//*******************************************************************
Zeppelin R.VI (Schütte-Lanz)with Mercedes D.IVa engines (1918)
//*******************************************************************

// Do not attempt to edit this file with FSedit! - use notepad or wordpad


[fltsim.0]
title=Zeppelin R.VI
sim=Zep-R6
model=
panel=
sound=
texture=
description=Zeppelin Staaken R.VI R27 - 1917 Riesenflugzeug, license built by Schütte Lanz, with 4 x 267 Hp Mercedes D.IVa high compression engines, altitude rated at 1450 RPM at 1300 meters, capable of payloads of upto 2 tonnes.
ui_manufacturer=Zeppelin Werke
ui_type=R-VI R27 (Schütte-Lanz)
ui_variation=1918 5-colour splinter lozenge
atc_heavy=0
checklists=
kb_checklists=
kb_reference=R6_ref

description=

[General]
performance=Length: 72 ft 6 in\nWing span: 138 ft 5 in\nWeight: 25,200 lbs\nPower: 4 x 267 Hp Mercedes D.IVa 6-cyl

[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=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		;6 machine guns and ammo
station_load.2=2200,0,0,0		;normal 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

;normal 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=0,0,0,293,0		 	
RightMain=0,0,0,293,0 		
;
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		;Mercedes D.IVa has direct drive
fixed_pitch_beta=25.000000		;actual pitch irrelevant - realistic 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

[autopilot]			;for beta testing
autopilot_available=0		;set 0 prior to release
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

[Reference Speeds]
flaps_up_stall_speed=40
full_flaps_stall_speed=40
cruise_speed=55


[contact_points]
point.0=1,-42.43,0.0,-2.80,1200,0,0.68,10,0.5,2.5,1.0,0.000000,0.000000,0.000000,0.000000,0.000000
point.1=1,3.29,-18.33,-10.0,1500,1,0.68,0 ,0.6,2.5,0.9,0.000000,0.000000,2.000000,0.000000,0.000000
point.2=1,3.29,18.33,-10.0,1500,2,0.68,0 ,0.6,2.5,0.9,0.000000,0.000000,3.000000,0.000000,0.000000
point.3=1,22.650,0.0,-7.75,1200,0,0.68,0 ,0.6,2.5,0.9,0.000000,0.000000,0.000000,0.000000,0.000000
point.4=2,-.05,-70.00,5.916667,1574,0.00,0.00,0.00,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.5=2,-1.66,69.16,5.916667,1574,0.00,0.00,0.00,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.6=2,24.5,0.00000,-3.0000,1574,0.00,0.00,0.00,0.00,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
point.7=2,-42.6,0.0,-0.0000,1800,0,0,0,0,0,0,0.000000,0.000000,0.000000,0.000000,0.000000

static_pitch=9.65
static_cg_height=9.25