Ho IX Glider Data Table
Usage
Flight study
Fuselage Construction
Steel tubing
Wing Construction
Wood
Capacity
Pilot
Span
16.0 m
Sweep Angle
32.2 degrees
Taper Ratio
7.5
Wing Root Thickness
13% chord
Wing Root Depth
4.5 m
Rib Spacing
0.4 m
Wing Area
46.0 m2
Aspect Ratio
5.6
Pilot position
Seated
Mid-section width
2.4 m
Cockpit width
0.80 m
Cockpit height (from seat)
1.1 m
Empty weight
1900 kg
Ballast (water)
---
Additional payload
100 kg
Maximum weight
2000 kg
Wing loading
43.5 kg/m2
Stall speed
75 km/h
Landing speed
Maximum speed
1000 km/h