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

 

75 km/h

 

Maximum speed

 

1000 km/h