Difference between revisions of "Standard Canard/Box"
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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 | ||
− | |||
}} | }} | ||
{{Infobox/Part/control surface | {{Infobox/Part/control surface | ||
+ | |area=1 | ||
|deflection=15 | |deflection=15 | ||
− | |||
}} | }} | ||
}} | }} |
Revision as of 18:55, 3 May 2015
Standard Canard | ||
Control surface by C7 Aerospace Division | ||
Cost | (total) | 720.00 |
Mass | (total) | 0.100 t |
Drag | 0.02 | |
Max. Temp. | 2000 K | |
Impact Tolerance | 12 m/s | |
Research | Hypersonic Flight | |
Unlock cost | 11 400 | |
Since version | 0.15 | |
Part configuration | standardCanard.cfg | |
Lift generated | 0.52 | |
drag-coeff | 0.5 | |
Lift generated | {{{lift}}} | |
Cont. surf. portion | 100% | |
Deflection range | {{{range}}}° | |
Actuator Speed | {{{speed}}}°/s |