//************************************************************
AEG G-IV 'realistic' flight dynamics for daylight operations
//************************************************************

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


[fltsim.0]
title=AEG G.IV Night Bomber 1917
sim=AEG_G4N
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=AEG_G4N_ref
kb_notes=G-IV_notes
description=German 1917 short-range tactical night bomber, in blue lozenge colour scheme.
atc_airline=
atc_flight_number=
ui_manufacturer=AEG Berlin
ui_type=G.IV
ui_variation=Night bomber
atc_heavy=0
atc_id=


[General]
performance=Two 260 hp 6-cyl Mercedes D.IVa\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=4
empty_weight=5291				

station_load.0=330,5,0,0 		;pilot and gunner including flying clothing
station_load.1=120,-1,0,0		;guns and ammo - reduce to 60 for night bombing
station_load.2=140,1,0,0		;water in radiators
station_load.3=165,-10,0,0 		;gunner - remove for night bombing



;**********************************************************************************************************

;max authorised payload 880lbs

;zero fuel weight with max payload=5291+495+880+120+140=7020
;MTOW=8000 so fuel with max bombload = 8079 - 7020 = 1153lbs
;German aviation fuel from 6/1917 about 60 Octane (at best) and had density about 6lbs per US gallon (set in air file)
;Fuel volume with max bomb load=1153/6 = 192 USG

;Lower the spoiler before take off to add the external bomb drag
;raise the spoiler if flying without external bombs

;***********************************************************************************************************

;Moments of Inertia
empty_weight_roll_MOI=74000
empty_weight_pitch_MOI=28000
empty_weight_yaw_MOI=58000
empty_weight_coupled_MOI=0

[fuel]
;aux fuel will be fully specified and selectable in a later revision
;IMPORTANT - Two of the fuel tanks contain bombs not fuel - observe handling notes - see 'how to drop bombs in FS2002'
;
;Max tankage originally 192 USG with 8 USG assumed unusable
;84 USG auxiliary tank added to some before first London raid and all before second London raid and MTOW then increased to 8550lbs
;
;Oil tanks included in the fuel tankage as these engines consumed 20+ Kg oil per flight
;
Center1=3,0,0,90,0			;MAIN fuel and oil in this tank
center2=0,0,0,92,0			;auxiliary tank 
LeftMain=0,0,0,73,0		 	;this is the internal load - open the fuel menu to drop these bombs (one by one = 5 USG each)
RightMain=1,0,0,73,0 			;this is the normal external load ( 4 x 50Kg) - open the fuel menu to drop these bombs (one by one = 19 USG each)
;
fuel_type=1.000000
number_of_tank_selectors=1


[GeneralEngineData]
engine_type=0
Engine.0=6,-9.0,0
Engine.1=6,9.00,0
fuel_flow_scalar=1.065				;including oil consumption	

[piston_engine]
;Mercedes D.IVa is a 260hp minimum Class IVa throttle gated HC engine rated 267hp at 1450rpm at 1300 metres

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 1916 prop data placed in 25 degree look up table
propeller_type=1
propeller_diameter=9.15		;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=0.75		;The wing is inefficient
wing_area=721.0				;but very large
wing_span=60.8
wing_root_chord=12.916667
wing_dihedral=2.9			
wing_incidence=6.0			;huge angle of incidence - Gotha flies nose down at Vmax but has reasonable view on approach
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=45
htail_span=13.5
htail_pos_lon=-29.166667
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=98.000000
vtail_span=5
vtail_sweep=0.000000
vtail_pos_lon=-30.000000
vtail_pos_vert=9.666667
elevator_area=19.2
aileron_area=32
rudder_area=16
elevator_up_limit=27.5			;control deflections estimated
elevator_down_limit=20.5
aileron_up_limit=17.0
aileron_down_limit=12.5
rudder_limit=15.0
elevator_trim_limit=20			;for use with AP during testing
spoiler_limit=60				;use to simulate drag of external bombs 
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=-0.4,-0.7,1.75

[autopilot]					;for beta testing set to 1,
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=30.000000
full_flaps_stall_speed=30.000000
cruise_speed=84

[contact_points]

point.0=1,-21.0,0,-3.8,1000,0,0.548,10,0.500,2.5,1.23,0.000000,0.000000,0.000000,0.000000,0.000000
point.1=1,0.5,-7.0,-7.27,1200,1,0.548,0 ,0.616,2.5,0.60,0.000000,0.000000,2.000000,0.000000,0.000000
point.2=1,0.5,7.0,-7.27 ,1200,2,0.548,0 ,0.616,2.5,0.60,0.000000,0.000000,3.000000,0.000000,0.000000

point.3=2.000000,-1.666667,-37.416667,-0.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-1.666667,37.416667,-0.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2,-21.0,0,0,1600,0,0,0,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,9.166667,0.000000,-0.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=10
static_cg_height=7.38

[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000