TL-Ultralight Stream
{{Short description|Czech ultralight aircraft}}
{{Use dmy dates|date=December 2022}}
{{Use British English|date=December 2022}}
| {{Infobox Aircraft Begin
| name= Stream | image=TL-Ultralight Stream at AERO Friedrichshafen 2018 (1X7A4327).jpg | caption=TL-Ultralight Stream at AERO Friedrichshafen 2018 }}{{Infobox Aircraft Type | type=Ultralight aircraft | national origin=Czech Republic | manufacturer=TL-Ultralight | designer= | first flight= | introduced=2013 | retired= | status=In production (2017) | primary user= | more users= | produced= | number built= | developed from= | variants with their own articles= }} |
The TL-Ultralight Stream is a Czech ultralight aircraft, designed and produced by TL-Ultralight of Hradec Králové, introduced at the AERO Friedrichshafen show in 2013.Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 84. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}
Design and development
The Stream is the company's fastest design to date. It was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever low-wing, an enclosed cockpit with two-seats-in-tandem under a bubble canopy, retractable tricycle landing gear and a single engine in tractor configuration.
The aircraft is made from composite materials. Its {{convert|9.0|m|ft|1|abbr=on}} span wing mounts flaps. Standard engines available are the {{convert|100|hp|kW|0|abbr=on}} Rotax 912ULS and 912iS, and the turbocharged {{convert|115|hp|kW|0|abbr=on}} Rotax 914 four-stroke powerplants, driving a three-bladed PowerMax propeller.{{cite web|url = http://www.tl-ultralight.cz/en/ultralight-aircraft/stream|title = TL-Ultralight Stream|accessdate = 22 March 2017|author=TL-Ultralight |work =tl-ultralight.cz |year=2017}}
Operational history
Specifications (Stream)
{{Aircraft specs
|prime units?=met
|genhide=
|crew=one
|capacity=one passenger
|length m=6.785
|length ft=
|length in=
|length note=
|span m=9.00
|span ft=
|span in=
|span note=
|height m=2.475
|height ft=
|height in=
|height note=
|wing area sqm=9.962
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=297
|empty weight lb=
|empty weight note=
|gross weight kg=472.5
|gross weight lb=
|gross weight note=
|fuel capacity=90
|more general=
|eng1 number=1
|eng1 name=Rotax 912ULS
|eng1 type=four cylinder, liquid and air-cooled, four stroke aircraft engine
|eng1 kw=75
|eng1 hp=
|prop blade number=3
|prop name=PowerMax
|prop dia m=
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|perfhide=
|max speed kmh=325
|max speed mph=
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|stall speed kmh=65
|stall speed mph=
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|never exceed speed kmh=335
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=1400
|range miles=
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|climb rate ms=6
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}}
References
{{reflist}}
External links
{{Commons category}}
- {{Official website|http://www.tl-ultralight.cz/en/ultralight-aircraft/stream}}
{{TL Ultralight aircraft}}
Category:TL Ultralight aircraft