ASW 28-18 / ASW 28-18 E


 Technical Data
Design Description 3-View Drawing Speed Polar Download

 

       

Wingspan (incl. winglets)

15 m

49.2 ft

18 m

59 ft

Wing area

10.5 m²

113 sqft

11.88 m²

128 sqft

Aspect ratio

21.43

27.27

Height of winglet

0.5 m

1.64 ft

0.5 m

1.64 ft

Span of tailplane

2.85 m

9.35 ft

Length of fuselage

6.585 m

21.6 ft

Cockpit width

0.64 m

2.09 ft

Cockpit hight

0.80 m

2.62 ft

Height at tailplane

1.3 m

4.26 ft

Empty mass

258 kg

569 lbs

270 kg

595 lbs

Max. take off weight

525 kg

1157 lbs

575 kg

1267 lbs

Max. wing loading

50 kg/m²

10.24 lbs/sqft

48.4 kg/m²

9.91 lbs/sqft

Min. wing loading

32 kg/m²

6.55 lbs/sqft

29 kg/m²

5.93 lbs/sqft

Waterballast, max.

190 l

418 lbs

190 l

418 lbs

Useful load, max.

159 kg

350 lbs

159 kg

350 lbs

Max. pilot weight

115 kg

253 lbs

115 kg

253 lbs

Max rough air speed

200 km/h

108 kts

200 km/h

108 kts

Vne

270 km/h

145 kts

270 km/h

145 kts

 

       

for m=343 kg:

for m=355 kg:

Min. speed

72 km/h

39 kts

71 km/h

38 kts

Min.sink

0.56 m/s

110 ft/min

0.48 m/s

94 ft/min

Best L/D (calculated)

45

(@ 100 km/h)

48

(@ 90 km/h)

 

       

ENGINE:

       

Type

SOLO 2350

2-stroke

Engine power (@ 4200 U/min)

18 hp

13.5 kW

Engine displacement

430 cm³

 

       

PROPELLER:

       

Manufacturer

AS

Diameter

1.2 m

3.93 ft

Blades

2

 

       

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