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词条 Solid Air Diamant Twin
释义

  1. Design and development

  2. Specifications (Diamant Twin with Bautek Pico wing)

  3. References

  4. External links

name=Diamant Twin image= caption=

}}{{Infobox Aircraft Type

type=Ultralight trike national origin=Germany manufacturer=Solid Air UL-Bau Franz designer= first flight= introduced= retired= status=In production (2013) primary user= more users= produced= number built= program cost= unit cost= €22,390 (2011) developed from= variants with their own articles=
}}

The Solid Air Diamant Twin ({{lang-en|Diamond}}) is a German ultralight trike, designed and produced by Solid Air UL-Bau Franz of Hundheim, Rheinland-Pfalz. The aircraft is supplied as a complete ready-to-fly-aircraft.[1]

Design and development

The Diamant Twin 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}} and, in fact, the aircraft has a maximum gross weight of {{convert|450|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 cockpit fairing, tricycle landing gear with wheel pants and a single engine in pusher configuration.[1]

The aircraft fuselage is made from fibreglass, with its double surface aluminum-framed wing covered in Dacron sailcloth. Unusually the engine firewall is made from fibreglass-laminated plywood. Its {{convert|10.1|m|ft|1|abbr=on}} span standard Bautek Pico wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar. The landing gear features fibreglass suspension. The powerplant is a horizontally opposed, four-cylinder, air-cooled, two-stroke, dual-ignition {{convert|83|hp|kW|0|abbr=on}} Hirth F-30 engine or, optionally a BMW four stroke powerplant.[1]

The aircraft has an empty weight of {{convert|190|kg|lb|0|abbr=on}} and a gross weight of {{convert|450|kg|lb|0|abbr=on}}, giving a useful load of {{convert|260|kg|lb|0|abbr=on}}. With full fuel of {{convert|40|l}} the payload is {{convert|231|kg|lb|0|abbr=on}}.[1]

A number of different wings can be fitted to the basic carriage, including the Bautek Pico and the La Mouette Ghost 12 and 14.[1]

Specifications (Diamant Twin with Bautek Pico wing)

{{Aircraft specs
|ref=Bayerl[1]
|prime units?=met


|genhide=
|crew=one
|capacity=one passenger
|length m=
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|span m=10.1
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|wing area sqm=14.8
|wing area sqft=
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|aspect ratio=
|airfoil=
|empty weight kg=190
|empty weight lb=
|empty weight note=
|gross weight kg=450
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|40|l}}
|more general=


|eng1 number=1
|eng1 name=Hirth F-30
|eng1 type=horizontally opposed, four-cylinder, air-cooled, two-stroke, dual-ignition aircraft engine
|eng1 kw=
|eng1 hp=83
|prop blade number=3
|prop name=composite
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=150
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=92
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=60
|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=4.5
|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=30.4
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 222. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

External links

  • {{Official website|http://www.diamantenwerft.de/solid-air/flugzeuge/diamant-twin/}}
{{Solid Air aircraft}}

5 : German sport aircraft 2000–2009|German ultralight aircraft 2000–2009|Single-engined pusher aircraft|Ultralight trikes|Solid Air aircraft

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