Difference between revisions of "Standard Canard/Box"
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m (*update to 0.25;) |
AlpacaMall (talk | contribs) m (Switched to new image file) |
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<noinclude>{{Data template used}}</noinclude> | <noinclude>{{Data template used}}</noinclude> | ||
{{Infobox/Part | {{Infobox/Part | ||
− | |file=Standard canard.png | + | |file=Standard canard v2.png |
|type=cs | |type=cs | ||
|manufacturer=C7 | |manufacturer=C7 | ||
|costs=720 | |costs=720 | ||
− | |mass=0. | + | |mass=0.1 |
|drag=0.02 | |drag=0.02 | ||
− | |temp= | + | |temp=2400 |
|tolerance=12 | |tolerance=12 | ||
− | |research= | + | |research=Advanced Aerodynamics |
|unlock cost=11400 | |unlock cost=11400 | ||
|since=0.15 | |since=0.15 | ||
|filename=standardCanard.cfg | |filename=standardCanard.cfg | ||
− | |part= | + | |part=airplaneFins |
|more={{Infobox/Part/winglet | |more={{Infobox/Part/winglet | ||
− | |||
|drag-coeff=0.5 | |drag-coeff=0.5 | ||
+ | |lift=0.52 | ||
}} | }} | ||
{{Infobox/Part/control surface | {{Infobox/Part/control surface | ||
− | | | + | |area=1 |
− | | | + | |deflection=15 |
}} | }} | ||
}} | }} |
Latest revision as of 06:01, 7 September 2021
Standard Canard | ||
Control surface by C7 Aerospace Division | ||
Cost | (total) | 720.00 |
Mass | (total) | 0.10 t |
Drag | 0.02 | |
Max. Temp. | 2400 K | |
Volume | ? | |
Impact Tolerance | 12 m/s | |
Research | Advanced Aerodynamics | |
Unlock cost | 11 400 | |
Since version | 0.15 | |
Part configuration | standardCanard.cfg | |
Lift generated | 0.52 | |
Drag coefficient | 0.5 | |
Deflection range | 15° | |
Surface area | 1 |