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Schleicher ASW 24

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Wingspan
  
15 m

Introduced
  
1987

Designer
  
Length
  
6.55 m

Retired
  
2000

Schleicher ASW 24 Schleicher ASW24 Photos AirplanePicturesnet

Manufacturer
  
Alexander Schleicher GmbH & Co

The ASW 24 is a modern single seat high performance composite Standard Class sailplane.

Contents

History

Schleicher ASW 24 Schleicher ASW24 Photos AirplanePicturesnet

The ASW 24 was designed by Schleicher's Gerhard Waibel, with Delft University professor Loek Boermans undertaking the role of aerodynamicist. The prototype made its first flight in 1987, having entered serial production later the same year. It nominally remained in production until 2000, although only a score were built in the mid-to-late 1990s.

Schleicher ASW 24 ASW 24

It entailed a large development effort, as it was a complete departure from the preceding ASW 19 and pioneered several successful innovations. The fuselage, airfoils, wings and empennage were completely new, as well as many systems, e.g. the electrical ballast management. The structure employed a large amount of the then still exotic carbon fibre. The OSTIV Award-winning safety cockpit made use of an organic shape, tall sidewalls, crumple zones and exotic aramid fibres for crash protection. A large wheel with a disc brake and a large canopy with excellent visibility were other strong points of the type.

Schleicher ASW 24 Schleicher ASW24 Untitled Aviation Photo 2223658 Airlinersnet

The ASW 24 was moderately successful in competitions. It won a single World Championship in 2001, fourteen years after its market launch. As the contemporary LS7, the ASW 24 overstretched the technology available at the time: it has excellent performance in the cruise but less so in the slow flight range. The higher-than-usual thermalling speed revealed itself a disadvantage in the typical competition gaggles, and its performance degrades somewhat when subject to turbulence, rain or wing contamination. However, the addition of winglets and a change to the outer wing leading edge, making it slightly blunter, improved these characteristics significantly.

Schleicher ASW 24 Schleicher ASW24 The University of Tokyo Soaring Club Aviation

According to World Champion Sarah Steinberg, it needs to be always proactively flown in thermals, thus imposing a higher workload upon the pilot. Notwithstanding, the aesthetically pleasing ASW 24 is a comfortable, safe and pleasant sailplane with high cross-country performance that remains competitive up to national championship level in most countries.

Schleicher ASW 24 saleplane Schleicher ASW24 pilots aviation flying pilotspaceeu

The fuselage of the ASW 24 was the basis, with small modifications, for the subsequent ASW 27, ASW 28 and ASG 29. It was superseded in production by the ASW 28.

Variants

Schleicher ASW 24 httpsuploadwikimediaorgwikipediacommonsthu

  • The ASW 24B of 1993 introduced winglets and a slightly revised airfoil that were partially successful in addressing the handling and performance issues.
  • The ASW 24E is a nominally self-launching variant employing a Rotax 275 engine and a propeller mounted on a retractable pylon. The engine installation is peculiar for its small size and power, more typical of a turbo, and for its manual start with a pilot-operated ripcord.
  • Specifications (ASW 24)

    Data from Jane's All the World's Aircraft 1988-89

    General characteristics

  • Crew: 1
  • Length: 6.55 m (21 ft 6 in)
  • Wingspan: 15 m (49 ft 3 in)
  • Height: 1.3 m (4 ft 3 in)
  • Wing area: 10 m2 (110 sq ft)
  • Aspect ratio: 22.5
  • Airfoil: DU 84-158
  • Empty weight: 230 kg (507 lb) ,ASW 24E 275 kg (606 lb))
  • Max takeoff weight: 500 kg (1,102 lb)
  • Water ballast: 155 kg (342 lb)ASW 24B 160 kg (353 lb)
  • Cockpit width: 0.64 m (2.10 ft)
  • Cockpit height: 0.81 m (2.66 ft)
  • ASW 24E

  • Powerplant: 1 × Rotax 275 1 cylinder 2-stroke retractable piston engine, 19 kW (25 hp)
  • Propellers: 2-bladed fixed pitch propeller
  • Performance

  • Stall speed: 69 km/h (43 mph; 37 kn)
  • Never exceed speed: 270 km/h (168 mph; 146 kn) in smooth air205 km/h (111 kn; 127 mph) in rough air205 km/h (111 kn; 127 mph) on aero-tow140 km/h (76 kn; 87 mph) on winch launch
  • g limits: +5.3 -2.65
  • Maximum glide ratio: 43.5 at 105 km/h (57 kn; 65 mph)ASW 24B 44 at 105 km/h (57 kn; 65 mph)
  • Rate of sink: 0.57 m/s (112 ft/min) at 70 km/h (38 kn; 43 mph) at 31 kg/m2 (6.3 lb/sq ft)
  • Wing loading: 50 kg/m2 (10 lb/sq ft)
  • Min loading: 30.5 kg/m2 (6.2 lb/sq ft)
  • References

    Schleicher ASW 24 Wikipedia