Engineering:Delta Pegass
From HandWiki
| Pegass | |
|---|---|
| Role | Two-seat ultralight cabin monoplane |
| National origin | Czech Republic |
| Manufacturer | Delta System-Air |
| First flight | 1995 |
The Delta Pegass is a Czech two-seat ultralight cabin monoplane designed and built by Delta System-Air.[1]
Design
The Pegass is a strut-braced high-wing monoplane powered by either an 80 hp (60 kW) Rotax 912UL or a 64 hp (48 kW) Rotax 582UL engine driving a three-bladed tractor propeller. It has a fixed tricycle landing gear and a cabin with two seats side-by-side, a door on each side of the fuselage for access.[1]
Specifications (Rotax 912UL)
Data from Jane's All the World's Aircraft 2004-05[1]
General characteristics
- Crew: 1
- Capacity: 1
- Length: 5.70 m (18 ft 8.5 in)
- Wingspan: 10.19 m (33 ft 5.25 in)
- Height: 2.37 m (7 ft 9.25 in)
- Wing area: 14.36 m2 (153.5 sq ft)
- Empty weight: 225 kg (496 lb)
- Gross weight: 450 kg (992 lb)
- Powerplant: 1 × Rotax 912UL , 60 kW (80 hp)
Performance
- Maximum speed: 170 km/h (105 mph, 91 kn)
- Stall speed: 65 km/h (41 mph, 36 kn)
- Endurance: 4 hours 0 minutes
References
Notes
Bibliography
- Jackson, Paul, ed (2004). Jane's All the World's Aircraft 2004-2005. Coulsdon, Surrey, United Kingdom: Jane's Information Group. ISBN 978-0-7106-2614-1.
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