Update to support horsepower

README.md

@@ -81,7 +81,7 @@ As an example, when you define a varient, say AIRBUS/A320/Varients/A320-111.txt,
 | ENG_NAME      | The name/model of the engines    				| IAE V2527E-A5 |
 | ENG_MAN      	| The name of the engine manufacturer    		| International Aero Engines |
 | ENG_MODEL     | The name of the engine model    				| V2527E-A5 |
-| ENG_THRUST    | Thrust per engine in newtons    				| 118320 |
+| ENG_THRUST    | Thrust per engine in newtons OR Power in horsepower (for prop/turbo props)    				| 118320 |
 | LENGTH      	| Length (nose to tail) in meters    			| 37.57 |
 | WINGSPAN     	| Wingspan in meters    						| 35.8 |
 | TAIL_HEIGHT   | Tail height in meters    						| 11.76 |

build/ALL_DATA.csv

@@ -816,8 +816,8 @@ AIRBUS,AIRBUS,0,A-300ST Beluga,A3ST,L,H,J,2,,,,,,,,,,,
 AIRBUS,AIRBUS,1,A-300ST Super Transporter,A3ST,L,H,J,2,,,,,,,,,,,,A-300ST Beluga
 AIRBUS,AIRBUS,1,Beluga,A3ST,L,H,J,2,,,,,,,,,,,,A-300ST Beluga
 AIRBUS,AIRBUS,1,Super Transporter,A3ST,L,H,J,2,,,,,,,,,,,,A-300ST Beluga
-AIRBUS,AIRBUS,0,A400M Atlas,A400,L,H,T,4,EP TP400-D6,Europrop International,TP400-D6,,45.1,42.4,14.7,4698,40000,422,116
-AIRBUS,AIRBUS,1,A400M Grizzly,A400,L,H,T,4,EP TP400-D6,Europrop International,TP400-D6,,45.1,42.4,14.7,4698,40000,422,116,A400M Atlas
+AIRBUS,AIRBUS,0,A400M Atlas,A400,L,H,T,4,EP TP400-D6,Europrop International,TP400-D6,11000,45.1,42.4,14.7,4698,40000,422,116
+AIRBUS,AIRBUS,1,A400M Grizzly,A400,L,H,T,4,EP TP400-D6,Europrop International,TP400-D6,11000,45.1,42.4,14.7,4698,40000,422,116,A400M Atlas
 AIRBUS,AIRBUS,0,C-212,C212,L,M,T,2,,,,,,,,,,,
 AIRBUS,AIRBUS,0,C-295,C295,L,M,T,2,,,,,,,,,,,
 AIRBUS,AIRBUS,1,C-295 Persuader,C295,L,M,T,2,,,,,,,,,,,,C-295

src/AIRBUS/A400/A400.txt

@@ -7,6 +7,7 @@ ENG_NUM=4
 ENG_NAME=EP TP400-D6
 ENG_MAN=Europrop International
 ENG_MODEL=TP400-D6
+ENG_THRUST=11000
 LENGTH=45.1
 WINGSPAN=42.4
 TAIL_HEIGHT=14.7