;*************************************************************************************************************** ;*Water handling* ;The real UWD had poor water handling. For maximum realism manoeuvre on the water with asymmetric power only. ;Water rudders were not available in the real UWD but they are provided for use in FS2002 ;Extend and retract water rudders with SHIFT + W ;Do not exceed 15 knots with water rudders extended or you may fracture a float strut leading to loss of control. ;*************************************************************************************************************** [fltsim.0] title=Gotha UWD sim=GOTHA-UWD model= panel= sound= texture= checklists= ui_manufacturer=Gothaer Waggonfabrik A.G. ui_type=G-1 Ursinus Wasser Doppeldecker ui_variation=Kreigsmarine Nr120 kb_reference=G-1UWD_ref description=The Gotha Ursinus long-range maritime reconnaissance seaplane was the original design from which the Gotha Grossflugzeug series was developed. Designed by Oskar Ursinus in 1914 and built under licence by the Gothaer Waggonfabrik it was not delivered until February 1916. [General] performance=Two 172 hp 6-cyl Mercedes D.III\nCruise climb at full throttle\nTrim with throttle\nReduce rpm to obtain level flight\n [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 max_number_of_stations=3 ;MTOW=6225 empty_weight=4260 station_load.0=650,-1.5,0,0 ;crew plus parabellum and ammo ;********************************************************************************************************************* ; ;Torpedo trials and training aircraft - when carrying torpedo only 2 crew and reduced fuel ;Normal fuel and oil=290Kg = 639lbs / 5.9 = 108 USG ;Maximum fuel and oil was 1145lbs as in G-I but use of more than 290Kg depended on sea state ;in these FDE normal fuel is loaded with 3 crew for coastal patrol ;********************************************************************************************************************* ;Moments of Inertia ;all approx empty_weight_roll_MOI=75000 empty_weight_pitch_MOI=28000 empty_weight_yaw_MOI=52000 empty_weight_coupled_MOI=0.000000 [fuel] ;Max tankage 194 USG including oil but default load is 108 USG allowing operation from the sea with modest swell ;German aviation fuel in 1916 about 55 Octane and had density about 5.9lbs per US gallon (set in air file) ;Oil tanks included in the fuel tankage as these engines consumed significant amounts of oil per flight ; center1=1,0,0,100,8 ;100 can be increased up to 186 if weather conditions permit fuel_type=1.000000 number_of_tank_selectors=1 [GeneralEngineData] engine_type=0 Engine.0=6.000000,-5.000000,0.500000 Engine.1=6.000000,5.000000,0.500000 fuel_flow_scalar=1.10000 ;including oil consumption [piston_engine] ;2 x Mercedes D.III class 3 engines each 172hp at 1420 rpm for combat ; cylinder_displacement=150.3 ;huge cylinders compression_ratio=4.73 number_of_cylinders=6 max_rated_rpm=1420 max_rated_hp=172 ;combat rating fuel_metering_type=1 cooling_type=0 normalized_starter_torque=0.300000 turbocharged=0 max_design_mp=0.000000 min_design_mp=0.000000 critical_altitude=0.000000 emergency_boost_type=0 emergency_boost_mp_offset=0.000000 emergency_boost_gain_offset=0.000000 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.000000 idle_rpm_mechanical_efficiency_scalar=1.000000 max_rpm_friction_scalar=1.000000 idle_rpm_friction_scalar=1.000000 [propeller] propeller_type=1 propeller_diameter=8.25 propeller_blades=2 propeller_moi=8.7 beta_max=25 beta_min=25 min_gov_rpm=1400.000000 prop_tc=0.100000 gear_reduction_ratio=1.000000 fixed_pitch_beta=25.0 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [airplane_geometry] wing_area=882.6 wing_span=72.2 wing_root_chord=6.12 wing_dihedral=2.8 wing_incidence=6.0 wing_twist=0 oswald_efficiency_factor=0.6 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=167.000000 htail_span=25.833333 htail_pos_lon=-34.166667 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=97.000000 vtail_span=11.229426 vtail_sweep=0.000000 vtail_pos_lon=-35.666667 vtail_pos_vert=1.500000 elevator_area=71.810000 aileron_area=102.900000 rudder_area=33.950000 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=60 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 //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 / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal [contact_points] point.0=4,15,8 ,-7.7,1575,0,0,0,0.5,2.5,0.7,0,0,0,0,0 point.1=4,15,-8 ,-7.7,1575,0,0,0,0.5,2.5,0.7,0,0,1,0,0 point.2=4,-15,-8,-7.1,1575,0,0,0,0.5,2.5,0.7,0,0,2,0,0 point.3=4,-15,8 ,-7.1,1575,0,0,0,0.5,2.5,0.7,0,0,3,0,0 point.4=2,-1.66,-36.0,-0.666,1574,0,0,0,0,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.5=2,-1.66,36.0,-0.666,1574,0,0,0,0,0,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.6=2,-35.6,0,0,1574,0,0,0,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.7=2,6.666,0,-0.666,1574,0,0,0,0,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 point.8=5, -15, -8, -8, 1800, 0, 0, 20, 0, 0, 1, 1, 1, 0, 0, 0 point.9=5, -15, 8, -8, 1800, 0, 0, 20, 0, 0, 1, 1, 1, 0, 0, 0 static_pitch=0.2 static_cg_height=7.6 [Reference Speeds] ;all IAS flaps_up_stall_speed=40 full_flaps_stall_speed=40 cruise_speed=48 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [autopilot] ;for beta testing only autopilot_available=0 use_no_default_bank=1 use_no_default_pitch=1 flight_director_available=0 default_vertical_speed=100.000000 autothrottle_available=0 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=0.000000 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=1,0 [Views] eyepoint=-5,0,6.2