Jora Jora

Source: Wikipedia, the free encyclopedia.
Jora
Jora Jora SRO landing on Drejø, Denmark
Role Two seat
ultralight
National origin Czech Republic
Manufacturer Jora Spol s.r.o.
Designer Oldrich Olsansky
Number built At least 161 by 2009

The Jora Jora is a

ultralight designed in the Czech Republic
in 1993. More than 160 had been sold by 2009.

Design and development

The Jora was designed by Oldrich Olsansky who also designed the similar

laminates, covered by polyester fabric. The main exception is the central fuselage section, which has a riveted tube frame.[1]

The Jora has separate wings with constant

flaperons), constructed like the wing, are attached to an auxiliary spar. Separate ailerons and flaps are an option, in which case the wing profile (airfoil) is changed from the laminar flow UA-2 to SL-1. The wings can be detached for transport, though wing folding is an option.[1]

Apart from its tube centre section the fuselage is wholly laminate with strengthening

The standard engine for the Jora is a 38.2 kW (52 hp)

two-stroke engine, housed under a short cowling. It can accept engines of up to 75 kW (100 hp).[1]

Operational history

By 2009 at least 161 Joras had been sold to customers in Australia, the Czech Republic, Denmark, Finland, France, Indonesia, Ireland, the Netherlands, Norway and South Africa.

Specifications (Rotax 582)

Data from Jane's All the World's Aircraft 2011/12[1]

General characteristics

  • Capacity: two
  • Length: 6.00 m (19 ft 8 in)
  • Wingspan: 10.60 m (34 ft 9 in)
  • Height: 1.95 m (6 ft 5 in)
  • Wing area: 12.50 m2 (134.5 sq ft) gross
  • Airfoil: UA-2 laminar flow
  • Empty weight: 225 kg (496 lb)
  • Max takeoff weight: 450 kg (992 lb)
  • Fuel capacity: 48 L (12.7 US gal; 10.6 Imp gal)
  • Powerplant: 1 × Rotax 582 two cylinder two stroke, 2.58:1 reduction gear, 38.8 kW (52.0 hp)
  • Propellers: 3-bladed Junkers, 1.60 m (5 ft 3 in) diameter carbon composite

Performance

  • Maximum speed: 140 km/h (87 mph, 76 kn)
  • Cruise speed: 120 km/h (75 mph, 65 kn)
  • Stall speed: 45 km/h (28 mph, 24 kn)
  • Never exceed speed: 162 km/h (101 mph, 87 kn)
  • Range: 563 km (350 mi, 304 nmi)
  • Service ceiling: 3,660 m (12,010 ft)
  • g limits: +4/-2
  • Rate of climb: 2.53 m/s (498 ft/min)
  • Wing loading: 36.0 kg/m2 (7.4 lb/sq ft) maximum
  • Power/mass: 86 W/kg

References


External links