Difference between revisions of "Tail Fin"
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+ | The '''Tail Fin''' is a [[winglet]] with a marginally small amount of lift and drag. | ||
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Revision as of 15:45, 19 August 2018
Tail Fin | ||
Winglet by C7 Aerospace Division | ||
Cost | (total) | 600.00 ![]() |
Mass | (total) | 0.13 t |
Drag | 0.02 | |
Max. Temp. | 2400 K | |
Volume | ? | |
Impact Tolerance | 12 m/s | |
Research | ![]() | |
Unlock cost | 3 800 ![]() | |
Since version | 0.15 | |
Part configuration | tailfin.cfg | |
Lift generated | 0.61 | |
Drag coefficient | 0.6 | |
Deflection range | 25° | |
Surface area | 1 |
The Tail Fin is a winglet with a marginally small amount of lift and drag.
“ | 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 |
” |
Changes
- Initial Release