[fltsim.0]
title=DG-202-17
sim=DG-202-17
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=DG-202_ref
kb_checklists=DG202_check
ui_manufacturer=Glaser/Dirks
ui_type=DG-202-17
ui_typerole="Glider"
ui_createdby"Wolfgang Piper"
ui_variation=Panel Standard
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=
description="DG202-17, Open Class glider. Designer: Wolfgang Piper, July 2009"
[fltsim.1]
title=DG-202-17 Holzpanel
sim=DG-202-17
model=
panel=Holz
sound=
texture=
kb_checklists=
kb_reference=DG-202_ref
kb_checklists=DG202_check
ui_manufacturer=Glaser/Dirks
ui_type=DG-202-17
ui_typerole="Glider"
ui_createdby"Wolfgang Piper"
Category=airplane
ui_variation=Panel Holz
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=
description="DG202-17, Open Class glider. Designer: Wolfgang Piper, July 2009"
[General]
performance=Span: 17 m\nEmpty Weight: 250 kg, Gross weight 450 kg\nMin. sink: 0.53 m/s at 75 km/h\nL/D max: 45.5 at 110 km/h\nV min: 70 km/h\nV max: 270 km/h
Category=airplane
[electrical]
max_battery_voltage=24
avionics_bus=0, 0 , 0
avionics=0, 0 , 0
additional_system=0, 0 , 0
flap_motor=0, 0 , 0
gear_motor=0, 0 , 0
[WEIGHT_AND_BALANCE]
reference_datum_position=0,0,0
empty_weight_CG_position=-1.80,0,0
max_number_of_stations=5
station_load.0="180, 0.8,0,0,Pilot"
empty_weight=525.000000
empty_weight_roll_MOI=1000.000000
empty_weight_pitch_MOI=2000.000000
empty_weight_yaw_MOI=800.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=993.000000
[flight_tuning]
cruise_lift_scalar=1.14
parasite_drag_scalar=1.1
induced_drag_scalar=1.82
elevator_effectiveness=1.25
aileron_effectiveness=1.1
rudder_effectiveness=1.1
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=3.5
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_tchdwn_s
touchdown=fx_tchdwn_s
[airplane_geometry]
wing_area=95
wing_span=55
wing_root_chord=3.4
wing_dihedral=1
wing_incidence=5
wing_twist=1
oswald_efficiency_factor=0.875082
wing_winglets_flag=1
wing_sweep=0.000000
wing_pos_apex_lon=-0.30
wing_pos_apex_vert=1.000000
htail_area=11.000000
htail_span=8
htail_pos_lon=-11
htail_pos_vert=0.000000
htail_incidence=4.500000
htail_sweep=0.000000
vtail_area=6
vtail_span=3
vtail_sweep=0.000000
vtail_pos_lon=-12
vtail_pos_vert=2
elevator_area=4
aileron_area=11.900000
rudder_area=3
elevator_up_limit=25
elevator_down_limit=25
aileron_up_limit=17
aileron_down_limit=10
rudder_limit=23.491270
elevator_trim_limit=35
spoiler_limit=59.988681
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
[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
// Long. Lat. Vert.
// Pos. Pos. Pos.
// 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
//--------------------------------------------------------------------------------------------------------------------------------
point.0=1, -14, 0, -0.45, 1574.8, 0, 0.5065, 0, 0.2 , 2.5, 0.3344, 0.5, 0, 0, 0, 0 // Gear Tail
point.1=1, 0.75, -0.01, -2.2, 1574.8, 1, 0.5065, 0, 0.20, 2.1, 0.5117, 0.5, 0.8, 2, 0, 0 // Gear Main
point.2=1, 0.75, 0.01, -2.2, 1574.8, 2, 0.5065, 0, 0.20, 2.1, 0.5117, 0.5, 0.8, 3, 0, 0 // Gear Main
point.3=2, -0.15, -28, 1.50, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 // Wing Tip
point.4=2, -0.15, 28, 1.50, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 // Wing Tip
point.5=2, -15.7, 0.0, 0.2, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 // Tail
point.6=2, 4.84, 0, -1.23, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 // Nose
//Converted with CPA V.1.05 by Wolfgang Piper
static_pitch=6.8
static_cg_height=2.2
gear_system_type=0
[Views]
eyepoint=1.77,0.00,0.86
gear_system_type=0
[GeneralEngineData]
engine_type=2
fuel_flow_scalar=1.000000
[Reference Speeds]
flaps_up_stall_speed=43.000000
full_flaps_stall_speed=39.00000
cruise_speed=50.0000
max_indicated_speed=250
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=3.000000
system_type=0
flaps-position.0=-12,0
flaps-position.1=-8,0
flaps-position.2=0,0
flaps-position.3=4,0
flaps-position.4=6,0
flaps-position.5=8,0
flaps-position.6=12,0 ;:L1
flaps-position.7=16,0 ;:L2
system_type = 3
lift_scalar = 1.0
drag_scalar = 0.5
pitch_scalar= -1.0
[keyboard_response]
elevator=60.000000,90.000000
aileron=60.000000,90.000000
rudder=60.000000,90.000000
[autopilot]
autopilot_available=0
flight_director_available=0
[direction_indicators]
direction_indicator.0=0,0
[fuel]
fuel_type=1.000000
[brakes]
toe_brakes_scale=1.000031
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
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=1
stick_shaker=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[pitot_static]
pitot_heat=0.000000
[vacuum_system]
max_pressure=0.000000
vacuum_type=0
electric_backup_pressure=0.000000
engine_map=1,1,1,1
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0
[Water Ballast System]
;/Tank.n = Gallons, Long, Lat, Vert, iValve
Tank.0=17.18, -1.8, 0.0, 0.0, 1 //Water 65 l
Tank.1=17.18, -1.8, 0.0, 0.0, 1 //Water 65 l
NumberOfReleaseValves=2
DumpRate=0.18494 //Gallons per second/ =42 l/min
