Usage

Experimenta l

Fuselage Construction

Steel Tube

Wing Construction

Wood

Capacity

Pilot

Span

16.5 m

Sweep Angle

29.5 degrees

Taper Ratio

8.4

Wing Root Thickness

20% chord

Wing Root Depth

3.5 m

Rib Spacing

0.4 m (0.2 at the wing leading edge)

Wing Area

32.0 m²

Aspect Ratio

8.5

Pilot position

Seated

Mid-section width

2.4 m

Cockpit width

0.8 m

Cockpit height (from seat)

0.70 m (plus cockpit bubble of 0.3 m)

Empty weight

250 kg

Ballast (water)

---

Additional payload

80 kg

Maximum weight

330 kg

Wing loading

10.3 kg/m²

Stall speed

42 km/h

Landing speed

42 km/h

Minimum Sink

0.7 m/s at 60 km/h and 10.3 kg/m² loading

Best Glide Ratio

24:1 at 72 km/h and 10.3 kg/m² loading

Maximum Speed (horizontal)

230 km/h

Maximum Speed

230 km/h