// PIASECKI H-21C for MS Flight Sim X
// By Mick Posch
// 6-5-2007
[fltsim.0]
title=Piasecki_H21C_USAF
sim=Piasecki_H21C
model=USAF
panel=
sound=
texture=USAF
atc_id=
atc_id_color=0xffffffff
checklists=
ui_manufacturer="Piasecki"
ui_type="H21-C"
ui_variation=U.S. Air Force
kb_checklists=Piasecki_H21C_check
kb_reference=Piasecki_H21C_ref
ui_typerole="Rotorcraft"
ui_createdby="Mick Posch"
description="The H-21C, also known as the Shawnee, Workhorse, and Flying Banana, was built by the Piasecki Helicopter Corporation beginning in the early Fifties. Several were acquired by the U.S. Air Force in the early Sixties."
-----------------------------------
[fltsim.1]
title=Piasecki_H21C_US_Army
sim=Piasecki_H21C
model=US_Army
panel=
sound=
texture=US_Army
atc_id=
atc_id_color=0xffffffff
checklists=
ui_manufacturer="Piasecki"
ui_type="H21-C"
ui_variation=U.S. Army
kb_checklists=Piasecki_H21C_check
kb_reference=Piasecki_H21C_ref
ui_typerole="Rotorcraft"
ui_createdby="Mick Posch"
description="The H-21C, also known as the Shawnee, Workhorse, and Flying Banana, was built by the Piasecki Helicopter Corporation beginning in the early Fifties. They were used by the U.S. Army in the early part of the Vietnam war."
-----------------------------------
[fltsim.2]
title=Piasecki_H21C_Canadian
sim=Piasecki_H21C
model=Canadian
panel=
sound=
texture=Canadian
atc_id=
atc_id_color=0xffffffff
checklists=
ui_manufacturer="Piasecki"
ui_type="H21-C"
ui_variation=Royal Canadian Air Force
kb_checklists=Piasecki_H21C_check
kb_reference=Piasecki_H21C_ref
ui_typerole="Rotorcraft"
ui_createdby="Mick Posch"
description="The H-21C, also known as the Shawnee, Workhorse, and Flying Banana, was built by the Piasecki Helicopter Corporation beginning in the early Fifties. They were used by the Royal Canadian Air Force in support roles."
-----------------------------------
[fltsim.3]
title=Piasecki_H21C_German
sim=Piasecki_H21C
model=German
panel=
sound=
texture=German
atc_id=
atc_id_color=0xffffffff
checklists=
ui_manufacturer="Piasecki"
ui_type="H21-C"
ui_variation=West German Army
kb_checklists=Piasecki_H21C_check
kb_reference=Piasecki_H21C_ref
ui_typerole="Rotorcraft"
ui_createdby="Mick Posch"
description="The H-21C, also known as the Shawnee, Workhorse, and Flying Banana, was built by the Piasecki Helicopter Corporation beginning in the early Fifties. This German Army version was equipped with rear view mirrors and landing gear covers."
-----------------------------------
[fltsim.4]
title=Piasecki_H21C_Civilian_1
sim=Piasecki_H21C
model=H21C_Civilian_1
panel=
sound=
texture=H21C_Civilian_1
atc_id=
atc_id_color=0xffffffff
checklists=
ui_manufacturer="Piasecki"
ui_type="H21-C"
ui_variation=Civilian - Purple
kb_checklists=Piasecki_H21C_check
kb_reference=Piasecki_H21C_ref
ui_typerole="Rotorcraft"
ui_createdby="Mick Posch"
description="The H-21C, also known as the Shawnee, Workhorse, and Flying Banana, was built by the Piasecki Helicopter Corporation beginning in the early Fifties. This configuration is a fictional civilian model. It lacks the cargo sling and rescue hook, and is equipped with more passenger-friendly seats than the military variations.
-----------------------------------
[fltsim.5]
title=Vertol_V-44_NYAirways
sim=Piasecki_H21C
model=V-44_NYAirways
panel=
sound=
texture=V-44_NYAirways
atc_id=
atc_id_color=0xffffffff
checklists=
ui_manufacturer="Vertol"
ui_type="V-44"
ui_variation=New York Airways
kb_checklists=Piasecki_H21C_check
kb_reference=Piasecki_H21C_ref
ui_typerole="Rotorcraft"
ui_createdby="Mick Posch"
description="The V-44 was built by the Vertol Aircraft Corporation (formerly the Piasecki Helicopter Corporation) in the late Fifties and early Sixties. The design was relatively unchanged from the H-21C, except for the floats that many were equipped with. They were used by New York Airways, serving destinations in New York, New Jersey, and Connecticut."
-----------------------------------
[fltsim.6]
title=Vertol_V-44_Civilian_1
sim=Piasecki_H21C
model=V-44_Civilian_1
panel=
sound=
texture=V-44_Civilian_1
atc_id=
atc_id_color=0xffffffff
checklists=
ui_manufacturer="Vertol"
ui_type="V-44"
ui_variation=Civilian - Purple & Green
kb_checklists=Piasecki_H21C_check
kb_reference=Piasecki_H21C_ref
ui_typerole="Rotorcraft"
ui_createdby="Mick Posch"
description="The V-44 was built by the Vertol Aircraft Corporation (formerly the Piasecki Helicopter Corporation) in the late Fifties and early Sixties. The design was relatively unchanged from the H-21C, except for the floats that many were equipped with. They probably never built any in this paint job, but hey, they should have. You'll never make a quiet entrance at a beach party when you show up in this sucker.
=======================================================
[General]
atc_type=Piasecki
atc_model=H-21C
performance="Maximum Speed\n143 kts 265 km/hr\n\nCruise Speed\n87 kts 161 km/hr\n\nEngine\n1425 HP Wright R-1820-103 Cyclone (Piston; Radial)\n\nMaximum Range\n450 nm 833 km\n\nService Ceiling\n10,000 ft 3,048 m\n\nFuel Capacity\n300 gal 1,135 L\n\nEmpty Weight\n8007 lb 3,640 kg\n\nMax Gross Weight\n15,013 lb 6,824 kg\n\nLength\n86 ft 26.2 m\n\nRotor Span\n44.25 ft 13.5 m\n\nHeight\n15.5 ft 4.7 m\n\nSeating\n19 + 2 Pilots"
editable=0
Category = Helicopter
=======================================================
[CameraDefinition.001]
Title = "Overhead Panel"
Guid = {E9DE1A19-008E-4080-81C3-2991002ED5C2}
Origin = Virtual Cockpit
MomentumEffect = No
ShowPanel = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .55
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.29, .31, -.18
InitialPbh=-30, -16, -26
cyclehidden=No
HotKeySelect=5
[CameraDefinition.002]
Title = "Center Console"
Guid = {EBB6EA57-440F-46d8-999B-2523B4683F3A}
Origin = Virtual Cockpit
MomentumEffect = No
ShowPanel = No
SnapPbhAdjust = none
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .9
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.22, -.01, -0.28
InitialPbh=45, 0, -30
HotKeySelect=6
[CameraDefinition.003]
Title = "Start up"
Guid = {6A7CCB29-E991-4c5f-B68D-23F6922DB5A5}
Origin = Virtual Cockpit
MomentumEffect = No
ShowPanel = No
SnapPbhAdjust = none
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.01, -0.23, -0.18
InitialPbh=20, 0, -45
[CameraDefinition.004]
Title = "Floor - Right"
Guid = {EE2696EA-0683-41a0-858B-2DD9AA26661A}
Origin = Virtual Cockpit
MomentumEffect = No
ShowPanel = No
SnapPbhAdjust = none
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .8
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.31, -.08, 0.17
InitialPbh=90, 40, 90
HotKeySelect=8
[CameraDefinition.005]
Title = "Floor - Left"
Guid = {9CCF3000-2D10-4001-BC29-FE09C36AA978}
Origin = Virtual Cockpit
MomentumEffect = No
ShowPanel = No
SnapPbhAdjust = none
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .9
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-.26, -.01, 0.02
InitialPbh=70, 0, -160
HotKeySelect=9
[CameraDefinition.006]
Title = "Engine Gauges"
Guid = {7A983BA6-E095-4f5b-AF57-54CC4B95BB7E}
Origin = Virtual Cockpit
MomentumEffect = No
ShowPanel = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz= -0.68, -0.01, -0.48
InitialPbh=10, 0, 0
HotKeySelect=4
[CameraDefinition.007]
Title = "Pilot's View"
Guid = {6B238EB8-8E52-4425-A72D-DBA3EC3154BC}
Origin = Virtual Cockpit
MomentumEffect = No
ShowPanel = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = FALSE
InitialZoom = 0.3
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=TRUE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
CycleHidden=Yes
InitialXyz= 0, 0, 0
InitialPbh=0, 0, 0
HotKeySelect=7
[WEIGHT_AND_BALANCE]
max_gross_weight = 15013 // (pounds)
empty_weight = 8007 // (pounds)
reference_datum_position = 8.33, 0.0, 0.0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -8.70, 0.0, 0.0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 160, -6.6, 0.89, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 160, -6.6, -0.78, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.0 = "Pilot"
station_name.1 = "Passenger"
;Moments of Inertia
empty_weight_pitch_MOI = 60000
//empty_weight_roll_MOI = 50000
empty_weight_roll_MOI = 80000
empty_weight_yaw_MOI = 100000
empty_weight_coupled_MOI = 0
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor = 0, 5 , 17.0
gear_motor = 0, 5 , 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2 , 17.0
marker_beacon = 1, 2 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_taxi = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
=======================================================
[CONTACT_POINTS]
//0 Class <0=none,1=wheel, 2=scrape, 3=skid>
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
================================================================================================================================
//Wheel contact points
StComp MSCratio Dratio
point.0= 1, 12.5, -3.500, -4.700, 3000.000, 0.000, 0.984, 38.000, 1.100, 1.300, 0.3300, 0.000, 0.000, 0.000, 0.000, 0.000 //LF
point.1= 1, 12.5, 3.500, -4.700, 3000.000, 0.000, 0.984, 38.000, 1.100, 1.300, 0.3300, 0.000, 0.000, 0.000, 0.000, 0.000 //RF
point.2= 1, -14.67, -6.500, -4.700, 3000.000, 1.000, 1.148, 0.000, 1.100, 1.300, 0.3300, 0.000, 0.000, 2.000, 0.000, 0.000 //LR
point.3= 1, -14.67, 6.500, -4.700, 3000.000, 2.000, 1.148, 0.000, 1.100, 1.300, 0.3300, 0.000, 0.000, 3.000, 0.000, 0.000 //RR
//Rotor contact points
point.4= 2, 30, 19, 11, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.5= 2, -45, 24, 12, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.6= 2, -45, -24, 12, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.7= 2, 30, -19, 11, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
//Tail contact point
point.8= 2, -36.3, 0, 4.5, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
=============================================================================================================================
//Float contact points:
point.9= 4, -9.800, -6.000, -2.800, 3000, 0.0, 0.00, 0.0, 0.85, 2.50, 0.60, 0.0, 0.0, 0.0, 0.0, 0.0 //LR
point.10= 4, -9.800, 6.000, -2.800, 3000, 0.0, 0.00, 0.0, 0.85, 2.50, 0.60, 0.0, 0.0, 0.0, 0.0, 0.0 //RR
point.11= 4, 16.000, -3.000, -1.000, 3000, 0.0, 0.00, 0.0, 0.85, 2.50, 0.60, 0.0, 0.0, 0.0, 0.0, 0.0 //LF
point.12= 4, 16.000, 3.000, -1.000, 3000, 0.0, 0.00, 0.0, 0.85, 2.50, 0.60, 0.0, 0.0, 0.0, 0.0, 0.0 //RF
================================================================================================================================
static_pitch= 0
static_cg_height= 3.500
=======================================================
gear_system_type=0
[brakes]
toe_brakes_scale=1.000031
parking_brake=1
=======================================================
[hydraulic_system]
normal_pressure = 0.0 //PSI
======================================================
[Views]
eyepoint= 12.9, 1.49, 6.15
//For virtual cockpit. The numbers are: (feet) longitudinal, lateral, vertical distance from reference datum.
=======================================================
[LIGHTS]
//Dome Light
light.6 = 4, 13.5, -0.8, 7.7, fx_vclighth,
//Dome light spilling ito cabin
light.7 = 4, 7, 0, 6, fx_vclighth,
[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 = 1
=====================================================
[exits]
number_of_exits=2
exit_rate.0=1 // lower values = slower
exit_rate.1=1
=======================================================
[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.
//NOTE: These map to cyclic (fore/aft), cyclic (left/right), and anti-torque
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[vacuum_system]
max_pressure=5.15 //PSI
vacuum_type=1 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
electric_backup_pressure=5.15 //PSI
engine_map=1
[pneumatic_system]
max_pressure=0.000000
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 0.0 //Scalar on heat effectiveness, 0 = not available
================================================================================
[EFFECTS]
wake=fx_wake
water=fx_H21C_spray
dirt=fx_H21C_tchdrt
startup=fx_H21C_engstrt
================================================================================
[fuel]
//Center1 = -8.85, -0.5, 0.0, 19.2, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1 = -8.85, 0.0, 0.0, 19.2, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//RightMain = -8.85, 0.5, 0.0, 10.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet),
Usable(gallons), Unusable (gallons)
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
engine_driven_pump=0
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -8.5, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.8 //Fuel flow scalar
min_throttle_limit = 0.0; //Minimum percent throttle. Generally negative for turbine reverser
[piston_engine]
power_scalar = 1 //Piston power scalar
cylinder_displacement= 90.0 //Cubic inches per cylinder
compression_ratio= 8.5 //Compression ratio
number_of_cylinders=4 //Number of cylinders
max_rated_rpm= 2700 //Max rated RPM
max_rated_hp= 180 //Max rated HP
fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3 //Starter torque factor
turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0 //Max design manifold pressure, (inHg)
min_design_mp= 0 //Min design manifold pressure, (inHg)
critical_altitude= 0 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 0.94 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 0.7 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction
magneto_order_left_right_both = 1 //sets the order of the magneto switch direction
[Reference Speeds]
cruise_speed = 90.0 //Knots True (KTAS)
max_indicated_speed = 125 //Red line (KIAS)
[autopilot]
autopilot_available= 0
flight_director_available= 0
[yaw_string]
yaw_string_available=1
[Helicopter]
reference_length = 21.58
reference_frontal_area = 17.7
reference_side_area = 44.5
side_aero_center = -12.5
right_trim_scalar = 0.65
correlator_available = 1
governed_pct_rpm_ref = 1.04
//governor_pid = 0.4, 0, 0.1, 0, 0.2 //R-22 default (power fluctuates when clutch = on, stable when clutch = off)
governor_pid = 0.1, 85, 0.1, 0, 0.2
rotor_brake_scalar = 100
torque_scalar = .01
cyclic_roll_control_scalar =8.0
cyclic_pitch_control_scalar =1.0
pedal_control_scalar =1.0
collective_on_rotor_torque_scalar = 1.0
[fuselage_aerodynamics]
drag_force_cf = 1.7
side_drag_force_cf = 10.0
pitch_damp_cf = -2.0
roll_damp_cf = -6.0
yaw_damp_cf = -0.1
yaw_stability_cf = 0.27
[MainRotor]
Position = -8.5, 0.2, 4.91 //Longitudinal, Lateral, Vertical feet from datum
Radius = 12.583 //feet
max_disc_angle = 5.0
RatedRpm = 510
Number_of_blades = 2
Weight_per_blade = 26.0
Weight_to_moi_factor = 0.58
//Affects rotor thrust - very sensitive:
inflow_vel_reference = 72.0
[SecondaryRotor]
Position = -22.8, -12.74, 1.8 //Longitudinal, Lateral, Vertical feet from datum
TailRotor = 1
Radius = 1.75 //feet
[deice_system]
structural_deice_type=0 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots
