[fltsim.0]
title=DG-101
sim=DG-100 V6
model=
panel=
sound=
texture=
kb_reference=dg-101_ref
kb_checklists=

ui_manufacturer=Glaser/Dirks
ui_type=DG-101
ui_typerole="Glider"
ui_createdby"Wolfgang Piper"
ui_variation=
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=
description="DG-101 G (gedämpftes Höhenleitwerk und einteilige Haube). Ein Leistungssegler der Standardklasse."


[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



[General]
performance=Spannweite: 15.0 m\nRüstgewicht: 235 kg,Max.Fluggewicht 418 kg\nBetes Sinken: 0.59m\/sec bei  74 km\/h\nBestes Gleiten 39.2  bei 105 km\/h\n
Category=airplane


[WEIGHT_AND_BALANCE]
reference_datum_position=0,0,0
empty_weight_CG_position=-1.2,0,0
max_number_of_stations=1
station_load.0="170,3,0,0,Pilot"
station_load.1="100,-0.5,0,0,Ballast"

empty_weight=519.000000
max_gross_weight=922.000000
empty_weight_roll_MOI=700.000000
empty_weight_pitch_MOI=800.000000
empty_weight_yaw_MOI=1000.000000
empty_weight_coupled_MOI=0.000000



[flight_tuning]

//cruise_lift_scalar=1.1
//parasite_drag_scalar=1.2
//induced_drag_scalar=0.70


cruise_lift_scalar=1.1
parasite_drag_scalar=1.10
induced_drag_scalar=0.9


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=2.0
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=118.000000
wing_span=49.0
wing_root_chord=2.8
wing_dihedral=1.499146
wing_incidence=0.000000
wing_twist=0.999756
oswald_efficiency_factor=0.756348
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=22.000000
htail_span=7.916667
htail_pos_lon=-13.750000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=22.000000
vtail_span=5.347897
vtail_sweep=0.000000
vtail_pos_lon=-13.750000
vtail_pos_vert=3.916667
elevator_area=9.460000
aileron_area=11.900000
rudder_area=7.700000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
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=0.400000
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,      0.3   , 2.5,    0.3344, 0.5,  0,    0,    0,    0    // Gear Tail
point.1=1, 0.75,   -0.2,  -2.15,   1574.8, 1,   0.5065,  0,      0.30,   2.5,    0.5117, 0.5,  0.8,  2,    0,    0    // Gear Main
point.2=1, 0.75,   0.2,   -2.15,   1574.8, 2,   0.5065,  0,      0.30,   2.5,    0.5117, 0.5,  0.8,  3,    0,    0    // Gear Main
point.3=2, -0.15, -24.3,  1.65,    1574.8, 0,   0,       0,      0,      0,      0,      0,    0,    5,    0,    0    // Wing Tip
point.4=2, -0.15,  24.3,  1.65,    1574.8, 0,   0,       0,      0,      0,      0,      0,    0,    6,    0,    0    // Wing Tip
point.5=2, -15.7,    0.0, 0.0,     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=6.5
static_cg_height=2.20
gear_system_type=0


[Views]
eyepoint=1.77,0.00,0.86


static_pitch=5
static_cg_height=1.333910
gear_system_type=0

[Reference Speeds]
flaps_up_stall_speed=41.000000
full_flaps_stall_speed=32.800000
cruise_speed=50
max_indicated_speed=152.734375
max_mach=0.229980


[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

[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

//[variometers]
//variometer.0=54,-116	


[Flaps.0]
type=0
span-outboard=0.500000
extending-time=0.000000
system_type=0

[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

[GeneralEngineData]
engine_type=2
fuel_flow_scalar=1.000000
[fuel]
fuel_type=1.000000
[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=13.21, 0.0, 0.0, 0.0, 1          //Water 50 l
Tank.1=13.21, 0.0, 0.0, 0.0, 1          //Water 50 l

NumberOfReleaseValves=2
DumpRate=0.18494                            //Gallons per second/ =42 l/min