[fltsim.0]
title=DFS 230 Eben Emael
sim=dfs230p
model=2
panel=
sound=
texture=eben
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=DFS (Deutsche Forschungsanstalt fur Segelflug)
ui_type="230 Assault Glider" V0.2
ui_variation=A-1,Eben-Emael,10 May 1940.
description=A total of 41 gliders were launched on May 10, 1940 for this mission. In each of them sat 10 paratroopers. The first group (85 men, code name "Granite", armed with handguns and 500Kgs explosives, mostly hollow and stick grenades)were under the command of Oberleutnant Witzig. This group utilized seven gliders. It was their task to take the Belgian Fort Eben Emael (near Maastrich) and hold it until the first army units, a group of 51st Engineer Battalion arrived. Thus the crossing of the Albert Canal was to be secured. The second group (96 men, code name "Beton"), under Leutnant Schacht, used eleven planes. The third group (92 men, code name "Stahl"), under Oberleutnant Altmann, with nine gliders was augmented by the fourth group (90 men, code name "Eisen"), under Leutnant Schachter, with ten '230. The most successful group was that of Oberleutnant Witzig, though it landed directly on the fort without its leader, his glider had to release prematurely and landed near Duren. Witzig was able, though, to obtain a new Ju 52 and fly on behind his group. He landed under the Belgian artillery fire, the battle was in full swing. Only on the next morning the engineers was able to meet Witzig's group. With that, the cornerstone of Belgian defense was in German hands.
atc_id_color=0000000000
visual_damage=0
[fltsim.1]
title=DFS 230 Regia Aeronautica
sim=dfs230p
model=1
panel=
sound=
texture=ra
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=DFS (Deutsche Forschungsanstalt fur Segelflug)
ui_type="230 Assault Glider" V0.2
ui_variation=A-1,Regia Aeronautica
description=The Royal Italian Air Force (Regia Aeronautica) received from Luftwaffe,during 1941,almost 20 DFS-230 and 4 Gotha Go-242 assault gliders. These aircrafts were used only for pilots training until 09/1943.
atc_id_color=0000000000
visual_damage=0
[fltsim.2]
title=DFS 230 LLG-1 H4+2-27
sim=dfs230p_ch
model=3
panel=
sound=
texture=llg127
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=DFS (Deutsche Forschungsanstalt fur Segelflug)
ui_type="230 Assault Glider" V0.2
ui_variation=B-1,H4+2-27
description=An aircraft of LLG-1 believed to have been used to carry men of 7/KG200 to Vassieux, during the operations on the Vercors Source. All the gliders of B-1's type were equipped with a drag chute in order to reduce the landing spaces.
atc_id_color=0000000000
visual_damage=0
[fltsim.3]
title=DFS 230 LLG-1 H4+2-13
sim=dfs230p_ch
model=4
panel=
sound=
texture=llg113
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=DFS (Deutsche Forschungsanstalt fur Segelflug)
ui_type="230 Assault Glider" V0.2
ui_variation=B-1,H4+2-13
description=Another aircraft of LLG-1 believed to have been used to carry men of 7/KG200 to Vassieux, during the operations on the Vercors Source. All the gliders of B-1's type were equipped with a drag chute in order to reduce the landing spaces, many of them were equipped also with a third escape door and two alternative tow systems, with traditional cables or a rigid system (a short towing bar with universal joints).
atc_id_color=0000000000
visual_damage=0
[fltsim.4]
title=DFS 230 Gran Sasso 1943
sim=dfs230p_ch
model=5
panel=
sound=
texture=eichen
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=DFS (Deutsche Forschungsanstalt fur Segelflug)
ui_type="230 Assault Glider" V0.2
ui_variation=C-1,Eiche Operation 12 Sept 1943
description=The DFS 230's last important operation was to deliver the group of hand picked commandos led by Otto Skorzeny against the mountain-top hotel that was used to hold Mussolini. All the gliders used during 'Eiche' operation were C-1 version, armed with a MG34 and equipped with drag chute and three brake rockets in the nose,in order to reduce the landing spaces.
atc_id_color=0000000000
visual_damage=0
[General]
atc_type=DFS
atc_model=230
editable=1
performance="Maximum Speed\t\n180 mph 290 kmh\n\nEngine\t\nnone\n\nGlide Ratio\t\n18 to 1\n\nEmpty Weight\t\n1880 lb 860 kg\n\nLength\t\n37.1 ft \t 11.24 m\n\nWingspan\n72.5 ft\t 21.97 m\n\nWing Area\t\n453 sq ft \t 41.26 m2\n\nAspect Ratio\t\n18.05\n\nMaximum L\/D (Calculated) \t\n~57 kts ~66 mph ~106 kmh\n\nMinimum Sink (Calculated) \t\n~47 kts ~54 mph\t ~87 kmh\n\nSeating\t\n 9\n\nUseful Load\t\n2700 lb \t1240 kg"
[weight_and_balance]
// ACM V2.3
max_gross_weight = 4608
empty_weight = 1896
reference_datum_position = 1, 0, 0
empty_weight_CG_position = -1, 0, 0
empty_weight_pitch_MOI = 3170
empty_weight_roll_MOI = 4703
empty_weight_yaw_MOI = 6775
empty_weight_coupled_MOI = 0
max_number_of_stations = 10
station_load.0 = 271.2, 6.15, 0, 1.93
station_load.1 = 271.2, 3.90, 0, 1.57
station_load.2 = 271.2, 2.58, 0, 1.51
station_load.3 = 271.2, 1.26, 0, 1.5
station_load.4 = 271.2, 0.06, 0, 1.54
station_load.5 = 271.2, -1.39, 0, 1.49
station_load.6 = 271.2, -2.62, 0, 1.47
station_load.7 = 271.2, -3.94, 0, 1.37
station_load.8 = 271.2, -5.42, 0, 1.41
station_load.9 = 271.2, -6.57, 0, 1.34
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4, 5.55, 0, 3.49, fx_vclight
light.1 = 3, -1.2, -33.41, 5.9, fx_navredsml
light.2 = 3, -1.20, 33.40, 5.90, fx_navgresml
light.3 = 3, -26.27, 0, 2.32, fx_navwhisml
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_tchdwn_s
touchdown = fx_tchdwn_s, 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 0
[contact_points]
static_pitch = 4.82
static_cg_height = 2.29
tailwheel_lock = 0
max_number_of_points = 9
point.0 = 1, -22.2526, 0, 0.4931, 3200, 0, 0.3, 0, 0.4, 2.5, 0.5, 0, 0, 4, 0, 0
point.1 = 1, -0.2923, -1.8528, -1.9587, 2200, 1, 1.05, 0, 0.5, 2.5, 0.83, 1, 1, 2, 0, 0
point.2 = 1, -0.2973, 1.8171, -1.9587, 2200, 2, 1.05, 0, 0.5, 2.5, 0.83, 1, 1, 3, 0, 0
point.3 = 2, -2.2009, 33.4062, 5.5518, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.4 = 2, -23.9555, 0, 0.9053, 2400, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.5 = 2, 10.3457, 0, 1.3888, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.6 = 2, -2.1944, -33.4219, 5.5506, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.7 = 4, 2.359, -0.586, -0.9119, 2200, 1, 0.6, 0, 0.5, 2.5, 0.83, 2, 2, 4, 0, 0
point.8 = 4, 2.3595, 0.586, -0.9128, 2200, 2, 0.6, 0, 0.5, 2.5, 0.83, 2, 2, 4, 0, 0
gear_system_type=0
[keyboard_response]
elevator = 160, 360
aileron = 160, 360
rudder = 160, 360
[forcefeedback]
gear_bump_nose_magnitude = 1000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 450
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 2000
crash_direction1 = 1000
crash_magnitude2 = 2000
crash_direction2 = 9000
crash_period2 = 7500
crash_duration2 = 2500000
stick_shaker_magnitude = 2000
stick_shaker_direction = 0
stick_shaker_period = 111111
[airplane_geometry]
//ACM_AREAW1// -0.0012,-0.0012,-0.4444,2.6157,0.9835,0.9835,-0.3862,2.4842,1.4400,1.4400
//ACM_AREAW2// -0.3519,2.4326,9.3065,9.3065,0.1921,1.4594,9.8079,9.8079,0.2266,1.3256
//ACM_AREAW3// 10.0516,10.0516,0.2533,1.2036,10.1878,10.1878,0.2967,1.0994,10.2811,10.2811
//ACM_AREAW4// 0.3770,0.9947,10.3366,10.3366,0.4611,0.8970,10.3830,10.3830,0.6577,0.6990
//ACM_AREAH1// 0.0003,0.0003,-1.3974,-0.2483,0.1430,0.1430,-1.3653,-0.2289,0.2504,0.2504
//ACM_AREAH2// -1.3430,-0.0173,0.3702,0.3702,-1.3178,0.2231,1.8523,1.8523,-1.0137,0.0010
//ACM_AREAH3// 2.0573,2.0573,-0.9674,-0.0315,2.1665,2.1665,-0.9373,-0.0860,2.2211,2.2211
//ACM_AREAH4// -0.8931,-0.1395,2.2583,2.2583,-0.8453,-0.1958,2.2957,2.2957,-0.6523,-0.4318
//ACM_AREAV1// -0.6197,-0.6197,2.1977,2.2806,-0.5569,-0.5569,2.1949,3.1375,-0.5180,-0.5180
//ACM_AREAV2// 2.1953,3.1863,-0.4693,-0.4693,2.1967,3.1970,0.1993,0.1993,1.5700,3.0787
//ACM_AREAV3// 1.2021,1.2021,1.7795,2.8996,1.3608,1.3608,1.8126,2.8401,1.4684,1.4684
//ACM_AREAV4// 1.8365,2.7530,1.5506,1.5506,1.8638,2.6412,1.6654,1.6654,2.0071,2.3559
//ACM_CAREAW1// 4.4298,4.4298,1.4938,2.0501,9.2860,9.2860,0.9854,1.4621,9.5136,9.5136
//ACM_CAREAW2// 0.9634,1.4005,9.7115,9.7115,0.9387,1.3449,9.8512,9.8512,0.9218,1.2962
//ACM_CAREAW3// 9.9741,9.9741,0.8944,1.2409,10.0860,10.0860,0.8705,1.1696,10.1794,10.1794
//ACM_CAREAW4// 0.8457,1.0973,10.2643,10.2643,0.8288,1.0188,10.3521,10.3521,0.8141,0.8718
//ACM_CAREAH1// 0.0093,0.0093,-0.4192,-0.2324,0.1377,0.1377,-0.4144,-0.2337,0.3700,0.3700
//ACM_CAREAH2// -0.4097,0.2307,0.7275,0.7275,-0.4052,0.1826,1.0197,1.0197,-0.4004,0.1342
//ACM_CAREAH3// 1.2933,1.2933,-0.4004,0.0961,1.7444,1.7444,-0.4004,0.0294,2.1203,2.1203
//ACM_CAREAH4// -0.4052,-0.0511,2.1236,2.1236,-0.9319,-0.0524,2.2899,2.2899,-0.7972,-0.2590
//ACM_CAREAV1// -0.6266,-0.6266,2.2146,2.2667,-0.5576,-0.5576,2.2197,3.1310,-0.5192,-0.5192
//ACM_CAREAV2// 2.2197,3.1900,-0.4762,-0.4762,2.2197,3.1988,0.6758,0.6758,2.2197,2.9948
//ACM_CAREAV3// 1.2036,1.2036,2.2197,2.8933,1.3573,1.3573,2.2197,2.8417,1.4730,1.4730
//ACM_CAREAV4// 2.2197,2.7504,1.5650,1.5650,2.2197,2.6175,1.6639,1.6639,2.2197,2.3863
wing_area = 452.8
wing_span = 68.97
wing_root_chord = 4.59
wing_dihedral = 3.5
wing_incidence = 3.0
wing_twist = -2.0
oswald_efficiency_factor = 1.0
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = -0.5
wing_pos_apex_vert = 3.98
htail_area = 58.78
htail_span = 15.43
htail_pos_lon = -23.43
htail_pos_vert = 0
htail_incidence = 0.0
htail_sweep = 0
vtail_area = 28.92
vtail_span = 4.69
vtail_sweep = 0
vtail_pos_lon = -16
vtail_pos_vert = 3.89
elevator_area = 22.93
aileron_area = 62.12
rudder_area = 19.01
elevator_up_limit = 26.0
elevator_down_limit = 26.0
aileron_up_limit = 30.0
aileron_down_limit = 30.0
rudder_limit = 30.0
elevator_trim_limit = 15.0
spoiler_limit = 70.0
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 0
avionics = 2, 5, 17
additional_system = 2, 20, 17
light_nav = 2, 5, 17
light_panel = 2, 5, 17
[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
[pitot_static]
vertical_speed_time_constant = 4 //Increasing this value will cause a more instantaneous reaction in the VSI
//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
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.67 //Brake scalar
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint=5.990, 0.0, 4.150
[flaps.0]
type = 0 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 0 // seconds
flaps-position.0 = 0 // degrees, KIAS
damaging-speed = 250 // KIAS
blowout-speed = 300
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=0
Com.1=1, 0
Nav.1=0, 0, 0
Adf.1=0
Transponder.1=0
Marker.1=0
[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=0,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 0
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[Reference Speeds]
flaps_up_stall_speed=40.0 //Knots True (KTAS)
full_flaps_stall_speed=40.0 //Knots True (KTAS)
cruise_speed=47.0 //Knots True (KTAS)
max_indicated_speed = 158 //Red line (KIAS)
[autopilot]
autopilot_available=0
flight_director_available=0
[yaw_string]
yaw_string_available=1
[stall_warning]
type=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[TailHook]
tailhook_length = 4
tailhook_position =-23.5321, 0.000, -1.000
cable_force_adjust = 1
[GeneralEngineData]
engine_type=2
fuel_flow_scalar=1.000000