[fltsim.0]
title=De Havilland 60 G
sim=De Havilland 60 G
model=
panel=
sound=
texture=G-AAHI
kb_checklists=DH60_Checklist
kb_reference=The DH 60 Moth
ui_manufacturer = De Havilland Aircraft Co LTD
atc_id = G-AAHI
ui_type = DH60 G Gipsy Moth
ui_variation =
description=First flown in the June, 1928, the DH60G Moth was a wooden DH60X airframe mated to De Havilland's new Gipsy engine.  The last production example of this aircraft was delivered in late summer of 1933, although it is reported that a few later aircraft may have been produced on special order after that time.  Approximately 690 examples were built. 


[General]
atc_type=De Havilland
atc_model=Moth
editable=0
performance=Maximum Speed\n102 mph\n\nCruise Speed\n75 - 85 mph\nEngine\n90 hp De Havilland Gipsy\n\nMaximum Range\n320 mi\n\nService Ceiling\n16,000 ft\n\nFuel Capacity\n23 gal\n\nEmpty Weight\n920lb\n\nMaximum Gross Weight\n1650 lb\n\nLength\n23 ft,11 in\n\nWingspan\n30 ft\n\nHeight\n8 ft, 9.5 in\n\nSeating\n2\n\nUseful Load\n588lb
Category=airplane


[forcefeedback]
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1
crash_magnitude1=10000
crash_direction1=1000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000
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=500
gear_bump_right_duration=250000
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111


[WEIGHT_AND_BALANCE]
empty_weight =920
reference_datum_position   =    0, 0, 0    // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     = -0.5, 0.000, 0.000

max_number_of_stations =3

;Moments of Inertia
empty_weight_pitch_MOI   =2233.00000
empty_weight_roll_MOI    =1337.00000
empty_weight_yaw_MOI     =2781.00000
empty_weight_coupled_MOI =0.00000
max_gross_weight =1650

station_load.0	=   0, -0.80,  0.0, -0.66, Passenger // Weight lbs), 
station_load.1	= 170, -3.50,  0.0, -0.66, Pilot
station_load.2  =  30, -4.50,  0.0,  0.00, baggage

[flight_tuning]
cruise_lift_scalar     =1.0
parasite_drag_scalar   =1.0
induced_drag_scalar    =1.0
elevator_effectiveness =1.0
aileron_effectiveness  =1.0
rudder_effectiveness   =1.25
pitch_stability        =1.0
roll_stability         =1.0
yaw_stability          =1.0
elevator_trim_effectiveness =1.00
aileron_trim_effectiveness  =1.0
rudder_trim_effectiveness   =1.0
p_factor_on_yaw=1.0
torque_on_roll=1.0
gyro_precession_on_roll=1.0
gyro_precession_on_yaw=1.0


[GeneralEngineData]
engine_type=0
Engine.0=5.74, 0.000, -0.85
Fuel_flow_scalar=1.0
min_throttle_limit=0.0
starter_type = 1

[piston_engine]
power_scalar =1.0
cylinder_displacement=77.5
compression_ratio=6.4
number_of_cylinders=4
number_of_magnetos = 2                   
max_rated_rpm=2100
max_rated_hp=100
fuel_metering_type=1
cooling_type=1
normalized_starter_torque=0.30
turbocharged=0
max_design_mp=29.92
min_design_mp=0.0
critical_altitude=0.0
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=1.1


[propeller]
thrust_scalar =1.1                  
propeller_type=1                              
propeller_diameter=6.81                  
propeller_blades=2                           
propeller_moi= 3.0                     
beta_max=20.00000                                 
beta_min=18.00000                               
min_gov_rpm=0.00000                            
prop_tc=0.00450                                
gear_reduction_ratio=1.0            
fixed_pitch_beta=19.2                     
low_speed_theory_limit=60            
prop_sync_available=0                       
prop_deice_available=0                       
prop_feathering_available=0                 
prop_auto_feathering_available=0 
min_rpm_for_feather=0.00000                   
beta_feather=0.00000                             
power_absorbed_cf=0.00000                         
defeathering_accumulators_available=0        
prop_reverse_available=0                    
minimum_on_ground_beta=0.00000                   
minimum_reverse_beta=0.00000 
rotation=-1


[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 14.0
max_generator_alternator_amps = 40.0

[exits]
number_of_exits = 2
exit_rate.0 = 0.8                               ;Percent per second
exit_rate.1 = 0.8


[contact_points]  
        //0  Class
        //1  Longitudinal Position       (feet)
        //2  Lateral Position            (feet)
        //3  Vertical Position           (feet)
        //4  Impact Damage Threshold     (Feet Per Minute)
        //5  Brake Map                   (0=None, 1=Left, 2=Right)
        //6  Wheel Radius                (feet)
        //7  Steer Angle                 (degrees)
        //8  Static Compression          (feet)  (0 if rigid)
        //9  Max/Static Compression Ratio
        //10 Damping Ratio               (0=Undamped, 1=Critically Damped)
        //11 Extension Time              (seconds)
        //12 Retraction Time             (seconds)
        //13 Sound Type

max_number_of_points=7
gear_system_type=0
tailwheel_lock=0
point.0=3, -15.53,   0.0,  -2.14,  1600.0, 0, 0.083, 60.0, 0.0815,  2.0,  0.5, 0.0, 0.0, 7.0, 0.0, 0.0
point.1=1,   0.71,  -2.66, -5.46,  1600.0, 1, 0.858,  0.0, 0.1440,  1.5,  0.7, 0.0, 0.0, 2.0, 0.0, 0.0
point.2=1,   0.71,   2.66, -5.46,  1600.0, 2, 0.858,  0.0, 0.1440,  1.5,  0.7, 0.0, 0.0, 3.0, 0.0, 0.0
point.3=2,   0.00, -20.5,   2.00,   800.0, 0, 0.000,  0.0, 0.0000,  0.0,  0.0, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2,   0.00,  20.5,   2.00,   800.0, 0, 0.000,  0.0, 0.0000,  0.0,  0.0, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2, -15.55,   0.0,  -1.65,  1800.0, 0, 0.000,  0.0, 0.0000,  0.0,  0.0, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2,   6.00,   0.0,  -5.00,   800.0, 0, 0.000,  0.0, 0.0000,  0.0,  0.0, 0.0, 0.0, 4.0, 0.0, 0.0

static_pitch = 11.19
static_cg_height = 5.073

[Views]
eyepoint = -3.7, 0.0, 0.950 //(feet) longitudinal, lateral, vertical distance from reference datum

[Flaps.0]
type= 2
span-outboard= 0.125
extending-time= 0.500
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 90.000, 0.000


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4,  -3.70,    0.00,   1.80,   fx_vclight,
light.1 = 2,  -8.02,   -1.026, -0.149,  fx_Moth_exhaust


[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_DH60_start
touchdown=fx_tchdwn_s, 1

[SMOKESYSTEM]

[FUEL]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1= 0.0, 0.0, 2.65 22.8, 0.000
fuel_type=1
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area               =243           
wing_span               =30            
wing_root_chord         =4.35            
wing_dihedral           =1.5                
wing_incidence          =0.0            
wing_twist              =0.0                
oswald_efficiency_factor=0.75              
wing_winglets_flag      =0                     
wing_sweep              =0.0            
wing_pos_apex_lon       =0.0                 
wing_pos_apex_vert      =2.6               
htail_area              =11.25               
htail_span              =8.90        
htail_pos_lon           =-13.6            
htail_pos_vert          =0.0            
vtail_area              =5.10              
vtail_span              =5.0                 
vtail_sweep             =0.0              
vtail_pos_vert          =0.45                
elevator_area           =15.88
aileron_area            =19.8                  
rudder_area             =11.5                 
elevator_up_limit       =25.0                 
elevator_down_limit     =25.0                 
aileron_up_limit        =20                
aileron_down_limit      =10             
rudder_limit            =28.0                  
elevator_trim_limit     =15.0                 
spoiler_limit           =1.0                 
spoilerons_available    =0                     
aileron_to_spoileron_gain =0.0                
min_ailerons_for_spoilerons =0.0               
min_flaps_for_spoilerons =0.0                   
htail_incidence=0.00000
htail_sweep=0.00000
vtail_pos_lon=-13.90
spoiler_handle_available=0
auto_spoiler_available=0
load_safety_factor=1.50

[brakes]
parking_brake = 0       //Parking brake not available
toe_brakes_scale =0.0
differential_braking_scale = 1.0        

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.00000
flap_limit_power=0.00000
flap_limit_idle=0.00000
//gear down and welded

[Reference Speeds]
flaps_up_stall_speed=35
full_flaps_stall_speed=35
cruise_speed=74
max_indicated_speed=135

[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to  1/2 and 1/8 respectively.
elevator =200, 1000
aileron  =200, 1000
rudder   =200, 1000


[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.00000
autothrottle_available=0
pitch_takeoff_ga=8.00000
max_pitch=10.00000
max_pitch_acceleration=1.00000
max_pitch_velocity_lo_alt=2.00000
max_pitch_velocity_hi_alt=1.50000
max_pitch_velocity_lo_alt_breakpoint=20000.00000
max_pitch_velocity_hi_alt_breakpoint=28000.00000
max_bank=25.00000
max_bank_acceleration=1.80000
max_bank_velocity=3.00000
max_throttle_rate=0.10000
nav_proportional_control=9.00000
nav_integrator_control=0.25000
nav_derivative_control=0.00000
nav_integrator_boundary=2.50000
nav_derivative_boundary=0.00000
gs_proportional_control=9.52000
gs_integrator_control=0.26000
gs_derivative_control=0.00000
gs_integrator_boundary=0.70000
gs_derivative_boundary=0.00000
yaw_damper_gain=0.00000
autothrottle_arming_required=0
default_pitch_mode=0
default_bank_mode=0
use_no_default_bank=1
use_no_default_pitch=1
autothrottle_takeoff_ga=1.00000
autothrottle_max_rpm=90.00000


[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1       = 0
Com.1         = 1, 0
Nav.1         = 0, 0, 0
Adf.1         = 0
Transponder.1 = 0
Marker.1      = 0

[stall_warning]
type=0
stick_shaker=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=2,0

[direction_indicators]
direction_indicator.0=1,0

[hydraulic_system]
normal_pressure=0.00000

[pitot_static]
pitot_heat=1.000000

[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,0,0,0

[pneumatic_system]
max_pressure=0.0
bleed_air_scalar=0.00

[deice_system]
structural_deice_type=0


