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词条 Adamoli-Cattani fighter
释义

  1. Design and development

  2. Operational history

  3. Specifications (estimated performance with 200hp engine)

  4. See also

  5. References

name = Adamoli-Cattani fighter image = caption = alt =

}}{{Infobox aircraft type

type = Fighternational origin = Italymanufacturer = Farina and Officine Moncenisiodesign group = designer = Signori Adamoli & Cattani[1]first flight = 1918introduced = retired = status = primary user = more users = produced = number built = 1[1]program cost = unit cost = developed from = variants with their own articles = developed into =
}}

The Adamoli-Cattani fighter was a prototype fighter aircraft designed as a private venture by two Italian aircraft builders in 1918.

Design and development

The Adamoli-Cattani was intended to be the smallest practical biplane around the most powerful engine available to them, a {{convert|149|kW|hp|abbr=on}} le Rhône M. The result was a reasonably conventional design, other than that the wings featured hinged leading edges in place of conventional ailerons. The Farina Coach Building factory in Turin began construction of the prototype; the Officine Moncenisio in Condove completed it.[1]

Operational history

Upon completion, ground testing revealed that the engine as installed could only deliver some 80% of its rated power, thus leaving the aircraft significantly underpowered. Limited tests continued until the end of World War I, when the Armistice made further development superfluous.[1]

Specifications (estimated performance with 200hp engine)

{{Aircraft specs
|ref=The Complete Book of Fighters[1]
|prime units?=met


|genhide=
|crew=1
|capacity=
|length m=6.10
|length ft=
|length in=
|length note=
|span m=8.60
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=
|wing area note
|volume note=
|aspect ratio=
|airfoil=
|empty weight kg=470
|empty weight lb=
|empty weight note=
|gross weight kg=675
|gross weight lb=
|gross weight note=
|fuel capacity=


|eng1 number=1
|eng1 name=le Rhône M
|eng1 type=9-cyl. air-cooled rotary piston engine
|eng1 kw=
|eng1 hp=200
|eng1 note=(rating) - actual power 119 kW (160 hp)
|power original=
|thrust original=


|perfhide=
|max speed kmh=186
|max speed mph=
|max speed kts=
|max speed note=
|max speed mach=
|range km=
|range miles=
|range nmi=
|endurance=2.25
|ceiling m=
|ceiling ft=
|ceiling note=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|more performance=


|guns= 2 x .303-in (7.7-mm) machine guns
|avionics=
}}

See also

Comparable aircraft:
  • Nieuport-Delage Ni-D 29

References

1. ^1 2 3 4 {{cite book |last=Green |first=William |title=The Complete Book of Fighters |year=1997 |publisher=Salamander Books Limited |location=London |page=8|isbn=1-85833-777-1 |author2=Gordon Swanborough}}
{{DEFAULTSORT:Adamoli-Cattani Fighter}}

4 : Single-engined tractor aircraft|Italian fighter aircraft 1910–1919|Military aircraft of World War I|Rotary-engined aircraft
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