Research Article
Multistrand, Fast Reaction, Shape Memory Alloy System for Uninhabited Aerial Vehicle Flight Control
| | Wing | Horizontal tail | Vertical tail | |
| Span | 66.5 | 22 | 6 | in | Area | 650 | 110 | 40.5 | in∧2 | MGC LE FS | 12 | 38.5 | 33 | in | Aspect ratio | 6.8 | 4.4 | 0.9 | | Thickness ratio | 0.11 | | | | Total polyhedral angle | 8 | N/A | N/A | | Aileron chord ratio | 0.19 | N/A | N/A | | Aileron span ratio | 0.38 | N/A | N/A | | Root chord | 9.5 | 6.03 | 9.5 | in | Tip chord | 6 | 4.34 | 4.06 | in | Average chord | $7.75 | $5.18 | $6.78 | in |
| | Fuselage | | | |
| Length | 47 | in | | | Maximum height | 1.91 | in | | | Minimum width | 2.17 | in | | |
|
|