//V-22 Osprey, with 'Modified' Engines, to do Mach 1+
//FDE Mods.05Dec29.Copyright @cb....Top Secret! Ha!

[fltsim.0]
title=V-22 Osprey US Marines Mach 1
sim=V22 Mach1
model=
panel=
sound=
texture=
checklists=
kb_checklists=V22_check
kb_reference=
atc_id=
atc_airline=US Marines
atc_flight_number=
ui_manufacturer=Bell Boeing
ui_type="V-22 Osprey"
ui_variation="USMC Mach1"
visual_damage=1 
description=Bell-boeing V-22 Osprey US Marines. 
Autor - Vlad Zhyhulskiy zh@selena.kherson.ua 20.10.02

[General]
performance=Crew :2 + 1 (loadmaster) Soldiers : 24 in 
crashworthy seats, 31 maximum, or 12 litters )
Power plant  : 2 x Allison T406-AD-400
Maximum power per engine : 2 x 4586 kW (6150 shp) 
Transmission ratings :3410 kW (4570 shp) or 4415 kW (5920 shp)
Max. speed: Mach 1.1 or 685 kts  (wink wink) 

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=-1.000000,0.000000,0.000000
max_gross_weight= 17000.000000
empty_weight=            3200.000000
//Useful Load=           13800 lbs
//Fuel=                          7220 lbs (1200 gals)(bal=6580 lbs)
max_number_of_stations =50
station_load.0 =   200.000000,0.000000,0.000000,0.000000 //Pilot
station_load.1 =   180.000000,0.000000,0.000000,0.000000 //Co-Pilot 
station_load.0 =   200.000000,0.000000,0.000000,0.000000 //Tools & Spare Parts 
station_load.2 = 5760.000000,0.000000,0.000000,0.000000 //24 Troops & Gear @ 240 lb each
station_load.0 =   200.000000,0.000000,0.000000,0.000000  //Load Master
//Tot Cargo Load=6540 lbs
;Moments of Inertia  
empty_weight_pitch_MOI=  1695000.000
empty_weight_roll_MOI=     1845000.000
empty_weight_yaw_MOI=   1765000.000
empty_weight_coupled_MOI=12500.000   //o=1100.000


[GeneralEngineData]
engine_type = 1
fuel_flow_scalar = 0.100
engine.0= 8.000000, -4.000000, 0.000000
engine.1= 8.000000,  4.000000, 0.000000
min_throttle_limit=-0.25.000000

[TurbineEngineData]
fuel_flow_gain=0.004500
inlet_area=20.861 
rated_N2_rpm=29920.000 
static_thrust=    20500.000
afterburner_available=1 
reverser_available=1

[jet_engine]
thrust_scalar =1.0

[fuel]
// gal x6.6106= pound(LBS)
Center1=    1.000000,  0.000000, 1.000000, 700.000000, 0.000000
LeftMain=   1.000000, -2.000000, 0.000000, 250.000000, 0.000000
RightMain=1.000000,  2.000000, 0.000000, 250.000000, 0.000000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0

[contact_points] //05Dec29.9pm.cb
point.0= 1.000,   26.000,    0.000,   -7.280, 3003.698, 1.000, 0.521, 60.000, 0.200, 2.0, 1.900, 2.000, 2.000, 0.000, 0.000, 0.000  //p7=42.000,
point.1= 1.000,    -2.900,   -5.850,   -7.150, 3003.698, 1.000, 0.521,   0.000, 0.303, 2.0, 0.820, 4.000, 4.000, 2.000, 0.000, 0.000  //p7=1.000,
point.2= 1.000,    -2.900,    5.850,   -7.150, 3003.698,  2.000, 0.521,  0.000, 0.303, 2.0, 0.820, 4.000, 4.000, 3.000, 0.000, 0.000  //p7=1.000,
point.3= 2.000,     4.000, -32.000, 16.000,        0.000,  0.000, 0.000,   0.000, 0.000, 0.0, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000,     4.000,  32.000, 16.000,        0.000,  0.000, 0.000,   0.000, 0.000, 0.0, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -32.100,    0.000,    0.055,  1802.219,  0.000, 0.000,   0.000, 0.000, 0.0, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000,  28.500,    0.000,   -2.683,    787.405,  0.000, 0.000,   0.000, 0.000, 0.0, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000  //p1=27.500,
point.7= 4.000,   -9.000,   -4.850,   -0.500,  3068.000,  0.000, 0.512, 20.000, 0.800, 2.5, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000
point.8= 4.000,   -9.000,    4.850,   -0.500,  3068.000,  0.000, 0.512, 20.000, 0.800, 2.5, 0.700, 0.000, 0.000, 1.000, 0.000, 0.000
point.9= 4.000,  12.350,   -4.450,   -0.800,  3068.000,  1.000, 0.512,   0.000, 0.800, 2.5, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000
point.10=4.000, 12.350,    4.450,   -0.800,  3068.000,  2.000, 0.512,   0.000, 0.800, 2.5, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000
static_pitch= 0.000
static_cg_height= 6.500   //m1=6.900
gear_system_type=0

[exits]
number_of_exits=2
exit_rate.0=0.2   // ;Percent per second
exit_rate.1=0.5

[keyboard_response]
elevator=125.000000, 900.000000
aileron = 125.000000, 900.000000
rudder = 125.000000, 900.000000

[airplane_geometry]
wing_area = 1001.000000
wing_span = 43.800
wing_root_chord =33.000
wing_dihedral =0.000
wing_incidence = -0.489
wing_twist = -0.99
oswald_efficiency_factor = 0.9
wing_winglets_flag = 0
wing_sweep =13.500
wing_pos_apex_lon = 5.02
wing_pos_apex_vert = 0
htail_area = 400.000000
htail_span = 21.57
htail_pos_lon = -20.82
htail_pos_vert = 0
htail_incidence = 0.000000
htail_sweep =27.000
vtail_area =250.000000
vtail_span =5.8333333
vtail_sweep = 45.000
vtail_pos_lon =-18.500000
vtail_pos_vert = 0.65
elevator_area = 50.005
aileron_area = 100.005
rudder_area =   50.005
elevator_up_limit =15.501974
elevator_down_limit = 20.626481
aileron_up_limit = 15.480565
aileron_down_limit = 15.896903
rudder_limit =36.982000
elevator_trim_limit =14.000000
spoiler_limit =59.950
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0

[flight_tuning]
roll_stability=2.0
roll_stability_scalar=1.0
elevator_trim_effectiveness=1.0
;;critcal_altitude=40000.000

[pitot_static]
vertical_speed_time_constant=60.0    //m1?=100.0

[Reference Speeds]
flaps_up_stall_speed=60.000
full_flaps_stall_speed=5.000 
cruise_speed=665.000 
max_indicated_speed=1000.000000  //o=940.000000
max_mach=1.2

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 1

[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1= 1
Com.1=  1, 1
Com.2=  1, 1
Nav.1=   1, 1, 1
Nav.2=   1, 1, 0
Adf.1=    1
Transponder.1 = 1
Marker.1= 0

[Weather]
TurbulenceScale=0.200000

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -27.14, -10.24,  12.5, fx_navredm ,
light.1=3, -27.14,  10.24, 12.5, fx_navgrem ,
light.2=2, -27.12, -10.28, 12.5, fx_strobeh ,
light.3=2, -27.12,  10.28,12.5, fx_strobeh ,
light.4=2,  -6.85,   0.00, -5.30, fx_beaconb ,

[Views]
eyepoint=0.495386, 0.000000, 12.499815

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=2500.000000
autothrottle_available=1 
autothrottle_arming_required=1
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000 
use_no_default_pitch=1		
use_no_default_bank=1
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000

[direction_indicators]
direction_indicator.0=3,0 

[Flaps.0]
type=1
span-outboard=0.5
extending-time=3
system_type=0
damaging-speed=0
blowout-speed=0
lift_scalar=0.2
drag_scalar=0.7
pitch_scalar=0.1
flaps-position.0=0
flaps-position.1= 5
flaps-position.2=20
flaps-position.3=50

[Flaps.1]
type= 2
span-outboard= 0
extending-time= 0
system_type= 0
damaging-speed= 300
blowout-speed= 300
lift_scalar=0.2
drag_scalar=0.8
pitch_scalar= 0.0
flaps-position.0=   0
flaps-position.1=   5
flaps-position.2=  10
flaps-position.3=  20

[brakes]
toe_brakes_scale=0.70   //o=1.000061
parking_brake=1
differential_braking_scale=1.0  //Delta on amt of brake when rudder is deflected

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000

[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0