Scheibe Spatz
The Scheibe Spatz (German: "Sparrow") is a German glider with a mixed metal and wood construction that was built in 1952 until 1962. Later versions were known as the L-Spatz, the letter L standing for Leistung, which is German for "performance".
Scheibe Flugzeugbau built the Spatz A in 1952. Two years later in 1954 the first L-Spatz 55 was airborne. Three hundred L-Spatz 55s were built in Germany, 155 were produced in France under the name A.60 Fauconnet, and 16 produced under in Italy named MS-30 L Passero. This model was discontinued in 1962.
It is a single-seater cantilever shoulder-winged sailplane with a cruising (max L/D) speed of 45 mph. It has an empty weight of 157 kg and a maximum take-off weight of 269 kg. The single spar wing and tail were constructed using fabric-covered wood, whereas the fuselage consisted of steel tubing covered with fabric.
The L-Spatz 55 has good climbing performance due to light construction. The glide angle is 29:1. The longest known cross-country flight was more than 600 km from Burg Feuerstein, Germany to France.
Many gliding clubs operated the L-Spatz 55, well known for its easy handling. Recovery from a spin in the L-Spatz 55 is easy.
Variants
- Spatz A
- Certified in 1952 with a 13.20 metre wingspan, 6.19 m length.
- Spatz B
- Strengthened and improved variant with a 13.20 metre wingspan, 6.19 m length, certified in 1952.
- Spatz 55
- Certified in 1952 with a 13.20 metre wingspan, 6.25 m length.
- L-Spatz
- Certified in 1954 with a 15.00 metre wingspan, 6.05 m length.
- L-Spatz 55
- Certified in 1954 with a 15.00 metre wingspan, 6.25 m length.
- L-Spatz III
- Certified in 1966 with a 15.00 metre wingspan, 6.25 m length.
- Avialsa 60 Fauconnet
- Licence production in France.
- Meteor MS-30 L-Passero
- Licence production in Italy.
Aircraft on display
Specifications (L-Spatz 55)
Data from The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde[2]
General characteristics
- Crew: 1
- Length: 6.25 m (20 ft 6 in)
- Wingspan: 15 m (49 ft 3 in)
- Wing area: 11.7 m2 (126 sq ft)
- Aspect ratio: 19
- Airfoil: Mü-Profil 14%
- Empty weight: 153 kg (337 lb)
- Max takeoff weight: 265 kg (584 lb)
Performance
- Never exceed speed: 180 km/h (112 mph; 97 kn)
- Rough air speed max: 110 km/h (68.4 mph; 59.4 kn)
- Aerotow speed: 110 km/h (68.4 mph; 59.4 kn)
- Winch launch max speed: 90 km/h (55.9 mph; 48.6 kn)
- Terminal velocity: 200 km/h (124.3 mph; 108.0 kn)
- g limits: +4 -2
- Maximum glide ratio: 29 at 80 km/h (49.7 mph; 43.2 kn)
- Rate of sink: 0.58 m/s (114 ft/min) at 67 km/h (41.6 mph; 36.2 kn)
- Wing loading: 22.6 kg/m2 (4.6 lb/sq ft)
See also
- Aircraft of comparable role, configuration and era
Schleicher Ka8
Notes
- ↑ National Soaring Museum (2011). "Sailplanes in Our Collection". Retrieved 28 July 2011.
- ↑ Shenstone, B.S.; K.G. Wilkinson (1958). The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde (in Primarily English with French and German) (1st ed.). Zurich: Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue. pp. 68–72.
References
- Shenstone, B.S.; K.G. Wilkinson (1958). The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde (in Primarily English with French and German) (1st ed.). Zurich: Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue. pp. 68–72.
External links
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