CVS: data/Aircraft/Lockheed-NF104A nf104a-base.xml, 1.2, 1.3 nf104a-yasim.xml, 1.1, 1.2

Update of /var/cvs/FlightGear-0.9/data/Aircraft/Lockheed-NF104A
In directory baron.flightgear.org:/tmp/cvs-serv11715

Modified Files:
	nf104a-base.xml nf104a-yasim.xml 
Log Message:
- new update 

Index: nf104a-base.xml
===================================================================
RCS file: /var/cvs/FlightGear-0.9/data/Aircraft/Lockheed-NF104A/nf104a-base.xml,v
retrieving revision 1.2
retrieving revision 1.3
diff -u -r1.2 -r1.3
--- nf104a-base.xml	14 Feb 2010 12:46:36 -0000	1.2
+++ nf104a-base.xml	28 Mar 2010 12:11:46 -0000	1.3
@@ -54,14 +54,6 @@
       <min-lb>180</min-lb>
     </weight>
 
-    <help>
-      <title>Convair F 106 Delta Dart</title>
-      <key>
-        <name>d</name>
-        <desc>Open/Close canopy</desc>
-      </key>
-    </help>
-
     <replay>
       <disable>1</disable>
     </replay>
@@ -96,4 +88,12 @@
     <keyboard include="Nasal/nf104a-keyboard.xml"/>
   </input>
  
+  <nasal>
+    <nf104a>
+      <file>Aircraft/Lockheed-NF104A/Nasal/doors.nas</file>
+      <file>Aircraft/Lockheed-NF104A/Nasal/light.nas</file>
+      <file>Aircraft/Lockheed-NF104A/Nasal/liveries.nas</file>
+    </nf104a>
+  </nasal>
+   
 </PropertyList>

Index: nf104a-yasim.xml
===================================================================
RCS file: /var/cvs/FlightGear-0.9/data/Aircraft/Lockheed-NF104A/nf104a-yasim.xml,v
retrieving revision 1.1
retrieving revision 1.2
diff -u -r1.1 -r1.2
--- nf104a-yasim.xml	1 Oct 2009 13:56:57 -0000	1.1
+++ nf104a-yasim.xml	28 Mar 2010 12:12:03 -0000	1.2
@@ -8,10 +8,10 @@
      Envergure    :  7.84 m  ( 25 ft 9 in )
      Longueur     : 16.60 m  ( 54 ft 9 in )
      Hauteur      :  4.10 m  ( 13 ft 6 in )
-     Masse à vide : 6080 kg  ( 13500 lbs )
+     Masse a vide : 6080 kg  ( 13500 lbs )
      Moteur       : General Electric J79-GE-3B 9600 lbf
                   : Rocket AR 2                6000 lbf
-     Réservoirs   :
+     Reservoirs   :
 -->
 
 <airplane mass="13500">
@@ -33,15 +33,15 @@
   </cruise>
 
   <!-- pilot eyepoint -->
-  <cockpit x="-2.72" y="0" z=".80"/>
+  <cockpit x="3.597" y="0" z="-0.154"/>
 
-  <fuselage ax="6.902" ay="0" az="-0.952" bx="-6.923" by="0" bz="-0.382" width="1.187" midpoint= "0.7" />
+  <fuselage ax="6.902" ay="0" az="-0.952" bx="-6.923" by="0" bz="-0.382" width="1.187" midpoint= "0.25" taper="0.2" />
 
   <wing x="-2.012" y="0.567" z="-0.714"
         chord="3.108"
-        length="3.103"
+        length="3.15"
         taper="0.34"
-        sweep="10"
+        sweep="8"
         dihedral="-8"
         camber="0.023">
         <stall aoa="21" width="8" peak="1.3"/>
@@ -64,7 +64,7 @@
          chord="1.624"
          length="1.654"
          taper="0.30"
-         sweep="10">
+         sweep="0">
          <stall aoa="22" width="13" peak="1.5"/>
          <flap0 start="0" end="1.00" lift="1.9" drag="1.4"/>
 
@@ -78,7 +78,7 @@
          chord="3.270"
          length="1.696"
          taper="0.35"
-         sweep="35">
+         sweep="18">
          <stall aoa="27" width="10" peak="1.5"/>
          <flap0 start="0" end=".8" lift="1.3" drag="1.3"/>
 
@@ -88,7 +88,7 @@
          <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
   </vstab>
 
-  <jet x="-2.265" y="0" z="-0.729"
+  <jet x="0" y="0" z="-0.729"
        mass="2204"
        thrust="9600"
        afterburner="10000"
@@ -144,11 +144,11 @@
 
 
   <!-- left wing tanks -->
-  <tank x="-0.5" y="2.2" z="-0.7" jet="true" capacity="1000"/>
+  <tank x="-2" y="2.2" z="-0.7" jet="true" capacity="1000"/>
   <!-- right wing tanks -->
-  <tank x="-0.5" y="-2.2" z="-0.7" jet="true" capacity="1000"/>
+  <tank x="-2" y="-2.2" z="-0.7" jet="true" capacity="1000"/>
 
-  <!-- CG Théorique x=-2.012 y=0.0 z=-0.551 -->
-  <ballast x="4.2" y="0.0" z="-1.5" mass="1000" />
+  <!-- CG Theorique x=-2.012 y=0.0 z=-0.551 -->
+  <ballast x="7" y="0" z="-2" mass="1000" />
 
 </airplane>

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