| 词条 | Scheibe Spatz | |||||||||||||||
| 释义 |
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 in France under the name Avialsa A.60 Fauconnet, and 16 in Italy as the Meteor MS-30 L Passero; production 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, including easy recovery from a spin. Variants
Certified in 1952 with a 13.20 metre wingspan, 6.19 m length.
Strengthened and improved variant with a 13.20 metre wingspan, 6.19 m length, certified in 1952.
Certified in 1952 with a 13.20 metre wingspan, 6.25 m length.
Certified in 1954 with a 15.00 metre wingspan, 6.05 m length.
Certified in 1954 with a 15.00 metre wingspan, 6.25 m length.
Certified in 1966 with a 15.00 metre wingspan, 6.25 m length.
Licence production in France.
Licence production in Italy.
Electric aircraft version powered by an electric drive system, with a nose-mounted propeller.[1] Aircraft on display
Specifications (L-Spatz 55){{Aircraft specs|ref=The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde[3] |prime units?=met
|minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |minimum control speed note= |g limits=+4 -2 |roll rate= |glide ratio=29 at {{convert|80|km/h|mph kn|abbr=on|1}} |sink rate ms=0.58 |sink rate ftmin= |sink rate note=at {{convert|67|km/h|mph kn|abbr=on|1}} |lift to drag= |wing loading kg/m2=22.6 |wing loading lb/sqft= |wing loading note= |more performance= |avionics= }} See also{{aircontent|see also= |related= |similar aircraft=
|lists= }} Notes1. ^Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 166. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}} 2. ^{{cite web|url = http://www.soaringmuseum.org/collection.html|title = Sailplanes in Our Collection|accessdate = 28 July 2011|last = National Soaring Museum|authorlink = |year = 2011|deadurl = yes|archiveurl = https://web.archive.org/web/20110516142717/http://www.soaringmuseum.org/collection.html|archivedate = 16 May 2011|df = }} 3. ^{{cite book|last=Shenstone|first=B.S.|title=The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde|year=1958|publisher=Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue|location=Zurich|pages=68–72|edition=1st|author2=K.G. Wilkinson |language=English, French, German}} References{{refbegin}}
External links{{commons category|Scheibe Spatz}}
4 : German sailplanes 1950–1959|Glider aircraft|Scheibe aircraft|Homebuilt aircraft |
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