//************************************************************* Zeppelin Staaken L prototype with Mercedes D.IVa engines (1917) //************************************************************* // Do not attempt to edit this file with FSedit! - use notepad or wordpad [fltsim.0] title=Staaken L 1917 sim=RVIWD model= panel= sound= texture= checklists= kb_checklists= kb_reference=L_ref description=Zeppelin Staaken L. 1917 Giant Seaplane version of the R.VI, with 4 x 267 Hp Mercedes D.IVa high compression engines, altitude rated at 1450 RPM at 1300 metres, capable of payloads of upto 2 tonnes. It was the first aircraft to be fitted with cannon. atc_airline= atc_flight_number= ui_manufacturer=Zeppelin Werke ui_type=Staaken L ui_variation=Giant Seaplane atc_heavy=0 atc_id= [General] performance=Length: 72 ft 6 in\nWing span: 138 ft 5 in\nWeight: 26,066 lbs\nPower: 4 x 267 Hp Mercedes D-IVa 6-cyl.\nMax. speed 135 Kph\nDetails:WW I Bomber\nMax. Load 2 tonnes\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 empty_weight=18500 ;ready for service including engine coolant etc station_load.0=1000,0,0,0 ;5 crew including flying clothing station_load.1=500,0,0,0 ;machine guns and ammo ;********************************************************************************************************** ;18500 + 1500 + 6000 = 26,000lbs max and default ;*********************************************************************************************************** ;Moments of Inertia empty_weight_roll_MOI=950000 empty_weight_pitch_MOI=350000 ;45 empty_weight_yaw_MOI=620000 empty_weight_coupled_MOI=0 [fuel] ; ;Max tankage including oil 1000 USG @ 6lbs=6000lbs ; ;Oil tanks included in the fuel tankage as these engines consumed 40+ Kg oil per flight ; LeftMain=15,0,0,200,0 center1=0,0,0,400,0 RightMain=-12,0,0,400,0 ;This is the aft tank ;tanks are defined left/center/right only to match available gauges so that you can monitor contents they are arranged fore and aft on the centreline simulating the eight real tanks used for trimming ; fuel_type=1.000000 number_of_tank_selectors=1 [GeneralEngineData] engine_type=0 Engine.0=12.66,-12.9,1.66 Engine.1=-7.25,-12.9,1.66 Engine.2=12.66,12.9,1.66 Engine.3=-7.25,12.9,1.66 fuel_flow_scalar=1.065 [piston_engine] ;Mercedes D.IVa is a throttle gated HC engine rated 267hp at 1450rpm at 4300 feet cylinder_displacement=220.6 ;huge cylinders compression_ratio=4.82 ;high compression does not allow full rpm at sea level number_of_cylinders=6 max_rated_rpm=1450 max_rated_hp=267 fuel_metering_type=1 cooling_type=0 normalized_starter_torque=0.300000 turbocharged=1 ;turbocharger used to mimic throttle gated HC Zeppelin engine max_design_mp=30.000000 min_design_mp=0.000000 critical_altitude=4300 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] gear_reduction_ratio=1.0 ;props turn at engine speed fixed_pitch_beta=25.000000 ;actual pitch irrelevant - 1917 prop data placed in 25 degree look up table propeller_type=1 propeller_diameter=9.1 ;set to give correct thrust in FS2002 propeller_blades=2 propeller_moi=5 beta_max=25 beta_min=25 min_gov_rpm=400.000000 prop_tc=0.100000 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] oswald_efficiency_factor=0.675 wing_area=3573 wing_span=138.33 wing_root_chord=12.95 wing_dihedral=0 wing_incidence=6.0 ;estimated wing_twist=0 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=160.000000 htail_span=24.000000 htail_pos_lon=-48.000000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=120.000000 vtail_span=12.489996 vtail_sweep=0.000000 vtail_pos_lon=-48.000000 vtail_pos_vert=15.000000 elevator_area=71.810000 aileron_area=130.000000 rudder_area=100.000000 elevator_up_limit=27.501974 elevator_down_limit=20.626481 aileron_up_limit=17.188734 aileron_down_limit=17.188734 rudder_limit=12.934522 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 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=16.5,-2,1 [direction_indicators] direction_indicator.0=1,0 [Reference Speeds] flaps_up_stall_speed=40 full_flaps_stall_speed=40 cruise_speed=50 [contact_points] point.0=4,-20,-11.3,-11.5,6000,0,0,0,0.5,2.5,0.2,0,0,0,0,0 point.1=4,-20,11.3,-11.5 ,6000,0,0,0,0.5,2.5,0.2,0,0,1,0,0 point.2=4,20,-11.3,-11.5 ,6000,0,0,0,0.5,2.5,0.2,0,0,2,0,0 point.3=4,20,11.3,-11.5 ,6000,0,0,0,0.5,2.5,0.2,0,0,3,0,0 point.4=2.000000,-1.666667,-69.166667,5.916667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.5=2.000000,-1.666667,69.166667,5.916667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.6=2.000000,-48.000000,0.000000,6.583333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.7=2.000000,24.500000,0.000000,-5.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 point.8=5, -20, -11.3, -11, 1800, 0, 0, 20, 0, 0, 1, 1, 1, 0, 0, 0 point.9=5, -20, 11.3, -11, 1800, 0, 0, 20, 0, 0, 1, 1, 1, 0, 0, 0 static_pitch=0 static_cg_height=11 [autopilot] autopilot_available=0 flight_director_available=0
