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词条 Moswey III
释义

  1. Design and development

  2. Operational history

  3. Specifications (Moswey III)

  4. See also

  5. References

name=Moswey III image= caption=

}}{{Infobox Aircraft Type

type=Glider national origin=Switzerland manufacturer=Moswey Segelflugzeug-Werke designer=Georg Mueller first flight= introduced=1938 retired= status= Production completed primary user= more users= produced= number built=more than 30 program cost= unit cost= developed from= variants with their own articles=
}}

The Moswey III is a Swiss mid-wing, single-seat, gull winged glider that was designed by Georg Mueller and produced by Moswey Segelflugzeug-Werke.[1][2]

Design and development

The Moswey series of gliders was developed prior to the Second World War in 1938. The third model was the first one to achieve full production status.[1]

The aircraft is built from wood. The fuselage is a monocoque design, while the wings and tail surfaces are a wooden frame covered in doped aircraft fabric covering. The fuselage is of a hexagonal section forward and a diamond section aft. The fuselage is built upon a main keel beam that also contains the control runs. The {{convert|14.0|m|ft|1|abbr=on}} span wing is a gulled design, employing a Goettingen 535 airfoil, with air brakes for glidepath control. The structure is stressed for aerobatics at +/-12g.[1][3]

The Moswey III was constructed by building the fuselage around a large tube, which was then removed after construction.[1]

The cockpit is noted for its small dimensions, with the wing roots providing the pilot's shoulder and elbow room.[1]

The Moswey III was not type certified and at least 30 were built.[1][2]

Operational history

One Moswey III was imported into the United States and remains on the Federal Aviation Administration aircraft registry in the Experimental - Racing/Exhibition category.[1][2]

Specifications (Moswey III)

{{Aircraft specs
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|prime units?=met


|genhide=
|crew=one
|capacity=
|length m=
|length ft=
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|length note=
|span m=14.0
|span ft=
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|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=136
|wing area note=
|aspect ratio=15.5
|airfoil=Goettingen 535
|empty weight kg=
|empty weight lb=304
|empty weight note=
|gross weight kg=
|gross weight lb=524
|gross weight note=
|more general=


|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=
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|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|g limits=+/-12
|roll rate=
|glide ratio= 27:1
|sink rate ms=
|sink rate ftmin=132
|sink rate note=
|lift to drag=
|wing loading kg/m2
|wing loading lb/sqft=3.85
|wing loading note=
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}}

See also

{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
  • List of gliders

}}

References

1. ^Said, Bob: 1983 Sailplane Directory, Soaring Magazine, page 93, Soaring Society of America November 1983. USPS 499-920
2. ^{{Cite web|url = http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=379HB|title = Make / Model Inquiry Results N379HB|accessdate = 19 July 2011|last = Federal Aviation Administration|authorlink = |date=July 2011}}
3. ^{{Cite web|url = http://www.ae.illinois.edu/m-selig/ads/aircraft.html|title = The Incomplete Guide to Airfoil Usage |accessdate = 1 July 2011|last = Lednicer |first = David |authorlink = |year = 2010}}

1 : Swiss sailplanes 1930–1939

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