[fltsim.0]
title=SF25C D-KOII Deutsch
sim=SF25C-D-KOII
model=
panel=
sound=
texture=
kb_checklists=sf25c_D-KOII_check
kb_reference=SF25C_D-KOII_ref
ui_manufacturer="Scheibe"
ui_type="SF25C D-KOII"
ui_typerole="Motorglider"
ui_createdby"Wolfgang Piper & Mathias Elsaesser"
ui_variation="Deutsch"
visual_damage=1
atc_heavy=0
atc_id=D-KOII
atc_model=Sportsaircraft
ATC_type=FA10
atc_airline=
atc_flight_number=
description="Scheibe SF 25 C "Esslinger Falke" \n mit 2-Bein-Fahrwerk \nMotor: 100 PS Rotax"
[fltsim.1]
title=SF25C D-KOII English
sim=SF25C-D-KOII
model=
panel=
sound=
texture=
kb_checklists=sf25c_D-KOII_check_en
kb_reference=SF25C_D-KOII_ref
ui_manufacturer="Scheibe"
ui_type="SF25C D-KOII"
ui_typerole="Motorglider"
ui_createdby"Wolfgang Piper & Mathias Elsaesser"
ui_variation="English"
visual_damage=1
atc_heavy=0
atc_id=D-KOII
atc_model=Sportsaircraft
ATC_type=FA10
atc_airline=
atc_flight_number=
description="Scheibe SF 25 C "Esslinger Falke" \n with taildragger undercarriage \nMotor: 100 PS Rotax"
[General]
performance=Länge/Length: 7.6 m \nSpannweite/Wingspan: 15.25m \nGewicht/Weight: 647 kg max, 455 kg leer/empty\nDesigner: Wolfgang Piper, Mathias Elsaesser, 03/2010
Category=airplane
[WEIGHT_AND_BALANCE]
reference_datum_position=0.0000, 0.0000, 0.0000
empty_weight_CG_position=-0.50000,0.000000,0.000000
max_number_of_stations=5
station_load.0=170,1.00000,-1.300000,0.000000
station_load.1=170,1.00000,1.300000,0.000000
empty_weight=1007.511000
empty_weight_roll_MOI=700.000000
empty_weight_pitch_MOI=2200.000000
empty_weight_yaw_MOI=900.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=1433.003000
CG_forward_limit = 0
CG_aft_limit = 1
[GeneralEngineData]
engine_type=0
Engine.0=6, 0.0, 0.0
fuel_flow_scalar=2.728
min_throttle_limit=0.000000
[piston_engine]
power_scalar=1.00
cylinder_displacement=75
compression_ratio=7.0
number_of_cylinders=3
max_rated_rpm=2700
max_rated_hp=350
fuel_metering_type=1
cooling_type=1
normalized_starter_torque=0.3
turbocharged=0
max_design_mp=0
min_design_mp=0
critical_altitude=0
emergency_boost_type=0
emergency_boost_mp_offset=0
emergency_boost_gain_offset=0
fuel_air_auto_mixture=1
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.51
idle_rpm_mechanical_efficiency_scalar=1.35
max_rpm_friction_scalar=1.0
idle_rpm_friction_scalar=1.1
[propeller]
thrust_scalar=0.7
propeller_type=0
propeller_diameter=5.0
propeller_blades=2
propeller_moi=2.0
beta_max=45.0
beta_min=14.0
min_gov_rpm=1970
prop_tc=0.06
gear_reduction_ratio=1.0
fixed_pitch_beta=26
low_speed_theory_limit=70
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=1
prop_auto_feathering_available=0
min_rpm_for_feather=700
beta_feather=-90
power_absorbed_cf=0.2
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=14
minimum_reverse_beta=0
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus = 0, 5 , 9.0
avionics = 1, 5 , 9.0
additional_system = 0, 4 , 9.0
fuel_pump = 0, 5 , 9.0
starter1 = 0, 50, 10.0
light_beacon = 0, 5 , 9.0
light_panel = 0, 5 , 9.0
max_battery_voltage = 13.5
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40
[airplane_geometry]
wing_area=200.000000
wing_span=55.000000
wing_root_chord=5.0
wing_dihedral=0
wing_incidence=-2.5
wing_twist=-0.999756
oswald_efficiency_factor=0.7
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=1.000000
wing_pos_apex_vert=0.000000
htail_area=27.000000
htail_span=9.583333
htail_pos_lon=-13.750000
htail_pos_vert=1.000000
htail_incidence=-3.0
htail_sweep=0.000000
vtail_area=15.000000
vtail_span=6.745369
vtail_sweep=0.000000
vtail_pos_lon=-15.000000
vtail_pos_vert=3.916667
elevator_area=9.0
aileron_area=11.900000
rudder_area=9
elevator_up_limit=20
elevator_down_limit=30
aileron_up_limit=25
aileron_down_limit=10
rudder_limit=30
elevator_trim_limit=20
spoiler_limit=40
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
auto_spoiler_available=0
spoiler_extension_time=0.500000
positive_g_limit_flaps_up=5.500000
positive_g_limit_flaps_down=5.500000
negative_g_limit_flaps_up=-3.500000
negative_g_limit_flaps_down=-3.500000
[flight_tuning]
cruise_lift_scalar=1.3
parasite_drag_scalar=1.40
induced_drag_scalar=0.2
elevator_effectiveness=0.8
aileron_effectiveness=0.8
rudder_effectiveness=1.1
pitch_stability=1.2
roll_stability=1.1
yaw_stability=0.9
elevator_trim_effectiveness=1.9
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[fuel]
Center1 = 4.5, 0.000, 1.000, 14.53, 0.000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=1
[contact_points]
//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
// Lang. Breit. Vert.
// Pos. Pos. Pos.
// 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
//--------------------------------------------------------------------------------------------------------------------------------
point.1 =1, -15.32, 0, -0.660, 1500, 0, 0.3, 180, 0.06, 10, 0.6, 0, 0, 0, 0, 0 // Gear Tail
point.2 =1, 1.62, -2.99, -3.0 , 1500, 1, 0.623, 0, 0.3, 2.5, 1, 0, 0, 2, 0, 0 // Gear left
point.3 =1, 1.62, 2.99, -3.0 , 1500, 2, 0.623, 0, 0.3, 2.5, 1, 0, 0, 2, 0, 0 // Gear right
point.4 =2, 5.738, 0, -2.2, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0, , // scrape front
point.5 =2, -14.78, 0, -0.302, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0, , // Tail
point.6 =2, 1.178, 25.174, 1.086, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 5, , // wing right
point.7 =2, 1.178, -25.17, 1.086, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 6, , // wing left
static_pitch = 7.0
static_cg_height=2.5
tailwheel_lock = 1
[Views]
eyepoint=0.48, -0.78, 1.80
[Reference Speeds]
flaps_up_stall_speed=38.000000
full_flaps_stall_speed=38.000000
cruise_speed=86
max_indicated_speed=120
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=0
Com.1=1, 1
Com.2=0, 1
Nav.1=0, 1, 1
Nav.2=0, 1, 0
Adf.1=0
Transponder.1=1
Marker.1=0
[autopilot]
use_no_default_bank=1
use_no_default_pitch=1
autopilot_available=0
flight_director_available=1
default_vertical_speed=700.000000
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
default_pitch_mode=0
default_bank_mode=0
[direction_indicators]
direction_indicator.0=2,0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
// long lat vert
light.0 = 1, -16.28, 0.00, 5.22, fx_beacon ;LTW oben
light.1 = 4, 1, 0.00, 0.5, fx_vclight ;Cockpit
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=2.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=39.992454,0.000000
[brakes]
toe_brakes_scale=1.0
parking_brake=1
//differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure=0.000000
electric_pumps = 0 //no electric pumps
[stall_warning]
type=1
stick_shaker=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[pitot_static]
pitot_heat=0.000000
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,1,1
