Difference between revisions of "FAT-455 Aeroplane Tail Fin/Box"

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(+added in 1.0;)
 
m (*update to 1.0.2;)
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|part=airlinerWings
 
|part=airlinerWings
 
|more={{Infobox/Part/winglet
 
|more={{Infobox/Part/winglet
 +
|drag-coeff=0.6
 
|lift=2.69
 
|lift=2.69
|drag-coeff=0.6
 
 
}}
 
}}
 
{{Infobox/Part/control surface
 
{{Infobox/Part/control surface
 +
|area=0.37
 
|deflection=15
 
|deflection=15
|area=0.37
 
 
}}
 
}}
 
}}
 
}}

Revision as of 18:57, 3 May 2015

This is a data template. To add content which doesn't belong to this template edit the English page (or one of its translations).
FAT-455 Aeroplane Tail Fin
Part image
Control surface by
WinterOwl Aircraft Emporium
Cost (total) 1 000.00 Funds
Mass (total) 0.36 t
Drag 0.02
Max. Temp. 1200 K
Volume  ?
Impact Tolerance 15 m/s
Research Experimental aerodynamics.png Experimental Aerodynamics
Unlock cost 4 000 Funds
Since version 1.0
Part configuration TailFin.cfg
Lift generated 2.69
Drag coefficient 0.6
Deflection range 15°
Surface area 0.37