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lynxmk9.xml
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lynxmk9.xml
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<!-- Country of Origin UK
Builder WESTLAND
Role Utility, attack, antitank
Rotor diameter 42 ft (12.8 m)
Dimensions (External)
Overall Length Rotors Turning 15. 16 m
Fuselage Length 13. 33 m
Width (excluding rotor) 2. 94 m
Overall Height 3. 48 m
Folded Length 10. 85 m
Folded Width 2. 94 m
Folded Height 3. 25 m
Main Rotor Diameter 12. 80 m
Tail Rotor Diameter 2. 36 m
Dimensions (Internal)
Cabin Length 2. 05 m
Cabin Width 1. 78 m
Cabin Height 1. 42 m
Accommodation
Cockpit Pilot and Co-Pilot or Observer
Cabin Up to 9 passengers
Rotor System
Main Rotor Type Semi-rigid
Main Rotor Blades 4 composite blades
Tail Rotor Type Fully articulated
Tail Rotor Blades 4 composite blades
Weights
Empty weight 3150 kg
Maximum All Up Mass 5330 kg
Cargo Hook Capacity 1360 kg
Standard Fuel 786 kg
Auxiliary Fuel Tank 353 kg each
Engines
Number 2 2
Make Rolls Royce LHTEC
Model Gem 42-1 CTS800-4N
Take-Off Rating 746 kW each 1015 kW each
Maximum Continuous 664 kW each 945 kW each
Performance
Cruise Speed 137 knots
Maximum Range (with auxiliary fuel) 530 nm
Endurance (with auxiliary fuel) 5. 4 hours
Armament Cannon, minigun, rockets, missiles, HOT or TOW antitank missiles
Blade airfoil NPL 9618 or NPL 9615, the model here is without BERP blade
-->
<!--
<airplane mass="7755">
-->
<airplane mass="7755" version="YASIM_VERSION_CURRENT">
<approach speed="47" aoa="16">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.3"/>
</approach>
<cruise speed="160" alt="0">
<control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
</cruise>
<rotor name="main" x="0.0" y="0" z="1.47" nx="0" ny="0" nz="1.0" fx="1" fy="0" fz="0" ccw="1"
maxcollective="18" mincollective="-4"
mincyclicele="-24.5" maxcyclicele="17"
mincyclicail="-15" maxcyclicail="18"
diameter="12.8" numblades="4" weightperblade="87" relbladecenter="0.62"
dynamic="0.85" rpm="305" rellenflaphinge="0.22" delta3="0.07"
delta=".28"
pitch-a="10"
pitch-b="15"
flapmin="-15"
flapmax="15"
flap0="-5"
phi0="0"
flap0factor="0"
notorque="0"
dragfactor="0.25"
translift-ve="20"
translift-maxfactor="1.2"
ground-effect-constant="0.1"
twist="-8"
taper="1"
chord="0.39"
number-of-segments="8"
number-of-parts="8"
rel-len-where-incidence-is-measured="0.7"
rel-len-blade-start="0.25"
tiltcenterx="0"
tiltcentery="0"
tiltcenterz="1.47"
mintiltyaw="0"
mintiltpitch="-5"
mintiltroll="0"
maxtiltyaw="0"
maxtiltpitch="0"
maxtiltroll="0"
airfoil-lift-coefficient="5.1"
airfoil-drag-coefficient0="0.015"
airfoil-drag-coefficient1="0.25"
incidence-stall-zero-speed="15"
incidence-stall-half-sonic-speed="14.5"
lift-factor-stall="0.28"
stall-change-over="5.5"
drag-factor-stall="2.0"
cyclic-factor="0.85"
rotor-correction-factor="0.9"
downwashfactor="0.4"
>
<control-input axis="/controls/flight/aileron-trim" control="CYCLICAIL"/>
<control-input axis="/controls/flight/aileron" control="CYCLICAIL"
src0="-1.0" src1="1.0"
dst0="-1.0" dst1="1.0"/>
<control-input axis="/controls/flight/elevator-trim" control="CYCLICELE"/>
<control-input axis="/controls/flight/elevator" control="CYCLICELE"
src0="-1.0" src1="1.0"
dst0="-1.0" dst1="1.0"/>
<control-input axis="/controls/engines/engine[0]/throttle" control="COLLECTIVE"
src0="0.0" src1="1.0"
dst0="1.0" dst1="-1.0"/>
</rotor>
<rotor name="tail" x="-7.64" y="0.38" z="1.37" nx="0.0" ny="-1" nz="0.0" fx="1" fy="0" fz="0" ccw="1"
maxcollective="17.7" mincollective="-12"
phi0="110"
diameter="2.36" numblades="4" weightperblade="2.5" relbladecenter="0.7"
dynamic="1" rpm="1780" rellenflaphinge="0.0" delta3="1" translift="0" delta="0.5"
sharedflaphinge="1"
flap0="-0.5"
pitch-a="10"
pitch-b="15"
airfoil-lift-coefficient="6.4"
airfoil-drag-coefficient0="0.0035"
airfoil-drag-coefficient1="0.10"
notorque="0"
taper="1"
chord="0.25"
number-of-segments="5"
number-of-parts="4"
rel-len-blade-start="0.33"
incidence-stall-zero-speed="9"
incidence-stall-half-sonic-speed="18"
lift-factor-stall="0.18"
stall-change-over="5.5"
drag-factor-stall="8"
rotor-correction-factor="0.9"
>
<control-input axis="/controls/flight/rudder-trim" control="COLLECTIVE" invert="true"/>
<control-input axis="/controls/flight/rudder" control="COLLECTIVE" invert="true"
src0="-1.0" src1="1.0"
dst0="-1.0" dst1="1.0"/>
<control-input axis="/controls/engines/engine[0]/throttle" control="COLLECTIVE"
src0="0.1" src1="1.0"
dst0="-.0007" dst1="-.0095"/>
</rotor>
<rotorgear
max-power-engine="2534"
max-power-rotor-brake="100"
rotorgear-friction="1.4"
engine-prop-factor="0.005"
engine-accel-limit="4"
yasimdragfactor="16"
yasimliftfactor="245"
>
<control-input axis="/controls/engines/engine[0]/magnetos" control="ROTORGEARENGINEON"/>
<control-input axis="/controls/rotor/brake" control="ROTORBRAKE"
src0="0.0" src1="1.0"
dst0="0.0" dst1="1.0"/>
</rotorgear>
<cockpit x="2" y=".45" z="0"/>
<fuselage ax="4.3" ay="0" az="0" bx="-3.35" by="0" bz="0"
width="2.1" taper="1" midpoint="0.5" idrag="0" cx="0.35" cy="0.7" cz="0.7"/>
<fuselage ax="-3.35" ay="0" az="-0.28" bx="-7.60" by="0" bz=".0.62"
width="0.40" taper="1" midpoint="0.5" idrag="0" cx="0.20" cy="0.4" cz="0.4"/>
<hstab x="-7.9" y="-0.5" z="1.3" taper="0.3" length="1.33" chord="0.74" sweep="0" incidence="0">
<stall aoa="16" width="4" peak="1.5"/>
</hstab>
<vstab x="-7.9" y="0" z="0.62" taper="0.6" length="1.46" chord="1.1" sweep="30">
<stall aoa="16" width="4" peak="1.5"/>
</vstab>
<!-- left -->
<gear x="-0.90" y="+1.40" z="-1.7" compression="0.35" spring="12" sfric="1" dfric="0.4">
<control-input axis="/controls/gear/brake-left" control="BRAKE" split="true"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE" split="true"/>
</gear>
<!-- right -->
<gear x="-0.90" y="-1.40" z="-1.7" compression="0.35" spring="12" sfric="1" dfric="0.4">
<control-input axis="/controls/gear/brake-right" control="BRAKE" split="true"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE" split="true"/>
</gear>
<!-- nose -->
<gear x="1.78" y="+0.00" z="-1.73" compression="0.35" spring="10" sfric="1" dfric="0.4"/>
<!-- tail skid -->
<gear x="-7.032" y="+0.00" z="-0.48" skid="1" compression="0.01" spring="0.1" sfric="1" dfric="1"/>
<!-- Left Door -->
<gear x="0" y="0" z="0" retract-time="4" compression="0">
<control-input axis="/controls/doors/left-door" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="4"/>
<control-output control="EXTEND" prop="/surface-positions/left-door-position"/>
</gear>
<!-- Right Door -->
<gear x="0" y="0" z="0" retract-time="4" compression="0">
<control-input axis="/controls/doors/right-door" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="4"/>
<control-output control="EXTEND" prop="/surface-positions/right-door-position"/>
</gear>
<tank x="0" y="0" z="-0.30" capacity="2220"/>
<tank x="0" y="0" z="-0.30" capacity="75"/>
<ballast x="2" y="0" z="-1" mass="1100"/>
<ballast x="1.6" y="+1.0" z="-0.7" mass="1200"/>
<ballast x="1.6" y="-1.0" z="-0.7" mass="1200"/>
<ballast x="-2" y="+0.8" z="0.4" mass="1700"/>
<ballast x="-2" y="-0.8" z="0.4" mass="1700"/>
<ballast x="-5" y="0" z="0.20" mass="450"/>
<weight x="2.0" y="0" z="1" mass-prop="/sim/weight[0]/weight-lb"/>
</airplane>