Difference between revisions of "Standard Canard/Box"

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m (*update to 1.0;)
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|part=airplaneFins
 
|part=airplaneFins
 
|more={{Infobox/Part/winglet
 
|more={{Infobox/Part/winglet
 +
|drag-coeff=0.5
 
|lift=0.52
 
|lift=0.52
|drag-coeff=0.5
 
 
}}
 
}}
 
{{Infobox/Part/control surface
 
{{Infobox/Part/control surface
 +
|area=1
 
|deflection=15
 
|deflection=15
|area=1
 
 
}}
 
}}
 
}}
 
}}

Revision as of 18:55, 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).
Standard Canard
Part image
Control surface by
C7 Aerospace Division
Cost (total) 720.00 Funds
Mass (total) 0.10 t
Drag 0.02
Max. Temp. 2000 K
Volume  ?
Impact Tolerance 12 m/s
Research Hypersonic flight.png Hypersonic Flight
Unlock cost 11 400 Funds
Since version 0.15
Part configuration standardCanard.cfg
Lift generated 0.52
Drag coefficient 0.5
Deflection range 15°
Surface area 1