Difference between revisions of "Delta Wing/Box"

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|drag-coeff=0.6
 
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|lift=2.0
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{{Infobox/Part/lifting surface
 
{{Infobox/Part/lifting surface

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).
Delta Wing
Part image
Wing by
C7 Aerospace Division
Cost (total) 600.00 Funds
Mass (total) 0.20 t
Drag 0.02
Max. Temp. 2000 K
Volume  ?
Impact Tolerance 15 m/s
Research Tech tree aerodynamics.png Aerodynamics
Unlock cost 6 400 Funds
Since version 0.15
Part configuration delta.cfg
Lift generated 2.0
Drag coefficient 0.6
Lift generated 2.0