Difference between revisions of "Tail Fin/Box"

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m (+type parameter; *ordered infobox parameters;)
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<noinclude>{{Data template used}}</noinclude>{{Infobox/Part
 
<noinclude>{{Data template used}}</noinclude>{{Infobox/Part
|file=
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|file=Tail_fin.png
 
|type=let
 
|type=let
 
|manufacturer=C7 Aerospace Division
 
|manufacturer=C7 Aerospace Division

Revision as of 02:12, 6 July 2014

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) 500.00 Funds
Mass (total) 0.02000 t
Drag 0.02
Max. Temp. 3400 K
Volume  ?
Impact Tolerance 12 m/s
Research Advanced construction.png Advanced Construction
Unlock cost 0 Funds
Since version 0.15
Part configuration [[Parts/Aero/tailfin/{{{filename}}}|{{{filename}}}]]
Lift generated 0.3
Drag coefficient 0.5