Ho II Data Table
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
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