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