“General Aviation Design Bureau T-2 Maverick”的意思、由来-开放百科全书

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General Aviation Design Bureau T-2 Maverick

释义

Design and development
Specifications (T-2 with Maverick II wing)
References

name=T-2 Maverick

image=

caption=

}}{{Infobox Aircraft Type

type=Ultralight trike

national origin=Ukraine

manufacturer=General Aviation Design Bureau of Ukraine

designer=

first flight=

introduced=1995

retired=

status=In production (2011)

primary user=

more users=

produced= 1995-present

number built=

program cost=

unit cost= €19,000 (2011)

developed from=

variants with their own articles=
}}

The General Aviation Design Bureau T-2 Maverick is a Ukrainian ultralight trike, designed and produced by the General Aviation Design Bureau of Ukraine, based in Kiev. The aircraft is supplied as a complete ready-to-fly-aircraft.^[1]

Design and development

The T-2 was produced starting in 1995 as a trainer for western markets under subcontract, but is now sold under the General Aviation Design Bureau's own name.^[1]

The T-2 Maverick was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of {{convert|450|kg|lb|0|abbr=on}}. The aircraft has a maximum gross weight of {{convert|450|to|540|kg|lb|0|abbr=on}} depending on the version. It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-side-by-side configuration open cockpit with two separate cockpit fairings, tricycle landing gear and a single engine in pusher configuration.^[1]

The aircraft's structure is made from tubing, with its double surface wing covered in Dacron sailcloth. Its {{convert|10.2|m|ft|1|abbr=on}} span wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar. Powerplants available are the twin cylinder, air-cooled, two-stroke, dual-ignition {{convert|50|hp|kW|0|abbr=on}} Rotax 503 engine, the liquid-cooled {{convert|64|hp|kW|0|abbr=on}} Rotax 582 engine or the four cylinder, air and liquid-cooled, four-stroke, dual-ignition {{convert|80|hp|kW|0|abbr=on}} Rotax 912UL engine.^[1]

The aircraft has an empty weight of {{convert|190|kg|lb|0|abbr=on}} and a gross weight of {{convert|450|to|540|kg|lb|0|abbr=on}} depending on the version, giving a useful load of {{convert|260|to|350|kg|lb|0|abbr=on}}. With full fuel of {{convert|30|l}} the payload is {{convert|238|to|328|kg|lb|0|abbr=on}}.^[1]

Two different wings have been supplied as standard, initially the Maverick 14.7 and, since 2000, the larger Maverick II with a wing area of {{convert|16.5|m2|sqft|abbr=on}}.^[1]

Specifications (T-2 with Maverick II wing)

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

|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=
|length in=
|length note=
|span m=10.2
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=16.5
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=190
|empty weight lb=
|empty weight note=
|gross weight kg=450
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|30|l}}
|more general=

|perfhide=
|max speed kmh=130
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=85
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=55
|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=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=4.0
|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=27.3
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^¹²³⁴⁵⁶Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 214. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

4 : Ukrainian sport aircraft 1990–1999|Ukrainian ultralight aircraft 1990–1999|Single-engined pusher aircraft|Ultralight trikes

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