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    Glasflugel / H-301 Schuemann Libelle

    Glider Reg. Number: N25KD

    1967


    Design & Development

    The Glasflügel H-301 Libelle is an early composite 15-metre Class single-seat sailplane produced by Glasflügel from 1964 to 1969.

    Glasflugel Libelle H-301

    In 1964 the H-301 Libelle ("Dragonfly") received the first German and first U.S. Type Certificate issued to an all-fiberglass aircraft. It had flaps, water ballast and retractable landing gear.

    There are two canopy variants: the normal canopy and a sleeker, lower-profiled 'racing' canopy with no side vent. The canopy is unique in that it has a catch that enables the front to be raised by 25 mm (1 in) in flight to provide a flow of ventilating air instead of the more conventional small sliding panel used for this purpose.

    The American Wil Schuemann pioneered several performance-enhancing modifications to the type, including a re-profiled wing, converting the airfoil to a Wortmann section, various fairings, a new canopy and a reshaped fuselage nose. Aircraft incorporating these changes are informally known as 'Schümanised' Libelles.

    The H-201 Standard Libelle was developed in 1967 as a Standard Class variant.

    The Libelle was a popular and influential design. Its light wings and easy rigging set a new benchmark. Handling is generally easy except that it is sensitive to sideslipping and has relatively ineffective airbrakes that make short landings tricky for inexperienced pilots.

    The H-201 Libelle (standard class) was superseded by the Hornet.

    The H-301 Libelle (open class) was superseded by the Mosquito.


    Specifications

    General characteristics

    • Crew: 1
    • Capacity: 50 kg (110 lb) water ballast
    • Length: 6.19 m (20 ft 4 in)
    • Wingspan: 15.00 m (49 ft 3 in)
    • Height: 1.25 m (4 ft 1 in)
    • Wing area: 9.5 m2 (102 ft2)
    • Aspect ratio: 23.6
    • Empty weight: 180 kg (400 lb)
    • Gross weight: 300 kg (660 lb)

    Performance

    • Maximum speed: 200 km/h (124 mph)
    • Maximum glide ratio: ca. 39
    • Rate of sink: 0.55 m/s (108 ft/min)
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