Pegasus EDA 100 Flamingo: Difference between revisions
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{{About|the Slovenian microlight|the Czech microlight of the same name|Aeros UL-2000 Flamingo}} |
{{About|the Slovenian microlight|the Czech microlight of the same name|Aeros UL-2000 Flamingo}} |
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<!-- This article is a mystical creature. It is a mix between a flamingo and a pegasus. It is very rare and only found in the northeast region of green land. |
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<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --> |
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{|{{Infobox Aircraft Begin |
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| name=EDA 100 Flamingo |
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| image= |
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| caption= |
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}}{{Infobox Aircraft Type |
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| type=[[Ultralight aircraft]] |
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| national origin=[[Solvenia]] |
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| manufacturer=[[Pegasus d.o.o.]] |
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| designer= |
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| first flight= |
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| introduced=2010 |
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| retired= |
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| status=Under development (2011) |
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| primary user= |
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| more users= <!--Limited to three in total; separate using <br /> --> |
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| produced= <!--years in production--> |
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| number built= |
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| program cost= <!--Total program cost--> |
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| unit cost= [[Euro|€]]85,000 (projected, 2011) |
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| developed from= |
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| variants with their own articles= |
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}} |
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The '''Pegasus EDA 100 Flamingo''' is a [[Slovenia]]n [[ultralight aircraft]], designed and under development by [[Pegasus d.o.o.]] of [[Branik]]. The Flamingo was introduced to the public at the Aero show held in [[Friedrichshafen]] in 2010. The aircraft will be supplied as a complete ready-to-fly-aircraft and is expected to be distributed by [[Fly Synthesis]] in Europe.<ref name="WDLA11">Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 68. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X</ref> |
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==Design and development== |
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The Flamingo was designed to comply with the [[Fédération Aéronautique Internationale]] microlight rules and intended as both a touring aircraft for private ownership and a [[Trainer (aircraft)|trainer]] for flying school use. It features a cantilever [[low-wing]], a two-seats-in-[[side-by-side configuration]] enclosed cockpit under a [[bubble canopy]], fixed or optionally retractable [[tricycle landing gear]] and a single engine in [[tractor configuration]].<ref name="WDLA11" /> |
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The aircraft is made from composites. Its {{convert|8.7|m|ft|1|abbr=on}} span wing has an area of {{convert|10.53|m2|sqft|abbr=on}} and mounts [[Flap (aircraft)|flaps]]. The standard engine available will be the {{convert|100|hp|kW|0|abbr=on}} [[Rotax 912ULS]] [[four-stroke]] powerplant, which is expected to give a cruise of {{convert|260|km/h|mph|0|abbr=on}} for the fixed gear version and {{convert|310|km/h|mph|0|abbr=on}} for the retractable version.<ref name="WDLA11" /> |
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<!-- ==Operational history== --> |
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==Variants== |
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;EDA 100 Flamingo Fixed Gear |
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:Model with fixed [[landing gear]].<ref name="WDLA11" /> |
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;EDA 100 Flamingo Retracable Gear |
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:Model with retractable landing gear.<ref name="WDLA11" /> |
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<!-- ==Aircraft on display== --> |
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==Specifications (EDA 100 Flamingo) == |
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{{Aircraft specs |
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|ref=Bayerl<ref name="WDLA11" /> |
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|prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show --> |
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<!-- |
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General characteristics |
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--> |
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|genhide= |
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|crew=one |
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|capacity=one passenger |
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|length m= |
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|length ft= |
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|length in= |
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|length note= |
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|span m=8.7 |
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|span ft= |
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|span in= |
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|span note= |
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|height m= |
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|height ft= |
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|height in= |
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|height note= |
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|wing area sqm=10.53 |
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|wing area sqft= |
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|wing area note= |
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|aspect ratio= |
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|airfoil= |
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|empty weight kg=285 |
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|empty weight lb= |
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|empty weight note= |
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|gross weight kg=472.5 |
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|gross weight lb= |
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|gross weight note= |
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|fuel capacity={{convert|100|l}} |
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|more general= |
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<!-- |
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Powerplant |
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--> |
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|eng1 number=1 |
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|eng1 name=[[Rotax 912ULS]] |
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|eng1 type=four cylinder, liquid and air-cooled, [[four stroke]] [[aircraft engine]] |
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|eng1 kw=75<!-- prop engines --> |
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|eng1 hp=<!-- prop engines --> |
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|prop blade number= |
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|prop name= |
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|prop dia m= |
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|prop dia ft= |
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|prop dia in= |
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|prop note= |
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<!-- |
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Performance |
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--> |
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|perfhide= |
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|max speed kmh=260 |
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|max speed mph= |
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|max speed kts= |
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|max speed note= |
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|cruise speed kmh= |
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|cruise speed mph= |
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|cruise speed kts= |
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|cruise speed note= |
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|stall speed kmh=64 |
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|stall speed mph= |
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|stall speed kts= |
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|stall speed note= |
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|never exceed speed kmh=360 |
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|never exceed speed mph= |
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|never exceed speed kts= |
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|never exceed speed note= |
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|range km= |
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|range miles= |
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|range nmi= |
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|range note= |
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|endurance= |
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|ceiling m= |
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|ceiling ft= |
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|ceiling note= |
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|g limits= |
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|roll rate= |
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|glide ratio= |
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|climb rate ms=8 |
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|climb rate ftmin= |
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|climb rate note= |
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|time to altitude= |
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|sink rate ms= |
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|sink rate ftmin= |
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|sink rate note= |
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|lift to drag= |
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|wing loading kg/m2= |
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|wing loading lb/sqft= |
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|wing loading note= |
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|power/mass= |
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|thrust/weight= |
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|more performance= |
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|avionics= |
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}} |
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==References== |
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{{reflist}} |
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<!-- ==External links== --> |
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{{Aviation lists}} |
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[[Category:Slovenian ultralight aircraft 2010–2019]] |
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[[Category:Single-engine aircraft]] |
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