The Pegasus PE-210A is a prototype of a single-engine trainer with canard developed by Oaxaca Aerospace and TechBA.
| PE-210A | |
|---|---|
 | |
| General information | |
| Type | Trainer/aerobatic |
| National origin | Mexico |
| Manufacturer | Oaxaca Aerospace |
| Status | In development |
| Number built | 1 |
Design and development
editOaxaca 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
editData from FAMEX 2015[2]
General characteristics
- Crew: 2
- Length: 24 ft 3 in (7.4 m)
- Wingspan: 29 ft 2 in (8.9 m)
- Wing area: 135 sq ft (12.5 m2)
- Empty weight: 2,756 lb (1,250 kg)
- Max takeoff weight: 661 lb (300 kg)
- Fuel capacity: 55.5 US Gallons (210 litres)
- Powerplant: 1 × Lycoming AEIO-390 , 210 hp (160 kW)
Performance
- Maximum speed: 220 kn (250 mph, 410 km/h)
- Cruise speed: 160 kn (190 mph, 300 km/h)
- Stall speed: 64 kn (73 mph, 118 km/h)
- Range: 860 nmi (990 mi, 1,600 km)
- Service ceiling: 17,700 ft (5,400 m)
References
edit
Wikimedia Commons has media related to Oaxaca PE-210A Pegasus.
- ↑ "Oaxaca Aerospace unveils 1st prototype of airplane developed in Mexico". Agencia EFE. April 29, 2025. Archived from the original on December 12, 2019. Retrieved March 10, 2025.
- ↑ Archived at Ghostarchive and the Wayback Machine: Pegasus PE-210A de Oaxaca Aerospace en la Feria Aeroespacial México 2015. YouTube.