Aviasouz Cruise
{{Short description|Russian ultralight trike}}
{{Use dmy dates|date=January 2022}}
{{Use American English|date=January 2022}}
| {{Infobox aircraft begin
| name=Cruise | image= | caption= }}{{Infobox aircraft type | type=Ultralight trike | national origin=Russia | manufacturer=Aviasouz | designer= | first flight= | introduced= | retired= | status=In production (2013) | primary user= | more users= | produced= | number built= | developed from= | variants with their own articles= }} |
The Aviasouz Cruise is a Russian ultralight trike, designed and produced by Aviasouz of Kazan. The aircraft is supplied as a complete ready-to-fly-aircraft.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 205. WDLA UK, Lancaster UK, 2011. ISSN 1368-485XBertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 96. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
The company was formed by former employees of the Tupolev Design Bureau.
Design and development
The aircraft 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|430|kg|lb|0|abbr=on}}. It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-side-by-side configuration open cockpit with a unique fibreglass cockpit fairing, tricycle landing gear with wheel pants and a single engine in pusher configuration.
The aircraft is made from bolted-together aluminum tubing, with its single surface wing covered in Dacron sailcloth. Its {{convert|10|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 powerplant is a twin cylinder, air-cooled, two-stroke, dual-ignition {{convert|64|hp|kW|0|abbr=on}} Rotax 582 engine, with the four cylinder, air and liquid-cooled, four-stroke, dual-ignition {{convert|80|hp|kW|0|abbr=on}} Rotax 912 engine optional. The aircraft has an empty weight of {{convert|180|kg|lb|0|abbr=on}} and a gross weight of {{convert|430|kg|lb|0|abbr=on}}, giving a useful load of {{convert|250|kg|lb|0|abbr=on}}. With full fuel of {{convert|50|L}} the payload is {{convert|214|kg|lb|0|abbr=on}}.
Specifications (Cruise)
{{Aircraft specs
|prime units?=met
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|crew=one
|capacity=one passenger
|length m=
|length ft=
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|span m=10
|span ft=
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|wing area sqm=14
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|empty weight kg=180
|empty weight lb=
|empty weight note=
|gross weight kg=430
|gross weight lb=
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|fuel capacity={{convert|50|L}}
|more general=
|eng1 number=1
|eng1 name=Rotax 582
|eng1 type=twin cylinder, liquid-cooled, two stroke aircraft engine
|eng1 kw=48
|eng1 hp=
|prop blade number=3
|prop name=composite
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|max speed kmh=125
|max speed mph=
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|cruise speed kmh=90
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|stall speed kmh=55
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|climb rate ms=4
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|wing loading kg/m2=30.7
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}}
References
{{reflist}}
External links
- {{Official website|https://web.archive.org/web/20130530075413/http://delta-avia.ru/}}
Category:2000s Russian sport aircraft
Category:2000s Russian ultralight aircraft