| Wing span | 23 m |
| MTOW | 105 kg |
| MR speed | ~20 KTAS |
| MCR speed | 45 KTAS |
| Max endurance | >400 hrs |
| Max useful load (fuel & payload) | 49 kg |





| developed by | TadMcGeer at al, Underwood, WA |
| Span | 3m |
| MTOW | 14kg |
| max payload + fuel | 5 kg |
| Engine | Enya 4cycle 800 W |
| max altitude | 15000 ft |
| vy @ MTOW | 40 KEAS |
| Manufacturer | Aurora Flight Sciences, Manassas, VA |
| Span | 18.1 m |
| MTOW | 800 kg |
| Max payload | 50 kg |
| Engine | Rotax 912, 4cycle, 80 HP, closed cycle, liquid cooled |
| prop | 2 composite blades, dia=4.4m, 600...1200 rpm |
| Vy | 50 KEAS |
| Design altitude | FL850 |