[fltsim.0]
title=DE SCHELDE D21
sim=D21
model=
panel=
sound=
texture=
atc_id=
ui_manufacturer=DE SCHELDE
ui_type=D XXI
ui_variation=
description=Dutch company called Koninklijke Maatschappij De Schelde\nstarted an aviation department with the collapse of Pander & Zonen\npicking up that company's chief engineer in 1935. From these came \nthe S.21 a single-seat fighter of unconventional layout intended for \nthe interceptor role. The aircraft had some unusual features. It was \nall-metal in construction, a reverse gull wing with twin booms. \nOnly one prototype was built as the Germans occupied the factory in 1940. \n
[General]
atc_type=Extra
atc_model=
editable=0
performance=Maximum Speed\t\n200 kts 230 mph\t370 kmh\n\nCruise Speed\t\n178 kts 205 mph \t330 kmh\n\nEngine\t\nTextron Lycoming AEIO-540 L1B5 300 hp\n\nPropeller\nThree-bladed constant speed\n\nMaximum Range\t\n415 nm 478 sm \t769 km\n\nService Ceiling\t\n16,000 ft \t4,877 m\n\nFuel Capacity\t\n42.3 U.S. gal\t160 L \n\nEmpty Weight\t\n1,470 lb \t\t667.8 kg\n\nMaximum Gross Weight\t\n2,095 lb \t\t950 kg\n\nLength\t\n23.36 ft\t\t7.12 m\n\nWingspan\t\n26.25 ft\t\t8 m\n\nHeight\t\n8.6 ft \t\t2.62 m\n\nFAA Certified Load Factor\t\n+\/- 10 G\n\nSeating\t \n1 \n\nUseful Load\t\n625 lb \t283.5 kg\n
[WEIGHT_AND_BALANCE]
max_gross_weight = 2095 // (pounds)
empty_weight = 1345 // (pounds)
reference_datum_position = 1.8, 0, 0 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -1.4, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 170, -5.9, 0.0, 0.0 //Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 1717
empty_weight_roll_MOI = 1395
empty_weight_yaw_MOI = 1856
empty_weight_coupled_MOI = 0.0
[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus = 0, 10, 9.5
avionics = 1, 5 , 9.5
additional_system = 0, 20, 9.5
marker_beacon = 1, 2 , 9.0
fuel_pump = 0, 5 , 9.0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[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=10 // degrees
flaps-position.2=20 // degrees
flaps-position.3=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
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 2.0, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0 //Fuel flow scalar
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 90.3 //Cubic inches per cylinder
compression_ratio= 8.7 //Compression ratio
number_of_cylinders=12 //Number of cylinders
max_rated_rpm= 2700 //Max rated RPM
max_rated_hp= 2300 //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= 0.3 //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= 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= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.2 //Propeller Diameter, (feet)
propeller_blades= 3 //Number of propeller blades
propeller_moi= 5.9 //Propeller moment of inertia
beta_max= 34 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 17 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1400 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.0 //Propeller gear reduction ratio
fixed_pitch_beta= 0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80 //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)
[autopilot]
autopilot_available=1
use_no_default_bank=1
use_no_default_pitch=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=0.000000
pitch_takeoff_ga=8.000000
//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, 5.48, 0.0, -4.40, 1181.1, 0, 0.522, 22.0, 0.3, 2.5, 0.7, 3.5, 3.5, 0, 0.0, 0.0
point.1=1, -5.02, -6.5, -4.30, 1574.8, 1, 0.522, 0.0, 0.3, 2.5, 0.7, 4.7, 4.7, 2, 0.0, 0.0
point.2=1, -5.02, 6.5, -4.30, 1574.8, 2, 0.522, 0.0, 0.3, 2.5, 0.7, 5.2, 5.2, 3, 0.0, 0.0
point.3=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.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, 6, 0.0, 0.0
point.5=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.6=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.7=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.8=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
static_pitch=3.82
static_cg_height=2.91
static_pitch = 10.54
static_cg_height = 3.45
[Views]
eyepoint = -7.00, 0.00, 2.4
[SMOKESYSTEM]
smoke.0=0.00, 1.70, 1.40, fx_smoke_w
[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 = 140, 240
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 = 3, 1.62, -13.58,-0.15, fx_navred
light.1 = 3, 1.62, 13.58,-0.15, fx_navgre
light.2 = 2, 1.02, -13.58,-0.15, fx_strobe
light.3 = 2, 1.02, 13.58,-0.15, fx_strobe
light.4 = 1, -13.85, -05.10,-0.55, fx_navred
light.5 = 1, -13.85, 05.10,-0.55, fx_navred
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
Center1 = -2.6, 0.0, 0.0, 11.1, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2 = -0.6, 0.0, 0.0, 2.3, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -1.8, -2.1, -0.8, 15.9, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -1.8, 2.1, -0.8, 15.9, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
[airplane_geometry]
wing_area = 112.0 //Square feet
wing_span = 24.6 //Feet
wing_root_chord = 4.8 //Feet
wing_dihedral = 2.6 //Degrees
wing_incidence = 0.0 //Degrees
wing_twist = 0.0 //Degrees
oswald_efficiency_factor= 0.6 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 3.0 //Degrees, wing leading edge
wing_pos_apex_lon = -0.7 //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 = 28.0 //Square feet
htail_span = 10.5 //Feet
htail_pos_lon = -13.1 //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 = 0.0 //Degrees
htail_sweep = 10.0 //Degrees, horizontal tail leading edge
vtail_area = 15.0 //Square feet
vtail_span = 4.4 //Feet, tip to body
vtail_sweep = 20.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -14.3 //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 = 10.0 //Square feet
aileron_area = 18.4 //Square feet
rudder_area = 7.0 //Square feet
elevator_up_limit = 26.0 //Degrees
elevator_down_limit = 26.0 //Degrees
aileron_up_limit = 30.0 //Degrees
aileron_down_limit = 30.0 //Degrees
rudder_limit = 30.0 //Degrees
elevator_trim_limit = 15.0 //Degrees
spoiler_limit = 0.0 //Degrees
spoilerons_available = 0 //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 = 55.0 //Knots True (KTAS)
cruise_speed = 178.0 //Knots True (KTAS)
[autopilot]
autopilot_available= 0
flight_director_available= 0
