A320-family/A320-100-CFM.xml

<?xml version="1.0"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>

<!-- Copyright (c) 2020 Josh Davidson (Octal450) -->

<fdm_config name="A320-family" version="2.0" release="BETA"
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">

	<fileheader>
		<author>Joshua Davidson (Octal450)</author>
		<version>Pre V1.0</version>
		<description>A32X FDE</description>
	</fileheader>
	
	<metrics file="Systems/a320-metrics"/>
	<mass_balance file="Systems/a320-mass-balance"/>
	<ground_reactions file="Systems/a320-ground-reactions"/>
	
	<propulsion>
		<engine file="cfm56_5a1_1">
			<location unit="M">
				<x> 14.3962788 </x>
				<y> -5.755 </y>
				<z> -1.04768 </z>
			</location>
			<orient unit="DEG">
				<roll> 0.0 </roll>
				<pitch> 2.2 </pitch>
				<yaw> 1 </yaw>
			</orient>
			<feed>5</feed>
			<thruster file="direct">
				<location unit="M">
					<x> 14.3962788 </x>
					<y> -5.755 </y>
					<z> -1.04768 </z>
				</location>
				<orient unit="DEG">
					<roll> 0.0 </roll>
					<pitch> 2.2 </pitch>
					<yaw> 1 </yaw>
				</orient>
			</thruster>
		</engine>
		
		<engine file="cfm56_5a1_2">
			<location unit="M">
				<x> 14.3962788 </x>
				<y> 5.755 </y>
				<z> -1.04768 </z>
			</location>
			<orient unit="DEG">
				<roll> 0.0 </roll>
				<pitch> 2.2 </pitch>
				<yaw> -1 </yaw>
			</orient>
			<feed>6</feed>
			<thruster file="direct">
				<location unit="M">
					<x> 14.3962788 </x>
					<y> 5.755 </y>
					<z> -1.04768 </z>
				</location>
				<orient unit="DEG">
					<roll> 0.0 </roll>
					<pitch> 2.2 </pitch>
					<yaw> -1 </yaw>
				</orient>
			</thruster>
		</engine>
		
		<engine file="APS3200">
			<location unit="M">
				<x> 38.9 </x>
				<y> 0 </y>
				<z> 0.95 </z>
			</location>
			<orient unit="DEG">
				<roll> 0.0 </roll>
				<pitch> 0.0 </pitch>
				<yaw> 0.0 </yaw>
			</orient>
			<feed>7</feed>
			<thruster file="direct">
				<location unit="M">
					<x> 38.9 </x>
					<y> 0 </y>
					<z> 0.95 </z>
				</location>
				<orient unit="DEG">
					<roll> 0.0 </roll>
					<pitch> 0.0 </pitch>
					<yaw> 0.0 </yaw>
				</orient>
			</thruster>
		</engine>
		
		<tank type="FUEL">	  <!-- Outer Left Wing Tank -->
			<location unit="M">
				<x> 18.9231 </x>
				<y> -5.1104 </y>
				<z> -0.61182 </z>
			</location>
			<capacity unit="LBS"> 1523.00 </capacity>
			<contents unit="LBS"> 1523.00 </contents>
			<unusable-volume unit="LTR"> 4.0 </unusable-volume>
			<priority>1</priority>
			<density unit="LBS/GAL">6.71</density>
			<temperature>50</temperature>
		</tank>
		<tank type="FUEL">	  <!-- Inner Left Wing Tank -->
			<location unit="M">
				<x> 18.9231 </x>
				<y> -5.1104 </y>
				<z> -0.61182 </z>
			</location>
			<capacity unit="LBS"> 12272.90 </capacity>
			<contents unit="LBS">  6000.00 </contents>
			<unusable-volume unit="LTR"> 28.0 </unusable-volume>
			<priority>1</priority>
			<density unit="LBS/GAL">6.71</density>
			<temperature>50</temperature>
		</tank>
		
		<tank type="FUEL">	  <!-- Center Tank - wing box may be modified to center fuel tank on the -100 so we have a center tank. Or mostly because its easier... -->
			<location unit="M">
				<x> 18.9731 </x>
				<y> 0 </y>
				<z> -0.61182 </z>
			</location>
			<capacity unit="LBS"> 14623.00 </capacity>
			<contents unit="LBS"> 42 </contents>
			<unusable-volume unit="LTR"> 23.20 </unusable-volume>
			<priority>1</priority>
			<density unit="LBS/GAL">6.71</density>
			<temperature>50</temperature>
		</tank>
		<tank type="FUEL">	  <!-- Inner Right Wing Tank -->
			<location unit="M">
				<x> 18.9231 </x>
				<y> 5.1104 </y>
				<z> -0.61182 </z>
			</location>
			<capacity unit="LBS"> 12272.90 </capacity>
			<contents unit="LBS">  6000.00 </contents>
			<unusable-volume unit="LTR"> 28.0 </unusable-volume>
			<priority>1</priority>
			<density unit="LBS/GAL">6.71</density>
			<temperature>50</temperature>
		</tank>
		<tank type="FUEL">	  <!-- Outer Right Wing Tank -->
			<location unit="M">
				<x> 18.9231 </x>
				<y> 5.1104 </y>
				<z> -0.61182 </z>
			</location>
			<capacity unit="LBS"> 1523.00 </capacity>
			<contents unit="LBS"> 1523.00 </contents>
			<unusable-volume unit="LTR"> 4.0 </unusable-volume>
			<priority>1</priority>
			<density unit="LBS/GAL">6.71</density>
			<temperature>50</temperature>
		</tank>
		<tank type="FUEL">	  <!-- Engine 1 Pipes -->
			<location unit="M">
				<x> 18.8231 </x>
				<y> 0 </y>
				<z> 0.19249 </z>
			</location>
			<capacity unit="LBS">10</capacity>
			<contents unit="LBS">0</contents>
			<priority>1</priority>
			<density unit="LBS/GAL">6.71</density>
		</tank>
		<tank type="FUEL">	  <!-- Engine 2 Pipes -->
			<location unit="M">
				<x> 18.8231 </x>
				<y> 0 </y>
				<z> 0.19249 </z>
			</location>
			<capacity unit="LBS">10</capacity>
			<contents unit="LBS">0</contents>
			<priority>1</priority>
			<density unit="LBS/GAL">6.71</density>
		</tank>
		<tank type="FUEL">	  <!-- APU Pipes -->
			<location unit="M">
				<x> 18.8231 </x>
				<y> 0 </y>
				<z> 0.19249 </z>
			</location>
			<capacity unit="LBS">10</capacity>
			<contents unit="LBS">0</contents>
			<priority>1</priority>
			<density unit="LBS/GAL">6.71</density>
		</tank>
	</propulsion>
	
	<system file="glass-effect"/>
	<system file="a320-fbw"/>
	<system file="a320-fcs"/>
	<system file="a320-fuel"/>
	<system file="a320-fwc"/>
	<system file="a320-fwc-phases"/>
	<system file="a320-spoiler"/>
	<system file="a320-electrical"/>
	<system file="a320-hydraulic"/>
    <system file="a320-pneumatic"/>
    <system file="a320-aircond"/> <!-- after pneu -->
	<system file="a320-lights"/>
	<system file="a320-engine-fire"/>
	<system file="a320-adr"/>
	<system file="a320-apu"/>
	<system file="a320-oxygen"/>
	<system file="a320-fmgc"/>
	<system file="a320-misc"/>
	
	<flight_control name="none"/>
	<aerodynamics file="Systems/a320-aerodynamics.xml"/>
	<external_reactions file="Systems/a320-external-reactions"/>

</fdm_config>