[fltsim.0]
title=Questair_Nuventure
sim=Questair_Nuventure
model=
panel=
sound=
texture=
kb_checklists=
description=The Questair Venture is a kitbuilt serious cross-country single-engine speed machine. Able to cruise at 287 kts (true airspeed) up above unpleasant weather, the Venture is ideal for leisure and business trips. With more speed and higher flight capability, this is a step up in complexity from the Cessnas. The Venture is built around a diminutive airframe reducing the wetted area. This enabled the aircraft to shatter 8 world-records on a derated Continental 550 engine, after its introduction. This model has full moving flying surfaces, opening geardoors and canopy (Shift-E). I have not however been able to implement the complex maingear animation (any help is greatly appreciated!) (c) Visual model, flight model and texture by Morten Ulrik Hansen morten@indsigt.it, Copenhagen, 2003.
[General]
atc_type=EXPERIMENTAL
atc_model=NUVENTURE
editable=1
performance=Maximum Speed\t\n286 kts 330 mph\t531 kmh\n\nCruise Speed\t\n240 kts 276 mph \t444 kmh\n\nEngine\t\nCont. IO-550N 310 hp\n\nPropeller\t\nTwo-bladed McCauley constant speed\n\nMaximum Range\t\n1,050 nm 1,204 sm \t1,945 km\n\nService Ceiling\t\n35,000 ft 10,668 m\n\nFuel Capacity\t\n56 U.S. gal 211 L \n\nEmpty Weight\t\n1,240 lb \t 462 kg\n\nMaximum Gross Weight\t\n2,000 lb \t 747 kg\n\nUseful Load\t\n424 lb \t 158 kg\n\nLength\t\n16,3 ft\t 5,1 m\n\nWingspan\t\n27,5 ft\t 8,4 m\n\nHeight\t\n9,58 ft\t 2,8 m\n\nSeating\t\n2
[WEIGHT_AND_BALANCE]
max_gross_weight = 2000.000
empty_weight = 1240.000
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 1.500, 0.000, 0.000
max_number_of_stations = 50
station_load.0 = 170.000, -3.100, -1.500, 0.000
station_load.1 = 170.000, -3.100, 1.500, 0.000
//station_load.2 = 100, -6.1, -1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.3 = 100, -6.1, 1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 765.000
empty_weight_roll_MOI = 470.000
empty_weight_yaw_MOI = 990.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =0.800
induced_drag_scalar =0.811
elevator_effectiveness =1.000
aileron_effectiveness =1.202
rudder_effectiveness =1.000
pitch_stability =2.001
roll_stability =1.301
yaw_stability =2.001
elevator_trim_effectiveness =0.800
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 0
Engine.0 = 4.100, 0.000, 0.000
fuel_flow_scalar= 1.000
[piston_engine]
power_scalar =1.901
cylinder_displacement= 90.300
compression_ratio= 8.700
number_of_cylinders= 6
max_rated_rpm= 2700.000
max_rated_hp= 310.000
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=1.500
idle_rpm_mechanical_efficiency_scalar=0.640
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
[propeller]
thrust_scalar =1.761
propeller_type= 0
propeller_diameter= 5.900
propeller_blades= 3
propeller_moi= 6.000
beta_max= 43.000
beta_min= 15.000
min_gov_rpm= 1100.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 1
prop_deice_available= 1
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
prop_reverse_available= 1
minimum_on_ground_beta= 1.000
minimum_reverse_beta= -14.000
[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= 1.000, 5.480, 0.000, -4.700, 1181.100, 0.000, 0.523, 33.660, 0.296, 2.500, 0.794, 3.500, 3.500, 0.000, 0.000, 0.000
point.1= 1.000, -1.480, -4.500, -4.700, 1574.800, 1.000, 0.523, 0.000, 0.286, 2.500, 0.808, 4.700, 4.700, 2.000, 0.000, 0.000
point.2= 1.000, -1.480, 4.500, -4.700, 1574.800, 2.000, 0.523, 0.000, 0.286, 2.500, 0.808, 5.200, 5.200, 3.000, 0.000, 0.000
point.3= 2.000, -3.900, -18.000, -0.670, 1574.800, 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, -3.900, 18.000, -0.670, 1574.800, 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, -20.230, 0.000, 0.830, 1574.800, 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, -1.480, 0.000, -2.170, 1574.800, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7= 2.000, -20.230, 0.000, 6.830, 1574.800, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.8= 2.000, -4.900, 0.000, -1.830, 1574.800, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000
max_number_of_points = 21
static_pitch = 1.840
static_cg_height = 4.400
[Views]
eyepoint = -3.9, 0.0, 0.0
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = -4.100, -7.900, -0.800, 47.500, 3.000
RightMain = -4.100, 7.900, -0.800, 47.500, 3.000
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
[airplane_geometry]
wing_area = 72.500
wing_span = 27.500
wing_root_chord = 4.026
wing_dihedral = 4.000
wing_incidence = 2.500
wing_twist = -1.500
oswald_efficiency_factor= 0.600
wing_winglets_flag = 0
wing_sweep = 2.000
wing_pos_apex_lon = 0.000
wing_pos_apex_vert = -0.800
htail_area = 19.080
htail_span = 10.250
htail_pos_lon = -8.930
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 1.000
vtail_area = 9.750
vtail_span = 4.760
vtail_sweep = 40.000
vtail_pos_lon = -8.930
vtail_pos_vert = 2.330
elevator_area = 4.082
aileron_area = 10.810
rudder_area = 3.509
elevator_up_limit = 28.000
elevator_down_limit = 21.000
aileron_up_limit = 25.000
aileron_down_limit = 18.000
rudder_limit = 24.000
elevator_trim_limit = 19.500
spoiler_limit = 90.000
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 = 61.000
full_flaps_stall_speed = 54.000
cruise_speed = 240.000
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1700.0
autothrottle_available= 0
pitch_takeoff_ga=8.000000
[forcefeedback]
gear_bump_nose_magnitude=3000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2700 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1300 ; 0 - 10000
ground_bumps_angle1=08900 ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200 ; 0 - 10000
ground_bumps_angle2=09100 ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
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= 5.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 25.000, 0.000
