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词条 Rotondi R-1 Gheppio
释义

  1. Development

  2. Operational history

  3. Specifications

  4. References

name =R-1 Gheppio image = caption =

}}{{Infobox Aircraft Type

type=Single seat glidernational origin=Italydesigner =Gianfranco Rotondifirst flight =1952status =Sole example destroyednumber built =1
}}

The Rotondi R-1 Gheppio ({{lang-en|Kestrel}}) was a lightweight, single seat Italian glider. It featured a relatively short wingspan (ten meters). One example was built in the early 1950s.

Development

The Ghoppia was a cantilever mid-wing monoplane. Its straight tapered wing was built in one piece for lightness around a single spar and had marked dihedral. The outer half of the wing's trailing edge carried ailerons mounted on a false spar; trailing edge airbrakes occupied the inner portion of the wingspan. These airbrakes turned out to be rather ineffective. The wing terminated in small tip bodies.[2]

The fuselage was built in two sections that bolted together. It was ovoid in cross-section, tapering aft to a conventional but integral tail. The fin was straight edged with a rounded tip and a small fillet at its base. Its rudder extended down to the keel. The tailplane was mounted on the fin near the top of the fillet, carrying elevators that had a large cut-out for rudder movement. The Ghoppia's cockpit was over the wing, under a rather prominent canopy which opened by sliding rearwards. This had perspex transparencies forwards and to the sides but was opaque rearwards and above. A skid, reaching aft to about mid-chord, and a tail bumper formed the undercarriage.[2]

Partly due to the single-piece wing, the Ghoppia was unusually light with an empty weight of only {{convert|80|kg|lb|abbr=on|0}}.

Operational history

The Ghoppia was first flown from Bresso, then later from Linate, sometimes launched by aerotow. The sole example was lost in an out-landing accident during a competition organised by the aeroclub of Milan.[2]

Specifications

{{Aircraft specs
|ref=Pedrielli (2011) p. 221
|prime units?=met
|capacity=One
|length m=5.50
|span m=10.0
|height m=
|height ft=
|height in=
|wing area sqm=8.0
|aspect ratio=12.5
|airfoil=
|empty weight kg=80
|gross weight kg=160
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|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=
|glide ratio=estimated, 23:1
|sink rate ms=
|sink rate ftmin=
|lift to drag=
|wing loading kg/m2=20.0
|wing loading note=
}}

References

1. ^{{cite web|url=http://www.scalesoaring.co.uk/VINTAGE/Documentation/Gheppio/R1_Gheppio.pdf|title=R1 Gheppio|accessdate=4 November 2013}}
[1]
}}

1 : Italian sailplanes 1950–1959

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