ASK 21 Mi


 Technical Data
Design Description 3-View Drawing Speed Polar Download

 

 

Span

17 m

Wing Area

17,95 m²

Wing aspect ratio

16,1

Fuselage length

8,35 m

Cockpit width

0,68 m

Cockpit height, front

0,90 m

Cockpit height, rear

0,90 m

Height at tailplane

1,55 m

Empty mass

ca. 495 kg

Max take-off mass

700 kg

Wing loading (90 kg payload)

32,6 kg/m²

Wing loading (max.)

39,0 kg/m²

Wing loading (without engine, 85 kg payload)

28,5 kg/m²

Max. payload in Cockpit

205 kg

Maximum speed

280 km/h

Minimum sink (single-seated)

0,65 m/s

Glide ratio (@ 90 km/h)

34

 

 

Engine Power

56 PS (41 kW)

Engine displacement

294 cm³

Volume of tank

26 liter

 

 

Take off distance on grass (max. take-off mass)

ca. 250 m

Climb rate (single seated)

ca. 2,9 m/s

Climb rate (double seated)

ca. 2,7 m/s

Cruising speed

140 km/h

Fuel consumption in full climb

ca. 19 l/h

Fuel consumption in cruise

ca. 14 l/h

Range (using saw-tooth method)

ca. 500 km

 

 


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