Engineering:Oaxaca PE-210A Pegasus
From HandWiki
Revision as of 02:17, 8 June 2022 by imported>Rtexter1 (add)
| 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
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
Data from FAMEX 2015[2]
General characteristics
- 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
- 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
- ↑ "-Oaxaca Aerospace unveils 1st prototype of airplane developed in Mexico". 29 April 2015. https://www.efe.com/efe/english/business/oaxaca-aerospace-unveils-1st-prototype-of-airplane-developed-in-mexico/50000265-2599362.
- ↑ Archived at Ghostarchive and the Wayback Machine: Pegasus PE-210A de Oaxaca Aerospace en la Feria Aeroespacial México 2015. YouTube.
 |  |
