I. Ae. 48 Data Table


Usage

 

Supersonic Fighter

Fuselage Construction

Metal

 

Wing Construction

 

Metal

 

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)

 

1.2 m

 

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