Difference between revisions of "Tail Fin/Box"

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m (*update to 0.25;)
m (*update to 1.0;)
Line 4: Line 4:
 
|manufacturer=C7
 
|manufacturer=C7
 
|costs=600
 
|costs=600
|mass=0.02
+
|mass=0.125
 
|drag=0.02
 
|drag=0.02
|temp=3400
+
|temp=2000
 
|tolerance=12
 
|tolerance=12
 
|research=Aerodynamics
 
|research=Aerodynamics
 
|unlock cost=3800
 
|unlock cost=3800
 
|since=0.15
 
|since=0.15
|filename=part.cfg
+
|filename=tailfin.cfg
|part=tailfin
+
|part=airplaneFins
 
|more={{Infobox/Part/winglet
 
|more={{Infobox/Part/winglet
|lift=0.3
+
|lift=0.61
|drag-coeff=0.5
+
|drag-coeff=0.6
 +
}}
 +
{{Infobox/Part/control surface
 +
|deflection=25
 +
|area=1
 
}}
 
}}
 
}}
 
}}

Revision as of 10:05, 29 April 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).
Tail Fin
Part image
Winglet by
C7 Aerospace Division
Cost (total) 600.00 Funds
Mass (total) 0.125 t
Drag 0.02
Max. Temp. 2000 K
Impact Tolerance 12 m/s
Research Tech tree aerodynamics.png Aerodynamics
Unlock cost 3 800 Funds
Since version 0.15
Part configuration tailfin.cfg
Lift generated 0.61
drag-coeff 0.6
Lift generated {{{lift}}}
Cont. surf. portion 100%
Deflection range {{{range}}}°
Actuator Speed {{{speed}}}°/s