- Design and development
- Specifications (Martin3 S100)
- References
- External links
| name=Martin3 S100 | image=File:Colyaer Martin3 S100 - 01.jpg | caption= }}{{Infobox Aircraft Type | type=Ultralight aircraft | national origin=Spain | manufacturer=Colyaer | designer= | first flight= | introduced= | retired= | status=In production | primary user= | more users= | produced= | number built= | program cost= | unit cost= | developed from= | variants with their own articles=Colyaer Freedom S100
}} |
The Colyaer Martin3 S100 is a Spanish ultralight aircraft, designed and produced by Colyaer of Portonovo.[1][2] Design and developmentThe aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in pusher configuration.[1][2] The aircraft is made from composites. Its {{convert|12.4|m|ft|1|abbr=on}} span wing has an area of {{convert|12.0|m2|sqft|abbr=on}} and flaps that can be deployed for landing and reflexed for cruise flight. The long wingspan gives the Martin3 a glide ratio of 23:1 and allows power-off soaring flights. The standard engine is the {{convert|100|hp|kW|0|abbr=on}} Rotax 912ULS four-stroke powerplant.[1][2] In 2015 the aircraft was marketed by Galicia Avionica SL.[3] Specifications (Martin3 S100) {{Aircraft specs
|ref=Bayerl[1]
|prime units?=met
|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=
|length in=
|length note=
|span m=12.4
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=12.0
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=280
|empty weight lb=
|empty weight note=
|gross weight kg=450
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|140|l}}
|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=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=
|perfhide=
|max speed kmh=260
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=180
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=65
|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=5
|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=37.5
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}
References1. ^1 2 3 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 36. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
2. ^1 2 Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 132. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
3. ^Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 57. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}
External links{{commons category|Colyaer aircraft}}- {{Official website|http://www.colyaer.com/martin3eng.htm}}
{{Colyaer aircraft}} 3 : Spanish ultralight aircraft 1990–1999|Homebuilt aircraft|Single-engined pusher aircraft |