them its just a sim model.
[fltsim.4]
title=White Disco Vollante'
sim=Disco
model=
panel=
sound=
texture=4
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Seruphum Aerospace Research
ui_type=
ui_variation=White
description=Born from the most imaginative concepts in lifting body technologies comes a flying body shaped like a saucer with enclosed dual ducted fans, a turbo charged 4 rotor fuel injected Wankel rotary engine with a carbon fibre block, a large gyro that enduces yaw and roll control which enables flying sideways like a helicopter without flight control surfaces. This is a STOL vehicle designed to take-off as well as land in sectored streets that allow flying vehicle flight interfacing. The dynamic body which produces lift also sports pop-out wings when added control surfaces are required. The most latest and compact state of the art avionics are installed on this 'craft'. If you find yourself being followed by an F16 or guys dressed in black are waiting for you in the driveway, tell them its just a sim model.
[fltsim.5]
title=Chome Disco Vollante'
sim=Disco
model=
panel=
sound=
texture=5
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Seruphum Aerospace Research
ui_type=
ui_variation=Chrome
description=Born from the most imaginative concepts in lifting body technologies comes a flying body shaped like a saucer with enclosed dual ducted fans, a turbo charged 4 rotor fuel injected Wankel rotary engine with a carbon fibre block, a large gyro that enduces yaw and roll control which enables flying sideways like a helicopter without flight control surfaces. This is a STOL vehicle designed to take-off as well as land in sectored streets that allow flying vehicle flight interfacing. The dynamic body which produces lift also sports pop-out wings when added control surfaces are required. The most latest and compact state of the art avionics are installed on this 'craft'. If you find yourself being followed by an F16 or guys dressed in black are waiting for you in the driveway, tell them its just a sim model.
[General]
atc_type=
atc_model=Disco
editable=1
performance=Maximum Speed\n350mph \n\nEngine\n3 Rotor Turbocharged Wankle or Hydrogen Turbine engine\n\nMaximum Range\n450 nm
[WEIGHT_AND_BALANCE]
max_gross_weight = 1800 // (pounds)
empty_weight = 800 // (pounds)
reference_datum_position = 4.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -3.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 170, -3.0, -1.5, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, -3.0, 1.5, 0.0 //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 5000.0
empty_weight_roll_MOI = 2537.0
empty_weight_yaw_MOI = 3860.0
empty_weight_coupled_MOI= 0.0
[flight_tuning]
cruise_lift_scalar = 0.80
parasite_drag_scalar = 0.05
induced_drag_scalar = 1.0
elevator_effectiveness = 1.4
aileron_effectiveness = 0.6
rudder_effectiveness = 1.6
pitch_stability = 2.0
roll_stability = 3.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.1
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 4.4, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0 //Fuel flow scalar
min_throttle_limit=0.00
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 90.3 //Cubic inches per cylinder
compression_ratio= 8.5 //Compression ratio
number_of_cylinders=6 //Number of cylinders
max_rated_rpm= 2800 //Max rated RPM
max_rated_hp= 200 //Max rated HP
fuel_metering_type= 0 //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.4 //Starter torque factor
turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0 //Max design manifold pressure, (inHg)
min_design_mp= 0 //Min design manifold pressure, (inHg)
critical_altitude= 0 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE
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= 0.9 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar = 2.2 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.8 //Propeller Diameter, (feet)
propeller_blades= 2 //Number of propeller blades
propeller_moi= 5.7 //Propeller moment of inertia
beta_max= 31.8 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 17.0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1000 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.0 //Propeller gear reduction ratio
fixed_pitch_beta= 20 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 45 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available= 0 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 0 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather= 0 //Minimum RPM for prop feathering
beta_feather= 0 //Feathering pitch angle (degrees)
power_absorbed_cf= 0 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available= 0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta= 0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0 //Minimum pitch angle in reverse, (degrees)
[TailHook]
tailhook_length=4 ;(feet)
tailhook_position = -15.0, 0.0, 2.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0
[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, 1.48, 3.00, -3.09, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.8, 3.2, 0
point.1 = 1, 1.48, -3.00, -3.09, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.8, 3.2, 0
point.2 = 1, -6.02, -4.40, -3.43, 2500, 1, 0.5, 0.0, 0.3, 2.5, 0.7, 5.8, 5.8, 2
point.3 = 1, -6.02, 4.40, -3.43, 2500, 2, 0.5, 0.0, 0.3, 2.5, 0.7, 5.8, 5.8, 3
point.4 = 2, -3.60, -17.9, 2.08, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.5 = 2, -3.60, 17.9, 2.08, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.6 = 2, -19.93, 0.0, 0.83, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.7 = 2, 1.40, 0.0, -1.33, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
point.8 = 2, -19.93, 0.0, 6.83, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7, 0.0, 0.0
point.9 = 2, -4.60, 0.0, -1.33, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8, 0.0, 0.0
max_number_of_points = 21
static_pitch =2.500 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height =3.40 //feet, altitude of CG when at rest on the ground
gear_system_type=0
[fuel]
//Tanks Position and capacity:
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -3.85, -2.10, 2.50, 46.0, 0.00
RightMain= -3.85, 2.10, 2.50, 46.0, 0.00
//Fuel type: 1 = Avgas, 2 = JetA
fuel_type=1
number_of_tank_selectors=1
electric_pump=1
[Views]
eyepoint= -3.40, 0.0, 0.4 //(feet) longitudinal, lateral, vertical distance from reference datum
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 20 // degrees
flaps-position.2 = 30 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[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
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 1, -7.20, 0.00, -1.40, fx_beacon
light.1 = 4, -1.14, 0.00, 1.10, fx_vclight
light.2 = 3, -2.90, -5.59, -1.00, fx_navred ,
light.3 = 3, -2.90, 5.59, -1.00, fx_navgre ,
light.4 = 2, -2.90, -5.59, -1.00, fx_strobe ,
light.5 = 4, 0.40, 0.00, 0.30, fx_vclight ,
light.6 = 2, -2.90, 5.59, -1.00, fx_strobe ,
light.7 =2, -13.30, 0.00, -0.40, fx_navwhi ,
light.8 = 1, -5.40, 0.00, 0.95, fx_beacon ,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[airplane_geometry]
wing_area = 100.0 //Square feet
wing_span = 10.0 //Feet
wing_root_chord = 4.9 //Feet
wing_dihedral = 1.7 //Degrees
wing_incidence = 1.5 //Degrees
wing_twist = -3.0 //Degrees
oswald_efficiency_factor= 0.6 //Measure of lift effeciency of wing
wing_winglets_flag = 1 //Are winglets available?
wing_sweep = 0.0 //Degrees, wing leading edge
wing_pos_apex_lon = -2.4 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 39.0 //Square feet
htail_span = 11.7 //Feet
htail_pos_lon = -18.3 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 3.2 //Degrees
htail_sweep = 10.0 //Degrees, horizontal tail leading edge
vtail_area = 18.0 //Square feet
vtail_span = 4.8 //Feet, tip to body
vtail_sweep = 40.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -16.2 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 1.5 //Feet, vertical distance from reference point, positive going up
elevator_area = 16.6 //Square feet
aileron_area = 18.3 //Square feet
rudder_area = 6.7 //Square feet
elevator_up_limit = 40.0 //Degrees
elevator_down_limit = 33.0 //Degrees
aileron_up_limit = 30.0 //Degrees
aileron_down_limit = 25.0 //Degrees
rudder_limit = 24.0 //Degrees
elevator_trim_limit = 19.5 //Degrees
spoiler_limit = 90.00 //Degrees
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed = 55.0 //Knots True (KTAS)
full_flaps_stall_speed = 42.2 //Knots True (KTAS)
cruise_speed = 312.0 //Knots True (KTAS)
max_indicated_speed=350.000000
[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 700.0
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
use_no_default_bank=1
default_bank_mode=0
[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
[brakes]
toe_brakes_scale=0.671407
parking_brake=1
[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 = 3
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
exit_rate.2 = 0.4 ;Percent per second
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
