1. Design and development

2. Specifications (MH-46 Eclipse)

3. References

4. External links

The Aerosette MH-46 Eclipse is a Czech ultralight aircraft, designed and produced by Aerosette of Chrastava. The aircraft is supplied as a complete ready-to-fly-aircraft.^[1][2]

Design and development

The MH-46 was designed to comply with the Fédération Aéronautique Internationale microlight rules and intended for personal use and flight training. It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.^[1][2]

The aircraft is made from composites. Its {{convert|9.71|m|ft|1|abbr=on}} span wing is supported by a single strut on each side. Standard engines available are the {{convert|64|hp|kW|0|abbr=on}} Rotax 582 two-stroke and the {{convert|100|hp|kW|0|abbr=on}} Rotax 912ULS four-stroke powerplant. The cockpit was designed for comfort and is {{convert|1.2|m|in|0|abbr=on}} wide at the pilot's elbow.^[1][2]

Specifications (MH-46 Eclipse)

|genhide=
|crew=one
|capacity=one passenger
|length m=6.34
|length ft=
|length in=
|length note=
|span m=9.71
|span ft=
|span in=
|span note=
|height m=2.18
|height ft=
|height in=
|height note=
|wing area sqm=11.5
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=285
|empty weight lb=
|empty weight note=
|gross weight kg=472.5
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|130|l}}
|more general=

|eng1 number=1
|eng1 name=Rotax 912ULS
|eng1 type=four cylinder, liquid and air-cooled, four stroke
|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=250
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=220
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=65
|stall speed mph=
|stall speed kts=
|stall speed note=flaps down
|never exceed speed kmh=298
|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=+4/-2
|roll rate=
|glide ratio=
|climb rate ms=8.7
|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=
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}

References

External links

• {{Official website|http://www.aerosette.eu/}}

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