Sim: Block 42 re-engined with F100-PW-229 as per ANG mod

Goodbye WAP.
BobDotCom · Jan 30, 2023 · 1a4ee45 · 1a4ee45
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Showing 8 changed files with 155 additions and 18 deletions.
diff --git a/Engines/F100-PW-220.xml b/Engines/F100-PW-220.xml
@@ -22,7 +22,7 @@
   <injected>          0 </injected>
 
   <!--
-      The engine used for block 20, 42 and 32.
+      The engine used for block 20 and 32 (previously also 42).
 
       Sources:
               Turbofan and Turbojet Engines: Database Handbook by Elodie Roux

diff --git a/Engines/F100-PW-229.xml b/Engines/F100-PW-229.xml
@@ -22,7 +22,7 @@
   <injected>          0 </injected>
 
   <!--
-      The engine used for block 52.
+      The engine used for block 52 and 42.
 
       Sources:
               Turbofan and Turbojet Engines: Database Handbook by Elodie Roux

diff --git a/README.md b/README.md
@@ -19,7 +19,7 @@ Includes the following Aircraft variants:
 - F-16C Block 30
 - F-16C Block 32
 - F-16CM Block 40 (CCIP)
-- F-16CM Block 42 (CCIP)
+- F-16CM Block 42 (CCIP, ANG)
 - F-16CJ Block 50
 - F-16CJ Block 52 (default version)
 - F-16E Block 60

diff --git a/Systems/f16-help.xml b/Systems/f16-help.xml
@@ -548,17 +548,17 @@ This test function can be found on the FUEL SELECTOR panel. It causes a fixed am
             ]]></text-12>
             <text-13><![CDATA[
 VARIANTS
-- F-16E Block 60: 19000/32500 lbf. Large horz. tail (mod. aero data).
-- F-16CJ Block 52: 17800/29000 lbf. Large horz. tail (mod. aero data).
-- F-16CJ Block 50: 17000/29000 lbf. Large horz. tail (mod. aero data).
-- F-16CM Block 42 (CCIP): 14670/23830 lbf. Large horz. tail (mod. aero data).
-- F-16CM Block 40 (CCIP): 18330/28620 lbf. Large horz. tail (mod. aero data).
-- F-16C Block 32: 14670/23830 lbf. Large horz. tail (mod. aero data).
-- F-16C Block 30: 18330/28620 lbf. Large horz. tail (mod. aero data).
-- F-16AM Block 20 (MLU 4.3 tape): 14670/23830 lbf. Small horz. tail (auth. aero data).
-- F-16A Block 10: 14670/23830 lbf. Small horz. tail (auth. aero data). Engine has authentic power curves.
-- YF-16: 14670/23830 lbf. Small horz. tail (auth. aero data). Engine has authentic power curves. The FBW in this variant has no spin, nose-slide or deep stall protection.
-- F-16 Simplified : 17800/29000 lbf.  Uses custom FBW, which can be switched off, made for FG and aero data. It is a simplified version of the other versions.
+- F-16E Block 60:  19000/32500 lbf. Large horz. tail (mod. aero data).
+- F-16CJ Block 52:  17800/29000 lbf. Large horz. tail (mod. aero data).
+- F-16CJ Block 50:  17000/29000 lbf. Large horz. tail (mod. aero data).
+- F-16CM Block 42 (CCIP, ANG):  17800/29000 lbf. Large horz. tail (mod. aero data).
+- F-16CM Block 40 (CCIP):  18330/28620 lbf. Large horz. tail (mod. aero data).
+- F-16C Block 32:  14670/23830 lbf. Large horz. tail (mod. aero data).
+- F-16C Block 30:  18330/28620 lbf. Large horz. tail (mod. aero data).
+- F-16AM Block 20 (MLU tape 4.3):  14670/23830 lbf. Small horz. tail (auth. aero data).
+- F-16A Block 10:  14670/23830 lbf. Small horz. tail (auth. aero data). Engine has authentic power curves.
+- YF-16:  14670/23830 lbf. Small horz. tail (auth. aero data). Engine has authentic power curves. The FBW in this variant has no spin, nose-slide or deep stall protection.
+- F-16 Simplified :  17800/29000 lbf.  Uses custom FBW, which can be switched off, made for FG and aero data. It is a simplified version of the other versions.
 
 The engines vary not only in thrust, but also in fuel consumption. Furthermore they differ in empty weight. Different Blocks have different sets of cockpit panels, MFDs and HSI/EHSI, alongside other changes. Variants will also have different sets of liveries that can be selected. There is also small changes in tail for different variants with and without braking chute.
             ]]></text-13>

diff --git a/Systems/jsb-mass-42.xml b/Systems/jsb-mass-42.xml
@@ -7,7 +7,7 @@
   <ixy unit="SLUG*FT2"> 0 </ixy>
   <ixz unit="SLUG*FT2"> 982 </ixz><!-- why is this negated when flying???? -->
   <iyz unit="SLUG*FT2"> 0 </iyz>
-  <emptywt unit="LBS"> 17200 </emptywt>
+  <emptywt unit="LBS"> 17800 </emptywt> <!-- Original 17200. With F100-PW-229, total is ca. 600lbs heavier. Sources: PW, USAF -->
   <location name="CG" unit="IN">
    <x> 8.5 </x><!-- See comment in metrics.xml -->
    <y> 0 </y>

diff --git a/Systems/jsb-propulsion-block42.xml b/Systems/jsb-propulsion-block42.xml
@@ -0,0 +1,137 @@
+<?xml version="1.0"?>
+
+ <propulsion>
+  <engine file="F100-PW-229">
+   <!--feed>0</feed>
+   <feed>1</feed>
+   <feed>2</feed>
+   <feed>3</feed-->
+   <feed>4</feed>
+   <feed>5</feed>
+   <!--feed>6</feed>
+   <feed>7</feed>
+   <feed>8</feed-->
+   <thruster file="direct">
+    <location unit="M">
+     <x> 4.2077 </x>
+     <y> 0 </y>
+     <z> 0 </z>
+    </location>
+    <orient unit="DEG">
+     <roll> 0.0 </roll>
+     <pitch> 0.0 </pitch>
+     <yaw> 0.0 </yaw>
+    </orient>
+   </thruster>
+  </engine>
+  <!--
+          This is a pseudo fuel system.
+          As can be read in manual it should have 12 tanks,
+          including possibility for 3 droptanks.
+          And engine only draws fuel from 2 of them.
+
+          Total internal JP-8 should be: 7160
+          Total external JP-8 should be: 9740 (the big tanks, there is 2 sizes)
+  -->
+  <refuel-rate unit="LBS/MIN"> 6000 </refuel-rate>
+  <dump-rate unit="LBS/MIN"> 1000 </dump-rate>
+  <tank type="FUEL"> <!-- FWD Tank F-1 / F-2 -->
+   <location unit="IN">
+    <x> -51.5 </x>
+   <y> 0 </y>
+   <z> 0 </z>
+   </location>
+   <capacity unit="LBS"> 2550.0 </capacity>
+   <contents unit="LBS"> 2550.0 </contents>
+   <type>JP-8</type>
+   <priority> 5 </priority>
+  </tank>
+  <tank type="FUEL"> <!-- Left wing tank -->
+   <location unit="IN">
+    <x> 8.5 </x>
+   <y> -80 </y>
+   <z>   0 </z>
+   </location>
+   <capacity unit="LBS"> 550 </capacity>
+   <contents unit="LBS"> 550 </contents>
+   <type>JP-8</type>
+   <priority> 4 </priority>
+  </tank>
+  <tank type="FUEL"> <!-- Right wing tank -->
+   <location unit="IN">
+    <x> 8.5 </x>
+   <y>  80 </y>
+   <z>   0 </z>
+   </location>
+   <capacity unit="LBS"> 550 </capacity>
+   <contents unit="LBS"> 550 </contents>
+   <type>JP-8</type>
+   <priority> 4 </priority>
+  </tank>
+  <tank type="FUEL"> <!-- AFT Tank A-1 -->
+   <location unit="IN">
+    <x> 68.5 </x>
+   <y> 0 </y>
+   <z> 0 </z>
+   </location>
+   <capacity unit="LBS"> 2550.0 </capacity>
+   <contents unit="LBS"> 2550.0 </contents>
+   <type>JP-8</type>
+   <priority> 5 </priority>
+  </tank>
+  <tank type="FUEL"> <!-- FWD Reservoir -->
+    <location unit="IN">
+    <x> -51.5 </x>
+   <y> 0 </y>
+   <z> 0 </z>
+   </location>
+   <capacity unit="LBS"> 480.0 </capacity>
+   <contents unit="LBS"> 480.0 </contents>
+   <type>JP-8</type>
+   <priority> 6 </priority>
+  </tank>
+  <tank type="FUEL"> <!-- AFT Reservoir -->
+    <location unit="IN">
+    <x> 68.5 </x>
+   <y> 0 </y>
+   <z> 0 </z>
+   </location>
+   <capacity unit="LBS"> 480.0 </capacity>
+   <contents unit="LBS"> 480.0 </contents>
+   <type>JP-8</type>
+   <priority> 6 </priority>
+  </tank>
+  <tank type="FUEL"> <!-- Left External Tank -->
+   <location unit="IN">
+    <x> -16.5 </x>
+   <y> -64.129 </y>
+   <z> -40 </z>
+   </location>
+   <capacity unit="LBS"> 3996 </capacity>
+   <contents unit="LBS"> 0 </contents>
+   <type>JP-8</type>
+   <priority> 3 </priority>
+  </tank>
+  <tank type="FUEL"> <!-- Right External Tank -->
+   <location unit="IN">
+    <x> -16.5 </x>
+   <y> 64.129 </y>
+   <z> -40 </z>
+   </location>
+   <capacity unit="LBS"> 3996 </capacity>
+   <contents unit="LBS"> 0 </contents>
+   <type>JP-8</type>
+   <priority> 3 </priority>
+  </tank>
+  <tank type="FUEL"> <!-- Center External Tank -->
+   <location unit="IN">
+    <x> -16.5 </x>
+   <y>   0 </y>
+   <z> -50 </z>
+   </location>
+   <capacity unit="LBS"> 1998 </capacity>
+   <contents unit="LBS"> 0 </contents>
+   <type>JP-8</type>
+   <priority> 2 </priority>
+  </tank>
+ </propulsion>
diff --git a/f16-block-42-set.xml b/f16-block-42-set.xml
@@ -5,7 +5,7 @@
  <sim>
   <description>General Dynamics F-16CM Block 42</description>
   <long-description>
-   The General Dynamics F-16CM Fighting Falcon (or Night Falcon) is a single-engine supersonic multirole fighter aircraft originally developed by General Dynamics (now Lockheed Martin) for the United States Air Force (USAF). Powered by F110-GE-100. Designed as an air superiority day fighter, it evolved into a successful all-weather multirole aircraft.
+   The General Dynamics F-16CM Fighting Falcon (or Night Falcon) is a single-engine supersonic multirole fighter aircraft originally developed by General Dynamics (now Lockheed Martin) for the United States Air Force (USAF). Powered by F100-PW-229 (ANG upgrade). Designed as an air superiority day fighter, it evolved into a successful all-weather multirole aircraft.
    Block 40/42 introduced LANTIRN pods, GPS, upgraded APG-68 radar, ATF and more. The Common Configuration Implementation Program (CCIP) is a modernization effort that seeks to standardize all USAF Block 40/42/50/52 F-16s to a common Block 50/52-based avionics software and hardware configuration. This includes features like new MMC, Colored MFDs, advanced IFF and Sniper ATP. Modified F-16CGs have been designated as CM.
   </long-description>
   <author>Erik Hofman, Martin "Pegasus" Schmitt, Pensacola, Nikolai V. Chr., J Maverick 16, Richard Harrison, Josh Davidson, Martien Van Der P., Jonathan Redpath, Gary Brown, Justin Nicholson, Enrico Castaldi, Timi, Barszczisbad, PH-JAKE, Bat Campion</author>
@@ -227,7 +227,7 @@
 
  <engines>
     <engine>
-      <rated-mil-dry type="double">14670</rated-mil-dry>
+      <rated-mil-dry type="double">17800</rated-mil-dry>
     </engine>
   </engines>
 

diff --git a/f16b42.xml b/f16b42.xml
@@ -57,7 +57,7 @@
  <system file="jsb-misc"/>
  <flight_control file="Systems/jsb-controls"/>
  <system file="autoflight"/>
- <propulsion file="Systems/jsb-propulsion-block32"/>
+ <propulsion file="Systems/jsb-propulsion-block42"/>
  <aerodynamics file="Systems/jsb-aerodynamics-block15-subtle.xml"/>