“General Aviation Design Bureau T-32 Maverick”的意思、由来-开放百科全书

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General Aviation Design Bureau T-32 Maverick

释义

Design and development
Specifications (T-32 Maverick)
References

name=T-32 Maverick

image=

caption=

}}{{Infobox Aircraft Type

type=Ultralight trike

national origin=Ukraine

manufacturer=General Aviation Design Bureau of Ukraine

designer=

first flight=

introduced=

retired=

status=Under development (2011)

primary user=

more users=

produced=

number built=at least one

program cost=

unit cost= €24,000 (projected, 2011)

developed from=

variants with their own articles=
}}

The General Aviation Design Bureau T-32 Maverick is a Ukrainian ultralight trike under development by the General Aviation Design Bureau of Ukraine, based in Kiev. The aircraft is intended to be supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.^[1]

The company has constructed trike designs for other manufacturers under contract in the past, but the T-32 is their own design.^[1]

Design and development

As a three-seat trike the T-32 Maverick does not comply with the Fédération Aéronautique Internationale microlight or the US light-sport aircraft categories, which are both limited to two seats, but may fit some country's amateur-built aircraft rules.^[1]

The T-32 Maverick features a cable-braced hang glider-style high-wing, weight-shift controls, a three-seat open cockpit, with the pilot sitting in front and a two-seat bench in the back, with a cockpit fairing. It can be mounted on tricycle landing gear or floats and has a single engine in pusher configuration.^[1]

The aircraft is made from bolted-together aluminum 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. The aircraft has many powerplant options, including the twin cylinder, liquid-cooled, two-stroke, dual-ignition {{convert|64|hp|kW|0|abbr=on}} Rotax 582 engine, the four cylinder, air and liquid-cooled, four-stroke, dual-ignition {{convert|80|hp|kW|0|abbr=on}} Rotax 912UL or {{convert|100|hp|kW|0|abbr=on}} Rotax 912ULS engine and the turbocharged {{convert|115|hp|kW|0|abbr=on}} Rotax 914. Automotive conversion engines of {{convert|60|to|110|hp|kW|0|abbr=on}} can also be fitted.^[1]

The aircraft has an empty weight of {{convert|280|kg|lb|0|abbr=on}} and a gross weight of {{convert|640|kg|lb|0|abbr=on}}, giving a useful load of {{convert|360|kg|lb|0|abbr=on}}. With full fuel of {{convert|60|l}} the payload is {{convert|316|kg|lb|0|abbr=on}}.^[1]

Specifications (T-32 Maverick)

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

|genhide=
|crew=one
|capacity=two passengers on a bench seat
|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=280
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|60|l}}
|more general=

|perfhide=
|max speed kmh=140
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=100
|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=3
|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=38.8
|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 213. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

3 : Ukrainian sport aircraft 2010–2019|Single-engined pusher aircraft|Ultralight trikes

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