“Pro.Mecc Freccia Anemo”的意思、由来-开放百科全书

词条

Pro.Mecc Freccia Anemo

释义

Design and development
Variants
Specifications (Freccia Anemo)
References
External links

name=Freccia Anemo

image=

caption=

}}{{Infobox Aircraft Type

type=Ultralight aircraft

national origin=Italy

manufacturer=Pro.Mecc

designer=

first flight=

introduced=2011

retired=

status=In production (2012)

primary user=

more users=

produced=

number built=

program cost=

unit cost= €77,500 (2015)

developed from= Pro.Mecc Sparviero

variants with their own articles=
}}

The Pro.Mecc Freccia Anemo ({{lang-en|Fast Arrow}}) is an Italian ultralight aircraft, designed and produced by Pro.Mecc of Corigliano d'Otranto. The aircraft was introduced at the AERO Friedrichshafen show in 2011. The Freccia is supplied as a complete ready-to-fly-aircraft.^[1]^[2]

Design and development

The Freccia was derived from the earlier Pro.Mecc Sparviero, with additional streamlining and a new elliptical wing planform. It was designed to conform to the Fédération Aéronautique Internationale microlight rules. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed or, optionally, retractable tricycle landing gear and a single engine in tractor configuration.^[1]^[2]

The aircraft is made from carbon fibre. Its {{convert|8.78|m|ft|1|abbr=on}} span wing has an area of {{convert|10.18|m2|sqft|abbr=on}} and double slotted flaps to allow a low stall speed. Engines available are the {{convert|100|hp|kW|0|abbr=on}} Rotax 912ULS, the turbocharged {{convert|115|hp|kW|0|abbr=on}} Rotax 914 and the {{convert|130|hp|kW|0|abbr=on}} ULPower UL350iS four-stroke powerplant.^[1]^[2]

Variants

Freccia

Fixed landing gear model, introduced in 2011^[1]^[2]

Freccia-RG

Retractable landing gear model, introduced in 2012^[1]^[2]

Specifications (Freccia Anemo)

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

|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=
|length in=
|length note=
|span m=8.78
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=10.18
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=285
|empty weight lb=
|empty weight note=
|gross weight kg=472.5
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|110|l}}
|more general=

|perfhide=
|max speed kmh=280
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=260
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=65
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=300
|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=8
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=46.4
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^¹²³⁴⁵Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 71. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
2. ^¹²³⁴Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 74. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}

External links

{{Official website|http://www.promecc.com/}}

2 : Italian ultralight aircraft 2010–2019|Single-engined tractor aircraft

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