Ho X a "Alita" Data Table
Usage
Hang Glider
Fuselage Construction
Wood
Wing Construction
Capacity
Pilot
Span
7.5 m
Sweep Angle
33.7 degrees
Taper Ratio
5
Wing Root Thickness
20% chord
Wing Root Depth
2.5 m
Rib Spacing
0.2 m
Wing Area
11.2 m2
Aspect Ratio
Pilot position
Prone
Mid-section width
---
Cockpit width
0.80 m
Cockpit height (from seat)
0.5 m
Empty weight
38 kg
Ballast (water)
Additional payload
80 kg
Maximum weight
112 kg
Wing loading
10.0 kg/m2
Stall speed
42 km/h
Landing speed
Minimum Sink
0.80 m/s at 50 km/h and 10 kg/m2 loading
Best Glide Ratio
18:1 at 78 km/h and 10 kg/m2 loading
Maximum Speed
170 km/h