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