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Delta Pegass

From Wikipedia, the free encyclopedia
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

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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)

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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

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Notes

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  1. ^ a b c Jackson 2004, p. 107

Bibliography

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  • 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.