Schleicher ASW 12

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Schleicher ASW 12
This ASW-12 (SN 12013) is owned by the National Soaring Museum in Elmira, NY and is pictured here on display at the Virginia Air & Space Center in Hampton, VA.
Type designation ASW 12
Competition class Open
Production run 1966-1970
Number built 14
Crew 1
Length 7.35
Height 1.50
Wingspan 18.30 m
Wing area 13.0 m²
Aspect ratio 25.8
Wing profile: Wortmann FX 62-K-131 modified and FX 60-126
Empty mass 324 kg
Water ballast -
Maximum mass 430 kg
Maximum wing loading 31.5 kg/m²
Maximum speed 200 km/h
Stall speed 68 km/h
Minimum sink rate ca. 0.57 m/s
Best glide ratio ca. 46

The ASW-12 is a single-seat Sailplane of glass composite construction. The wing is shoulder mounted and it has a T-tail. It is essentially a developed production version of the Akaflieg Darmstadt D-36.

[edit] History

In 1965 Gerhard Waibel left the Technical University of Darmstadt to enter Alexander Schleicher GmbH & Co as a designer. His first project for his new employer was the ASW-12. This sailplane achieved numerous records and victories in national and international competitions. The exploits of Hans-Werner Grosse in an ASW-12 are legendary, e.g. the 1461 km flight of April 25, 1972 from Lübeck to Biarritz which stood for thirty years as the absolute World Free Distance Record.

[edit] Construction

The fuselage of the ASW-12 was extremely slender for its time. It has a retractable landing gear and a two-piece canopy, of greater depth than was the case with the D-36. Each individual fuselage was manufactured - as with the D-36 - in two halves laid-up on positive molds. The construction material was a double sandwich of glass-fibre reinforced composite over balsa wood. This is an unusual and expensive procedure for serial production.

The wing planform is double-tapered. The profile is a modified Wortmann FX 62-K-131 at the wing root and a Wortmann FX 60-126 at the tip. The wings were built in the usual fashion in negative molds, and are also of fiberglass/balsa wood sandwich construction. Water ballasting is not available.

As landing aid the ASW-12 possesses only a parachute brake, an unreliable system that lacks modulation. A number of ASW-12 were retroffited with a second chute to increase the odds of successful landings.

[edit] Sources

Sailplane Directory

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