//********************************************** Zeppelin R.V with Maybach Mb.IVa engines (1918) //********************************************** // Do not attempt to edit this file with FSedit! - use notepad or wordpad [fltsim.0] title=Zeppelin R.V (5 x Maybach) sim=StaakenR41 model= panel= sound= texture= description=Zeppelin Staaken R.V - 1917 Riesenflugzeug with 5 x 245 Hp Maybach Mb.IVa high compression engines, altitude rated at 2500 metres, capable of payloads of upto 2 tonnes. ui_manufacturer=Zeppelin Werke ui_type=R-V ui_variation=1917 Haxagonal lozenge livery atc_heavy=0 checklists= kb_checklists= kb_reference=R-V_ref [General] performance=Length: 72 ft 6 in\nWing span: 138 ft 5 in\nWeight: 25,200 lbs\nPower: 5 x 245 Hp Maybach Mb.IVa 6-cyl [WEIGHT_AND_BALANCE] reference_datum_position=0.0,0.0,0.0 empty_weight_CG_position=0.0,0.0,0.0 max_number_of_stations=3 empty_weight=17600 ;ready for service including engine coolant etc station_load.0=1400,0,0,0 ;crew including flying clothing station_load.1=480,0,0,0 ;machine guns, ammo etc, station_load.2=2200,0,0,0 ;default bombload ;*********************************************************************************************** ;max authorised bombload 2000Kg=4400lbs ;max payload=6280lbs ;zero fuel weight with max payload=23,880lb ;MTOW=25,200lbs so fuel with max bombload = 25200 - 23880 = 1320lbs = 220 USG ;default bombload 1000Kg allows 3520lbs fuel=586 USG ;*********************************************************************************************** ;Moments of Inertia empty_weight_roll_MOI=740000 empty_weight_pitch_MOI=450000 empty_weight_yaw_MOI=520000 empty_weight_coupled_MOI=0 [fuel] ; ;Max tankage including oil 726 USG @ 6lbs=4356lbs but normal fuel = 586 USG ; ;Oil tanks included in the fuel tankage as these engines consumed 40+ Kg oil per flight ; LeftMain=0,-22.5,0,293,0 RightMain=0,22.5,0,293,0 fuel_type=1.0 number_of_tank_selectors=1 [GeneralEngineData] engine_type=0 Engine.0=7.250000,-12.916667,1.750000 Engine.1=26.0,0.0,0.0 Engine.2=7.250000,12.916667,1.750000 fuel_flow_scalar=1.065 [piston_engine] ;Maybach Mb.IVa is a throttle gated HC engine rated 245hp at 1400rpm at 8200 feet cylinder_displacement=233.83 ;huge cylinders compression_ratio=4.94 ;high compression does not allow full rpm at sea level number_of_cylinders=6 max_rated_rpm=1400 max_rated_hp=245 fuel_metering_type=1 cooling_type=0 normalized_starter_torque=0.300000 turbocharged=1 ;turbocharger used to mimic throttle gated HC Zeppelin engine power_scalar=1.66 max_design_mp=30.0 min_design_mp=0.0 critical_altitude=8200 emergency_boost_type=0 emergency_boost_mp_offset=0.0 emergency_boost_gain_offset=0.0 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.0 idle_rpm_mechanical_efficiency_scalar=1.0 max_rpm_friction_scalar=1.0 idle_rpm_friction_scalar=1.0 [propeller] gear_reduction_ratio=1.0 ;Props turn at engine speed but with reversed rotation fixed_pitch_beta=25.0 ;actual pitch irrelevant - 1918 prop data placed in 25 degree look up table propeller_type=1 propeller_diameter=9.4 ;set to give correct thrust in FS2002 propeller_blades=2 propeller_moi=5 beta_max=25 beta_min=25 min_gov_rpm=400.0 prop_tc=0.100000 low_speed_theory_limit=80.0 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.0 beta_feather=0.0 power_absorbed_cf=0.0 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.0 minimum_reverse_beta=0.0 [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=0.0 wing_pos_apex_lon=0.0 wing_pos_apex_vert=0.0 htail_area=160.0 htail_span=24.0 htail_pos_lon=-48.0 htail_pos_vert=0.0 htail_incidence=0.0 htail_sweep=0.0 vtail_area=120.0 vtail_span=12.489996 vtail_sweep=0.0 vtail_pos_lon=-48.0 vtail_pos_vert=15.0 elevator_area=71.810000 aileron_area=130.0 rudder_area=100.0 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=0.0 min_ailerons_for_spoilerons=0.0 min_flaps_for_spoilerons=0.0 [keyboard_response] elevator=150.0,250.0 aileron=150.0,250.0 rudder=150.0,250.0 [Views] eyepoint=15,-1,2 [direction_indicators] direction_indicator.0=1,0 [Reference Speeds] flaps_up_stall_speed=40 full_flaps_stall_speed=40 cruise_speed=55 [contact_points] point.0=1.0,23.0,0.0,-9.4,1574.80315,0.0,0.663231,0.0,0.417046,2.5,0.987238,0.0,0.0,0.0,0.0,0.0 point.1=1.0,-1.0,-11.3,-9.6,1574.80315,1.0,0.663231,0.0,0.425471,2.5,0.799629,0.0,0.0,2.0,0.0,0.0 point.2=1.0,-1.0,11.3,-9.6,1574.80315,2.0,0.663231,0.0,0.425471,2.5,0.799629,0.0,0.0,3.0,0.0,0.0 point.3=2.0,-1.67,-69.17,5.917,1574.80315,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,5.0,0.0,0.0 point.4=2.0,-1.67,69.17,5.97,1574.80315,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,6.0,0.0,0.0 point.5=2.0,-48.0,0.0,0.0,2475.91274,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,9.0,0.0,0.0 point.6=2.0,24.5,0.0,-5.0,1574.80315,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,4.0,0.0,0.0 point.0=7,-42.6,0.0,-2.50,1200,0,0.68,10,0.5,2.5,1.0,0.0,0.0,0.0,0.0,0.0 static_pitch=0.192261 static_cg_height=9.711857 [autopilot] autopilot_available=0 flight_director_available=0