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词条 Bagalini Bagaliante
释义

  1. Design and development

  2. Specifications (Bagaliante)

  3. See also

  4. References

  5. External links

name=Bagaliante image= caption=

}}{{Infobox Aircraft Type

type=Motor glider national origin=Italy manufacturer= designer=Marino Bagalini first flight= introduced= retired= status= primary user= more users= produced= number built= program cost= unit cost= US$250 (plans only, 1998) developed from= variants with their own articles=
}}

The Bagalini Bagaliante (a portmanteau of "Bagalini" and "Glider") is an Italian high-wing, strut-braced, single-seat, pusher configuration, conventional landing gear motor glider that was designed by Marino Bagalini and made available as plans for amateur construction.[1][2]

Design and development

The Bagaliante is constructed from wood and metal and is of pod-and-boom layout.[1]

The {{convert|12.2|m|ft|1|abbr=on}} span wing employs a Göttingen 535 airfoil at the wing root, transitioning to an NACA 4412 section at the wingtip. The wing uses a semi-tapered planform, tapering outboard of the mid-span point. The specified engine is a {{convert|19|kW|hp|0|abbr=on}} Rotax 277 two-stroke aircraft engine, mounted aft of the cockpit and driving a pusher propeller mounted above the tail boom. The fixed mainwheels are located beside the fuselage on small sponsons.[1][3]

Even with the small Rotax 277 fitted, the takeoff and landing distance is {{convert|46|m|ft|1|abbr=on}}[1]

The estimated time to build the aircraft from the plans is 700 hours.[1]

Specifications (Bagaliante)

{{Aircraft specs
|ref=Purdy[1]
|prime units?=met


|genhide=
|crew=one
|capacity=
|length m=
|length ft=21.00
|length in=
|length note=
|span m=12.2
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil= root: Gottingen 535, tip: NACA 4412
|empty weight kg=
|empty weight lb=242
|empty weight note=
|gross weight kg=
|gross weight lb=407
|gross weight note=
|fuel capacity={{convert|11|l|USgal}}
|more general=


|eng1 number=1
|eng1 name=Rotax 277
|eng1 type=
|eng1 kw=
|eng1 hp=26
|prop blade number=2
|prop name=wooden
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=
|max speed mph=54
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=37
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=26
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=900
|climb rate note=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|more performance=
|avionics=
}}

See also

{{aircontent
|see also=
  • List of gliders

|related=
|similar aircraft=
|lists=
}}

References

1. ^Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, page 304. BAI Communications. {{ISBN|0-9636409-4-1}}
2. ^{{Cite web|url = http://www.pilotmix.com/index.php?pgid=11&lang=en&maxInfo=356|title = Bagalini Bagaliante|accessdate = 8 September 2011|last = Pilot Mix|authorlink = |year = n.d.}}
3. ^{{Cite web|url = http://www.ae.illinois.edu/m-selig/ads/aircraft.html|title = The Incomplete Guide to Airfoil Usage |accessdate = 8 September 2011|last = Lednicer |first = David |authorlink = |year = 2010}}

External links

  • Photos of Bagalini Bagaliante
  • Photo of Bagalini Bagaliante
{{Bagalini aircraft}}

3 : Bagalini aircraft|Italian sailplanes 1980–1989|Homebuilt aircraft

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