Difference between revisions of "Tail Fin/Box"

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m (*update to 1.0.2;)
m (*update to 1.0.4;)
 
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|mass=0.125
 
|mass=0.125
 
|drag=0.02
 
|drag=0.02
|temp=2000
+
|temp=2400
 
|tolerance=12
 
|tolerance=12
 
|research=Aviation
 
|research=Aviation

Latest revision as of 12:09, 27 June 2015

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Tail Fin
Part image
Winglet by
C7 Aerospace Division
Cost (total) 600.00 Funds
Mass (total) 0.13 t
Drag 0.02
Max. Temp. 2400 K
Volume  ?
Impact Tolerance 12 m/s
Research Aviation.png Aviation
Unlock cost 3 800 Funds
Since version 0.15
Part configuration tailfin.cfg
Lift generated 0.61
Drag coefficient 0.6
Deflection range 25°
Surface area 1