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Schleicher ASW 24

sch-asw24


The ASW-24, which first flew in 1987, is the Standard Class successor to the Schleicher ASW-19. Approach control is effected by top surface Schempp-Hirth type airbrakes.

Designer Waibel won the 1992 OSTIV Award for significant contributions to safety for the ASW-24 design.

The ASW-24E is the self-launching version.

ASW-24
Wing span: 15m / 49.2ft
Wing area: 10sq.m / 107.6sq.ft
Empty Weight: 230kg / 507lb
Payload: 270kg / 595lb
Gross Weight: 500kg / 1102lb
L/DMax: 44 105 kph / 57 kt / 65 mph
MinSink: 0.58 m/s / 1.90 fps / 1.13 kt
Wing Load: 50kg/sq.m / 10.24lb/sq.ft
Water Ballast: 170kg / 375lb
Aspect ratio: 22.5
Airfoil: Boermans DU 84-158
Seats: 1

ASW-24E
Engine: 19kW/ 25bhp Rotax 275
Wing span: 15m / 49.2ft
Wing area: 10sq.m / 107.6sq.ft
Empty Weight: 230kg / 507lb
Payload: 270kg / 595lb
Gross Weight: 500kg / 1102lb
L/DMax: 44 105 kph / 57 kt / 65mph
MinSink: 0.58 m/s / 1.90 fps / 1.13kt
Wing Load: 50kg/sq.m / 10.24lb/sq.ft
Water Ballast: 170kg / 375lb
Aspect ratio: 22.5
Airfoil: Boermans DU 84-158
Seats: 1

 

 


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