Ho X (XIII b) Data Table
Usage
Experimental
Fuselage Construction
Steel tubing
Wing Construction
Wood
Capacity
Pilot
Span
7.2 m
Sweep Angle
70 degrees
Taper Ratio
20
Wing Root Thickness
7% chord
Wing Root Depth
10 m
Rib Spacing
0.3 m
Wing Area
37.8 m2
Aspect Ratio
1.4
Pilot position
Recumbent (lying on the back)
Mid-section width
---
Cockpit width
0.60 m
Cockpit height (from seat)
0.70 m
Empty weight
600 kg
Ballast (water)
Additional payload
100 kg
Maximum weight
700 kg
Wing loading
18.5 kg/m2
Stall speed
56 km/h
Landing speed
88 km/h
Maximum speed
1000 km/h
Minimum Sink
2.0 m/s at 70 km/h and 18.5 kg/m2 loading
Best Glide Ratio
9:1 at 97 km/h and 18.5 kg/m2 loading
Maximum Speed (horizontal)
500 km/h