//**********************************************
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