Oaxaca PE-210A Pegasus
| PE-210A | |
|---|---|
| |
| Role | Trainer/aerobatic |
| National origin | Mexico |
| Manufacturer | Oaxaca Aerospace |
| Status | In development |
| Number built | 1 |
The Pegasus PE-210A is a prototype of a single-engine trainer with canard developed by Oaxaca Aerospace and TechBA.
Design and development
[edit]Oaxaca Aerospace began the project in 2011 with the objective of designing an agile, fast and inexpensive two-seat airplane and concluded in mid-2013, the year in which the ground tests began. The aircraft has a rear mounted Lycoming AEIO-390 engine, canards and a tandem design cockpit with dual flight controls. The rear seat is at a higher level with respect to the front seat, which allows a view of 300° vertical and 240° horizontal. The aircraft was first presented to the public at Feria Aeroespacial México (FAMEX) 2015.[1]
Specifications
[edit]Data from FAMEX 2015[2]
General characteristics
[edit]- Crew: 2
- Length: 7.4 m
- Wingspan: 8.9 m
- Wing area: 12.5 m^2
- Canard area: 1.48 m^2
- Max. takeoff weight: 1250 kg
- Payload: 350 kg
- Powerplant: 1x Lycoming AEIO-390 210 HP
- Fuel capacity: 210 L
Performance
[edit]- Maximum speed: 221 kn / 410 km/h
- Cruise speed: 162 kn / 300 km/h
- Stall speed: 64 kn / 118 km/h
- Service ceiling: 18000 ft / 5400 m
- Range: 864 nmi / 1600 km
References
[edit]
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