“Bagalini Colombo”的意思、由来-开放百科全书

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Bagalini Colombo

释义

Design and development
Specifications (Colombo)
References
External links

name=Colombo

image=

caption=

}}{{Infobox Aircraft Type

type=Homebuilt aircraft

national origin=United States

manufacturer=

designer=Marino Bagalini

first flight=

introduced=

retired=

status=Plans available (1998)

primary user=

more users=

produced=

number built=

program cost=

unit cost= US$220.00 (plans only, 1998)

developed from=

variants with their own articles=
}}

The Bagalini Colombo ({{lang-en|Dove}}) is an Italian homebuilt aircraft that was designed by Marino Bagalini. The aircraft is supplied in the form of plans for amateur construction.^[1]

Design and development

The Colombo features a strut-braced parasol wing, a two-seats in side-by-side configuration open cockpit with a windshield, fixed conventional landing gear, or optional tricycle landing gear, and a single engine in tractor configuration.^[1]

The aircraft is made from wood and metal, with its flying surfaces covered in doped aircraft fabric. Its {{convert|10.5|m|ft|1|abbr=on}} span wing employs an RSG 35 airfoil at the wing root, transitioning to an RSG 36 airfoil at the wing tip. The wing mounts Junkers ailerons and has a wing area of {{convert|16.723|m2|sqft|abbr=on}}. The standard engine used is the {{convert|40|hp|kW|0|abbr=on}} Rotax 447 two-stroke powerplant.^[1]^[2]

The Colombo has an empty weight of {{convert|150|kg|lb|abbr=on}} and a gross weight of {{convert|320|kg|lb|abbr=on}}, giving a useful load of {{convert|170|kg|lb|abbr=on}}. With full fuel of {{convert|23|l}} the payload is {{convert|151|kg|lb|abbr=on}}.^[1]

The manufacturer estimates construction time from the supplied kit to be 700 hours.^[1]

Specifications (Colombo)

{{Aircraft specs
|ref=AeroCrafter and The Incomplete Guide to Airfoil Usage^[1]^[2]
|prime units?=met

|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=21
|length in=0
|length note=
|span m=
|span ft=34.40
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=330
|empty weight note=
|gross weight kg=
|gross weight lb=700
|gross weight note=
|fuel capacity={{convert|23|l}}
|more general=

|perfhide=
|max speed kmh=
|max speed mph=62
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=41
|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=120
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=800
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=3.9
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^¹²³⁴⁵Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 126. BAI Communications, 15 July 1998. {{ISBN|0-9636409-4-1}}
2. ^¹{{Cite web|url = http://www.ae.illinois.edu/m-selig/ads/aircraft.html|title = The Incomplete Guide to Airfoil Usage |accessdate = 12 December 2013|last = Lednicer |first = David |year = 2010}}

External links

[https://archive.is/20131212180451/http://images2.jetphotos.net/img/4/1/5/9/16426_1314568951.jpg Photo of a Colombo]
Photo of a Colombo

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