I. Ae. 48 Data Table
Usage
Supersonic Fighter
Fuselage Construction
Metal
Wing Construction
Capacity
Two crew, tandem seating
Engine
2 Rolls-Royce A
Thrust
2 x 5,000 kg (2 x 11,000 lbs)
Span
9.0 m
Sweep Angle
65 degrees
Wing Root Thickness
3% chord
Wing Root Depth
10 m
Wing Area
50.0 m2
Aspect Ratio
1.62
Cockpit width
1.2 m
Cockpit height (from seat)
Empty weight
6000 kg
Ballast (weapons and ammunition)
600 kg
Additional payload
200 kg (Crew)
Fuel
11,000 kg
Maximum weight
16,800 kg
Wing loading
345-156 kg/m2
Thrust to weight
1.68 kg/daN
Landing speed
155 km/h
Maximum Speed
Mach 2.2