Ho IX v-2 Data Table


Usage

 

Fighter

 

Fuselage Construction

Steel tubing

 

Wing Construction

 

Wood

 

Capacity

 

Pilot

 

Motor type

 

Two Junkers 004 jet turbine engines

Power

 

2 x 900 daN (2 x 2000 lbf)

Span

 

16.8 m

 

Sweep Angle

 

32.2 degrees

 

Taper Ratio

 

7.8

 

Wing Root Thickness

 

13% chord

 

Wing Root Depth

 

4.7 m

 

Rib Spacing

 

0.4 m

 

Wing Area

 

52.8 m2

 

Aspect Ratio

 

5.35

 

Pilot position

 

Seated

 

Mid-section width

 

3.2 m

 

Cockpit width

 

0.80 m

 

Cockpit height (from seat)

 

1.1 m

 

Empty weight

 

4844 kg

 

Ballast (water)

 

232 kg

 

Additional payload

 

100 kg

 

Fuel

 

1700 kg

 

Maximum weight

 

6876 kg

 

Wing loading

 

130 kg/m2

 

Engine loading

3.82 kg/daN

 

Stall speed

 

150 km/h

 

Landing speed

 

130 km/h

 

Cruise speed

 

900 km/h

 

Maximum speed (horizontal)

960 km/h

 

Maximum speed

 

1000 km/h