I. Ae. 37 Data Table
Usage
Test Vehicle
Fuselage Construction
Wood
Wing Construction
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
Best Glide Ratio
10:1 at 149 km/h and 25 kg/m2 loading
Maximum Speed
250 km/h