Difference between revisions of "Tail Fin"

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* Initial Release
* Initial Release

Revision as of 18:37, 31 July 2014

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
Impact Tolerance 12 m/s
Research Aviation.png Aviation
Unlock cost 3 800 Funds
Since version 0.15
Part configuration airplaneFins
Lift generated 0.61
Drag coefficient 0.6
Deflection range 25°
Surface area 1

This tailfin has passed extensive modeling in our patented P.A.S system.(Paper Airplane Simulation). This fin has been blunted to prevent accidental dismemberment of installing technicians.

C7 Aerospace Division


  • Initial Release