I. Ae. 37 Data Table


Usage

 

Test Vehicle

 

Fuselage Construction

Wood

 

Wing Construction

 

Wood

 

Capacity

 

Pilot

 

Span

 

10.0 m

 

Sweep Angle

 

63.4 degrees

 

Taper Ratio

 

infinite

Wing Root Thickness

 

10% chord

 

Wing Root Depth

 

10 m

 

Rib Spacing

 

0.40 m

 

Wing Area

 

48.0 m2

 

Aspect Ratio

 

2.1

 

Pilot position

 

First 50 flights prone,
then seated

Mid-section width

 

--- m

 

Cockpit width

 

1.0 m

 

Cockpit height (from seat)

 

0.8 (when seated, 1.1) m

 

Empty weight

 

11060 kg

 

Ballast (water)

 

---

 

Additional payload

 

100 kg

 

Maximum weight

 

1200 kg

 

Wing loading

 

25.0 kg/m2

 

Landing speed

 

72 km/h

 

Stall speed

 

72 km/h

 

Best Glide Ratio

 

10:1 at 149 km/h and 25 kg/m2 loading

Maximum Speed

 

250 km/h